767fuelingmanual.pdf

AIR TRANSPORT INTERNATIONAL

B767 FUELING MANUAL This manual is the property of Air Transport International, Limited Liability Company. It is issued for the use of Air Transport International, Limited Liability Company authorized personnel.

Revision Number:

Issued:

1

07-29-09

All rights reserved, including the right to reproduce this publication. No part may be reproduced: stored in any retrieval system: or transmitted in any part or form by any means electronic, photocopying, microfilm, microfiche, mechanical, or otherwise, without prior written permission of Air Transport International, Limited Liability Company.

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AIR TRANSPORT INTERNATIONAL RECORD OF REVISIONS TYPE MANUAL: ATI REVISION NO. Complete thru Rev. 01

B767 Fueling Manual

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL TABLE OF CONTENTS ATI B767 FUELING MANUAL TABLE OF CONTENTS 01 - GENERAL PROCEDURES 02 - PERSONNEL REQUIREMENTS FOR FUELING 03 - TURBINE ENGINE FUEL SUBSTITUTIONS 04 - SAFETY REQUIREMENTS 05 - BIOCIDE TREATMENT OF FUEL TANKS 06 - RESERVED FOR FUTURE USE 07 - B767 FUELING PROCEDURES 08 - FUEL MEASURING STICK TABLES

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 01 - GENERAL PROCEDURES TABLE OF CONTENTS 01.01 - GENERAL FUELING PROCEDURES 01. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02. Contract Fuel Facilities . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03. Non-Contract (AD Hoc) Fuel Facilities . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 04. Contaminated Fuel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 05. Turbine Aircraft Fueling Unit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 06. Fuel Quantity Measurement and Verification . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 07. Refueling Policy . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 08. Use of Fuel Truck Meter and Fueling Tolerance . . . . . . . . . . . . . . . . . . . . . . . . . . . . 09. Using Fuel Measuring Sticks (Magnastick) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10. Draining of Aircraft Sumps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11. Minimum Fuel Requirement. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12. Who To Contact For Problems Relating To Fuel Servicing . . . . . . . . . . . . . . . . . . . . 13. Hydrometer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14. Glossary of Terms . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

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01.01.1 01.01.1 01.01.1 01.01.2 01.01.3 01.01.7 01.01.8 01.01.8 01.01.9 01.01.10 01.01.11 01.01.12 01.01.12 01.01.12

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 01 - GENERAL PROCEDURES 01.01 GENERAL FUELING PROCEDURES 1. Introduction. This manual will be distributed to all station fueling contractors, installed on each aircraft, and will be strictly adhered to. (FAR 121.135, 121.137). a. Management is responsible for determining that fueling regulations are followed at all times whether fueling is being done by employees or contract fuelers. The only exception will be where some ordinances may conflict (military and foreign countries) with regulations. b. The grade and type of fuel to be used in airplanes is outlined in the ATI B767 Fueling Manual. Individuals not having this manual must contact Maintenance regarding type and grade of fuel. (See Section 03.01, Table 3.01-1 for approved fuels). (1) The use of fuel other than Jet A/A1 is authorized for turbine engines. It will be the responsibility of the person fueling the airplane to determine that action is taken to notify Maintenance whenever fuel other than kerosene type is used. Procedures which must be followed after the use of turbine fuel other than kerosene are contained in Section 3.01, Turbine Engine Fuel Substitution. 2. Contract Fuel Facilities a. Contract fuel facilities will ensure that fuel delivered is free of contamination. This may be accomplished by the contract agency verifying with adequate records that their fuel is maintained free of contamination by an acceptable and recognized method. Reports will be forwarded to Quality Control. b. In the event it is necessary to fuel a company aircraft from a contract agency that does not have adequate records to prove their fuel is free of contamination, no fuel will be delivered to the company aircraft until the fuel facility is audited and fuel checked for contamination. The aircraft Captain shall be primarily responsible for the above when obtaining fuel from any facility not normally used by the company. 3. Non-Contract (AD Hoc) Fuel Facilities. As a supplemental air carrier, ATI operates into many remote and unique locations on a one-time basis with little or no advance notice. It is impossible under these circumstances to accomplish surveillance in advance of the aircraft arriving at these locations. ATI may use non-contract fuel servicing facilities, which it encounters associated with its activity as a supplemental air carrier, in accordance with the following guidelines: a. The Captain shall be notified that this procedure is required through the ATI Charter Advisory Summary. Upon the notification to the Captain, the following shall apply: (1) Prior to fueling from a non-contract fuel facility, a qualified ATI employee, as delegated by the Captain, shall determine that the correct grade of fuel is available and that it will be delivered into the aircraft in a pure, uncontaminated state. Revision 1

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01.01.1

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 01 - GENERAL PROCEDURES (2) For all fueling operations (hydrant and truck), review of the filter change due date placard located on the vehicle or hydrant to ensure it has not expired and that the daily inspection requirements are completed and annotated on the records with the unit. (3) Sump the fuel truck prior to delivering fuel into the aircraft, and evaluate the contamination level present in the fuel in accordance with paragraph 4 following. (4) Annotate the results of this requirement in the Aircraft Logbook. Aircraft Logbook entry will be: Discrepancy Block: “Fuel Source Inspection Required”; Corrective Action: “Fuel Source Inspection C/W Per Fueling Manual 1.01”. Enter the Signature and Certificate Number of the Person who performed the inspection. b. Only a qualified ATI employee, as delegated by the Captain, will supervise and/or fuel the aircraft, ensuring compliance with ATI fueling procedures. 4. Contaminated Fuel a. The color of jet fuel generally ranges from water white to light straw or amber. Other colors may be an indication the fuel has been contaminated by other products or unauthorized additives. In such cases, it will be the facility operator’s responsibility to discontinue fuel transfer and/or receipt and quarantine product until fuel has been determined acceptable for aircraft use. b. Procedures (1) If contaminated turbine fuel has been loaded into airplane tanks, thoroughly drain all sumps to ensure removal of any water or other substance that will not mix with the fuel. Observe JP-4 procedures. Notify Maintenance Control. (2) Drain approximately one gallon of turbine fuel from the sump into a clean, white, dry container. Ensure both sump valves are closed after draining the sump. (3) Place the container on a level surface and check the bottom of the container for water droplets, solid contaminants, and/or hazy, cloudy or discolored fuel. (4) If the fuel sample is other than clean and bright, retain the one gallon sample in a sealable container and notify Maintenance Control of the findings. Repeat sump draining until no further contamination is found. Identify the type of contamination using these terms:

(1) (2) (3) (4)

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b. Solid Contaminant Clear Slight Particulate Matter Particulate Matter Dirty

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(1) (2) (3) (4) (5)

c. Moisture Content Bright Hazy Cloudy Wet (free water) Discoloration

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 01 - GENERAL PROCEDURES c. Definition of Solid Contaminant Levels (1) Clear: Refers to lack of particles, silt or sediment, flakes or dye, rust or solids. (2) Slight Particulate Matter: Contains several fine to moderate sized particles. (3) Particulate Matter: A sample in which many small particles may be seen floating or settled to the bottom. (4) Dirty: Discoloration, or many particles dispersed in the fuel or have settled to the bottom. Also, brown slimy material. d. Definition of Moisture Content Levels (1) Bright: Brightness is a quality independent of the color of the sample and refers to the lack of suspended or free water in the sample. Bright fuel tends to sparkle. (2) Hazy: A condition resulting from fine droplets of moisture dispersed throughout the sample producing a dull, hazy appearance. This is usually a temporary condition brought about by a drop in temperature. This condition can also occur when the sample is aerated as a result of being obtained when the dispensing system is pressurized. (3) Cloudy: The result of minute droplets of water dispersed throughout the sample rendering it from semi- to completely opaque. (4) Wet: Any form of free water from droplets to bulk water found in bottom of container or clinging to the sides. (5) Discoloration: Any water accumulation that shows a brown or black color is cause for further investigation by Maintenance. This type contamination is usually the result of fuel delivery or refinery problems and must be resolved with the contract Oil Company. e. Emergency Procedures Familiarization. All personnel involved with the fueling of airplanes are responsible for being completely familiar with all emergency procedures relative to the fueling operation. This must include familiarization with: (1) Emergency procedures to stop the flow of all fuel from the fueling facility. (2) Procedures to be followed when fuel spillage occurs. (3) Location of all emergency and fire fighting equipment and its use. 5. Turbine Aircraft Fueling Unit a. These instructions cover the use of aircraft fueling equipment. In addition, these instructions can be used to monitor procedures of contract personnel servicing aircraft.

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01.01.3

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 01 - GENERAL PROCEDURES b. Vehicle Positioning (1) Positioning of fueling unit will be determined by local station management to suit each situation. CAUTION:

DO NOT CONTINUE THE APPROACH OF FUELING UNITS IF FEELER ANTENNAS CONTACT AIRPLANE WING.

(2) Drive unit outboard of number one engine pod to fuel B767 Series. Stop unit with rear platform under fuel caps. Set parking brake. Put gearshift in neutral. Install chocks. (3) If hydrant pit location or ramp congestion makes preceding impractical, back the unit in between engine pods from leading edge of wing. Stop the unit with rear platform under fuel caps. Set parking brake. Put gearshift in neutral. Install chocks. (4) Turn drive-fuel switch to FUEL position, if installed. (5) Never attempt to move fueling unit either by pushing or with engine power when it is attached to the fuel pit or to the airplane. c. Bonding (Reference NFPA-407) (1) Prior to making any fueling connection to the aircraft, the fueling equipment shall be bonded to the aircraft by use of a cable, thus providing a conductive path to equalize potential between the fueling equipment and aircraft. The bond shall be maintained until fueling connections have been removed, thus permitting the reuniting of separated charges that could be generated during the fueling operation. (2) In addition to the above, when fueling overwing, the nozzle shall be bonded with a nozzle bond cable having a clip or plug to a metallic component of the aircraft that is metallically connected to the tank filler port. The bond connection shall be made before the filler cap is removed. If there is no plug receptacle or means of attaching a clip, the operator shall touch the filler cap with the nozzle spout before removing the cap so as to equalize the potential between the nozzle and the filler port. The spout shall be kept in contact with the filler neck until the fueling is completed. (3) When a hydrant servicer or cart is used for fueling, the hydrant coupler shall be connected to the hydrant system prior to bonding the fuel equipment to the aircraft. (4) Bonding and fueling connections shall be disconnected in reverse order of connection. d. Hook-up Hydrant Cart (1) Check condition of mating surface of fuel and sensing lines for cleanliness and burrs before making connections. (2) Open hydrant pit cover and check for presence of water or other contaminants. Do not connect inlet hose to hydrant valve if water is less than 3 inches below top of valve. 01.01.4

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 01 - GENERAL PROCEDURES (3) Connect inlet hose to hydrant valve. (4) Connect sense line coupling to hydrant valve. e. Check prior to fueling - all types of fueling units. (1) Air pressure check. Check pressure in air receiver. If less than 95 psi, run engine at fast idle until it builds up to 95 psi. (If more than two minutes are required, the unit is leaking and must be checked by maintenance personnel after fueling. Advise Supervisor.) Resume fueling if 70 psi is available in air receiver. (2) Pressure control check: (a) Connect underwing hoses; lock the underwing nozzles in the aircraft fill fitting adapters. (b) Squeeze deadman control and observe fuel pressure rise on operator's gauge. Maximum allowable pressure is 70 psi. If pressure is within this limit, release deadman control. (c) Open the underwing fuel nozzle valve. Unit is now ready to fuel aircraft. (d) If pressure is above 70 psi in step (1) preceding, notify Supervisor. Remove truck from service. Fuel truck and hydrant valve must be checked before it continues in service. f. Aircraft Servicing (1) Set fuel meter(s) to zero. (Record meter reading on form provided, as required.) CAUTION:

IF ONLY ONE HOSE IS USED DURING FUELING, THE MANUAL SHUTOFF (IF INSTALLED) FOR THE UNUSED HOSE MUST BE CLOSED.

(2) Depress deadman control. This control must be held in the fueler's hand. Do not release deadman control during the fueling operation, except in case of emergency such as fire, fuel leak, accident, or incident which would endanger personnel or the aircraft. WARNING: TO BLOCK OPEN DEADMAN CONTROL WILL BE CAUSE FOR DISMISSAL OF THOSE INVOLVED. (3) Fueler position (a) The fueler must be positioned to observe the fueling vehicle delivery meter and fueling pressure gauge, the hydrant valve and aircraft connections, the meter and some of the operation on the other side of the aircraft. In no circumstances will the fueler be in the cab or on the seat of the vehicle during operation. Original

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 01 - GENERAL PROCEDURES (4) Duties of operator during fueling: (a) Observe fueling pressure gauge for proper operating pressure. Maximum pressures are: Steady Flow: Surge: Lock-In: NOTE:

40 psi 120 psi (during aircraft fill valve closure) 70 psi (during pre-fueling pressure control check)

Pressure fluctuations up to 45 psi allowable at flow rated below 50 gpm.

(b) Monitor filter pressure differential during steady high rate flow. Allowable limits: Minimum -1/2 psi Maximum-12 psi (Filter / separators) -24 psi (Bendix "Go-No-Go" Fuse) (c) Watch for leaks on the truck, (including hoses that are not in use) hydrant pit or at the aircraft. (d) An increase in steady flow pressure to above 40 psi is an indication that the primary pressure control valve is malfunctioning. Fueling may be completed with the secondary valve control provided fueling pressure remains below 50 psi. When fueling is complete, the refueler on hydrant truck and hydrant pit must be removed from service. (e) Stop fueling immediately if fuel pressure exceeds 50 psi. Remove fueling vehicle and/or hydrant pit from service. (5) Irregularities (a) Report all irregularities to supervisor. Supervisor will advise Maintenance. Irregularities include but are not limited to: inoperative gauges, sticking or erratic gauges, inoperative transit lights, inoperative fill valve, early closing high level shutoffs, discrepancies between cockpit and underwing gauges, etc. Reporting is required to ensure the aircraft is scheduled for repair and to alert down line stations of potential problems. (b) In the event fueling unit shuts down during operation, immediately check the following: 1) Pump switch in hydrant pit (Where installed). 2) Sense coupler hydrant valve for proper seating. 3) Check air pressure in receiver. 70 psi minimum is needed for operation. 01.01.6

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 01 - GENERAL PROCEDURES 4) After checking 1), 2), and 3) preceding, if trouble is not corrected, notify Supervisor who will request aid from maintenance personnel. (6) Completion of fueling operation. When fueling is complete: (a) Take magnastick reading, if required. (b) Open one aircraft fill valve momentarily. (This releases lock-up pressure in system). Check to see that operator's pressure gauge reading drops to 0-5 psi. Close fill valve. (c) Disconnect underwing nozzle, stow and lock in receptacle. Do not drag coupler, carry to truck. Replace dust caps. (d) Install and lock caps on aircraft fueling adapters. (e) Replace airplane fitting covers and close access doors where installed. (f) Disconnect and stow hydrant hose or boom and sense coupler. Do not drag hoses. Walk or carry to truck. (g) Replace dust caps on hydrant pit valve and sense coupler. Close lid. (h) Disconnect ground wires from airplane. Disconnect ground wire from ramp fitting. NOTE: Walk ground wires into reel. Do not let clips drag on ground. (i) (j)

Record fuel delivered from meter reading on proper form. If unit cannot be driven because of an interlock malfunction, recheck hose storage fitting. If the unit still cannot be driven, call Supervisor. NOTE: Do not operate sealed switches on dashboard (when provided) unless ordered to by Supervisor.

(k) Truck cannot be driven away from aircraft unless all connections and hoses are stowed properly in their receptacles. This actuates interlocks, which make it possible to drive the truck. 6. Fuel Quantity Measurement and Verification a. The quantity of fuel aboard an airplane must be accurately determined before dispatch whenever fuel has been added or removed. b. Determination of fuel quantity is accomplished by fueling (or defueling) to desired aircraft gauge amount and then verifying by comparison with the meter on the fueling vehicle. Verification is required every time an aircraft is refueled. c. Magnastick reading will be taken and recorded under the following circumstances: (1) When "Calculated Gallons to be Added" and gallon from fuel truck differ by more than the allowable tolerance. (2) When required by "Gauge Inoperative " Special Procedures. Original

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 01 - GENERAL PROCEDURES (3) When requested by the Flight Crew. NOTE:Refer to Minimum Equipment List if magnastick inoperative. 7. Refueling Policy a. It should be understood that ATI does not own the refueling concession that refuels our aircraft. However, the Company will ensure the following policies are adhered to during refueling or defueling. (1) (2) (3) (4) (5) (6)

Refueling units will be maneuvered with caution in the refueling areas. Proper clearance will be maintained between the aircraft and refueling unit. Fueling and defueling must always be accomplished out-of-doors. During refueling and defueling, bonding wires must be used. At no time are fueling nozzle levers to be blocked or wedged open. In the event fuel is spilled, extra precautions should be taken to ensure sufficient time has elapsed for complete dissipation of fumes before the battery master switch or outside power connection is changed. Also, if spillage is excessive and ground or ramp is covered with fuel, fire fighting apparatus should be called to clear area of fuel and fumes by flooding area with water and/or chemicals as required. A clearance will then be obtained from the fire department before continuing the operation.

8. Use of Fuel Truck Meter and Fueling Tolerance a. Test Fuel Quantity Gauges (1) If any do not test, notify Maintenance and use "Gauge Inoperative" fueling procedure. (2) If gauges test OK, continue to step “b” following. b. Determine quantity of fuel aboard before fueling by use of the fuel tank quantity gauges. (1) Do not use totalizer or flight log figures. (2) Be alert to differences in gauge readings which could indicate a faulty gauge. Refer to specific airplane fueling procedures for tolerances and action. c. Subtract this amount from total quantity to be aboard (including taxi fuel) to obtain calculated pounds to be added. d. Pump fuel into aircraft tanks. Stop fueling each tank short of the desired amount (about 200 pounds on standard body aircraft). Trim each tank until the desired amount is reached. At the same time monitor the truck meter. The goal is to obtain desired aircraft gauge quantities and truck calculated gallons to be added at the same time.

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 01 - GENERAL PROCEDURES CAUTION:

FUEL QUANTITY GAUGES MUST BE CLOSELY MONITORED DURING ENTIRE FUELING OPERATION TO DETECT FAULTY GAUGE(S) (I.E.GAUGE LAGS OR COMPLETELY STOPPED) WHICH COULD CAUSE A FUEL SPILL.

(1) Each tank gauge must indicate the desired amount, never less. e. Compare actual number of gallons pumped into plane (as read on truck meter) to the calculated gallons to be added: (1) If the number of gallons added to bring all gauges to their desired reading is less than the amount calculated to be added, retest gauges to ensure none have failed during fueling. Then add more fuel until the actual gallons loaded equals the calculated gallons to be added. (a) This additional fuel may cause the aircraft fuel gauges to indicate slightly more than the desired amounts and may fill the tanks to automatic shutoff. If auto shutoff occurs before the correct amount is boarded, the remainder of the fuel may be added to the next tank in the fueling sequence. (2) If the number of gallons added to bring the gauges to their desired readings is more than the amount calculated but does not exceed the listed tolerance, the load is verified as OK. (3) If preceding steps fail to achieve agreement between fuel truck meter and calculated amount to be added, the fuel load must be verified by use of magnasticks. Maintenance must be advised of this condition. They will review actual gauge reading and magnastick reading to identify any gauges which may be in need of calibration. They will repair or defer as necessary. 9. Using Fuel Measuring Sticks (Magnastick) a. Magnastick readings taken without regard to airplane attitude are used to confirm distribution of fuel to proper tanks. b. Magnastick limits applicable to all aircraft are -2.0 inch, +2.0 inch. c. Magnastick charts which convert observed stick readings in inches to equivalent gallons and also to pounds will be found in the Fueling Manual for each specific airplane. d. When any cockpit gauge is inoperative, fueling must be accomplished by the "Gauge Inoperative" special procedure in Section 07.05. When adding fuel to a tank with an inoperative fuel quantity indicating system, the primary reference is the operative portion(s) of the airplane system and/or the fuel truck meter. Magnastick, when specified, is a backup device used to confirm that fuel has been added to the correct tank in the approximate amount. Original

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 01 - GENERAL PROCEDURES 10. Draining of Aircraft Sumps a. Sumps will be drained into a clean, dry container and inspected for the presence of contamination under the following conditions: (1) Prior to each aircraft fueling, except for: (a) last minute topping off of fuel prior to departure (with fuel obtained from a Company approved fuel vendor), or (b) for fuel added at intermediate stops (with fuel obtained from a Company approved fuel vendor). WARNING: IF FUEL IS OBTAINED FROM A NON-CONTRACT FUEL FACILITY, SECTION 1.01, SUBPARAGRAPH 3, NON-CONTRACT (AD HOC) FUEL FACILITIES, PROCEDURES MUST BE FOLLOWED. (2) Within one hour prior to flight if the aircraft has been on the ground for a period of 12 hours or more and is not being fueled for its next flight. b. If contamination is noted on a sump inspection, the sumps will be drained until all presence or indications of contamination are eliminated. c. When the fuel temperature is below 0° C (32° F) the fuel tank sumps need not be drained. d. An aircraft that has been in a heated hangar when the outside air temperature is below 0° C (32° F) must have the fuel sumps drained before removal from the hangar. 11. Minimum Fuel Requirement a. The FAA Approved Flight Manual for each type of airplane lists the minimum fuel for dispatch. b. The figures shown do not include the taxi fuel allowance. c. Minimum fuel loads must be equally distributed in the main tanks. NOTE: See individual fueling charts for actual fuel distribution.

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 01 - GENERAL PROCEDURES

DENSITY

U. S.

SPECIFIC

POUNDS PER

GALLONS

GRAVITY

U. S. GALLON 6.90 6.89 6.85 6.80 6.75 6.70 6.65 6.60 6.55 6.50 6.45

PER POUND .1449 .1451 .1460 .1470 .1481 .1492 .1503 .1515 .1526 .1538 .1550

60°/60* F .8287 .8275 .8287 .8168 .8107 .8048 .7988 .7927 .7868 .7807 .7747

DEGREES API 39.25 39.5 40.5 41.75 43.05 44.3 45.65 47.0 48.35 49.7 51.15

RELATIONSHIP BETWEEN FUEL DENSITY SPECIFIC GRAVITY AND A.P.I. DEGREES Table 1.01-1 POUNDS PER

POUNDS PER

POUNDS PER

U. S. GALLON 6.9 6.8 6.7 6.6 6.55 6.5

IMPERIAL GAL. 8.287 8.167 8.047 7.927 7.807 7.807

LITER 1.823 1.797 1.770 1.744 1.731 1.717

RELATIONSHIP BETWEEN POUNDS PER U.S. GALLON/PER IMPERIAL GALLON/ PER LITER Table 1.01-2 CONVERSION FACTORS 1 U.S. GALLON 1.201 U.S. GALLON 0.2642 U.S. GALLON

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= = =

0.8327 IMPERIAL GALLON 1 IMPERIAL GALLON 0.220 IMPERIAL GALLON

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= 3.785 LITER = 4.546 LITER = 1 LITER

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 01 - GENERAL PROCEDURES 12. Who to Contact for Problems Relating to Fuel Servicing a. Technical problems encountered during fueling will immediately be brought to the attention of the ATI employee supervising the fueling. The status of such problems will be communicated to Maintenance Control. Problems

Manual Reference

Leaks: Inoperative Valves W/O elec power Overwing Fueling: Excess Fueling Pressure: Contamination: Defueling: Fuel Spills:

Boeing 767 Structural Repair Manual Fueling Manual, Section 07.07 Fueling Manual, Section 07.08 Fueling Manual, Section 01.01 Fueling Manual, Section 01.01 Fueling Manual, Section 07.09 Fueling Manual, Section 04.01

b. For assignment of additional manuals, extra manual pages, replacement of lost or damaged pages contact the Quality Control Manager of Publications and Training. 13. Hydrometer: Used to Measure Specific Gravity of Fuel Thermo-Hydrometer-S.G. (or equivalent) Range .750 to 850 SP. GR. Range .20° F TO 130° F 14. Glossary of Terms a. Actual Fuel: The total amount of fuel that is actually loaded; the sum of minimum cleared, including Structural Check and Payload Fuel and Taxi Fuel. b. Ballast Fuel: See payload fuel. c. Cleared Fuel: The fuel planned for the trip plus reserve and contingency fuel. On multi-stop trips where refueling is not planned, a cleared fuel load for each down line departure can be developed by the originating flight plan. Flight Operations has stated that the display fuel load for the thru station is the Operations Agent source for the fuel load at that station. It DOES NOT account for the taxi-out fuel allowance. (Ref. Minimum Cleared Fuel). d. Ferry Fuel: The amount of fuel carried in addition to the Minimum Cleared Fuel. This will be in accordance with procedures applying when down line stations are set up for preplanned through fuel loads or other special cases which may be requested. 01.01.12

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 01 - GENERAL PROCEDURES e. Minimum Cleared or Required Fuel: The amount of fuel required for a given trip after consideration of trip length, altitude, wind conditions, alternate specified, Federal Aviation Regulations, and Company regulations. Minimum cleared fuel is equal to the planned trip burnout plus reserve fuel and any contingency fuel. It does not include any taxi fuel allowance for the fueling origination. (Ref.: Cleared Fuel, Ferry Fuel, Payload Fuel). f. Payload Fuel: Fuel that is not planned to be burned. May be intended to avoid or minimize down line refueling (see Ferry Fuel), may be the result of inoperative tanks, or may involve Balance Control where fuel is used as ballast. See Structural Check Fuel. g. Refueled Origination: Any trip departure after the airplane has been refueled; not necessarily the same as trip origination. h. Required Fuel: See Minimum Cleared Fuel i. Structural Check Fuel: The design of an airplane is predicated on a defined fuel loading and burnout schedule. In some designs it is permissible to mismanage the fuel loading provided the structural implications are checked. The most common situation is when the wing tanks are not filled before fuel is loaded and the fuel load is equalized. Both involved refueling fuel spill protection. Structural check fuel differs from payload fuel in that it is cleared or usable fuel. j. Taxi Fuel Allowance: Since the engines will burn off some fuel in the process of taxiing out to the end of the runway, a better measure of the actual takeoff gross weight will result if this factor is taken into account. Further, under some circumstances it will be possible to accommodate more payload by recognizing a taxi fuel allowance. The taxi fuel allowance is periodically updated to fit changing conditions. 15. Fueling Facilities Inspection and Report a. The guidance for maintenance personnel in performing inspections fo the fueling facilities can be found in the ATI GMM, Section 5.109. b. The Fuel Equipment Inspection Report (Form M-11) can be found in the ATI GMM, Section 4.03.

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 02 - PERSONNEL REQUIREMENTS FOR FUELING TABLE OF CONTENTS 02.01 - PERSONNEL REQUIREMENTS FOR FUELING 01. Pressure Fueling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02. Overwing Fueling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03. Ground Personnel Responsibilities . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 04. Maintenance Personnel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 02 - PERSONNEL REQUIREMENTS FOR FUELING 02.01 PERSONNEL REQUIREMENTS FOR FUELING NOTE: A qualified fueler may be the Operations or Maintenance person assigned to supervise the contract fuel vendor during the fueling operation. 1. Pressure Fueling a. One qualified fueler may perform the entire fueling operation if the use of one person meets local municipal regulations. Personnel assigned to fueling will make the necessary connections from the fueling facility to the airplane. They will also operate the necessary controls to fuel the airplanes. b. The person assigned to fuel the airplane will closely observe the fueling operation and be alert for any sign of malfunction or dangerous condition. CAUTION:

FUEL QUANTITY GAUGES MUST BE CLOSELY MONITORED DURING ENTIRE FUELING OPERATION TO DETECT FAULTY GAUGES (I.E. GAUGE LAGS OR COMPLETELY STOPS) THAT COULD CAUSE A FUEL SPILL.

2. Overwing Fueling. One qualified fueler may perform the entire fueling operation if the use of one person meets local municipal regulations and if that person can monitor the fuel truck meter from the fueling position. 3. Ground Personnel Responsibilities a. All Aircraft. Ground personnel will be responsible for positioning, connecting and operating the fueling unit(s) and take magnastick readings when required. b. B767. The qualified person delegated this responsibility, will operate the fueling controls and fill the fuel tanks to the quantity desired. When fueling is completed, the qualified person delegated this responsibility, will take magnastick readings if required and check these readings against the quantities on the Magnastick Chart. 4. Maintenance Personnel. Maintenance Personnel are responsible for the following items when assigned to fuel or defuel: a. The proper fuel load and proper grade fuel.

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 02 - PERSONNEL REQUIREMENTS FOR FUELING b. Ensure the aircraft was not damaged during refueling and/or defueling. If the aircraft was damaged, notify Maintenance Control and take appropriate action. NOTE: The responsibility for ascertaining that the fueling or defueling is properly accomplished for flight rests with the Captain.

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 03 - TURBINE ENGINE FUEL SUBSTITUTIONS TABLE OF CONTENTS 03.01 - TURBINE ENGINE FUEL SUBSTITUTIONS 01. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02. Fueling with JP-4/Jet B or When Aircraft Contains Residual JP-4/Jet B Fuel. . . . . . 03. Slow Rate Pressure Fueling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 04. Overwing Fueling Procedure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 05. Placards . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 03 - TURBINE ENGINE FUEL SUBSTITUTIONS 03.01 TURBINE ENGINE FUEL SUBSTITUTIONS 1. General a. All fuels listed in Table 3.01-1 are approved for all aircraft subject to special requirement where noted. FUEL TYPE IN ORDER OF PREFERENCE 1. JET A or JET A-1

ENGINE TYPE CF6-80A

2. JP-5

CF6-80A

3. JP-8

CFM6-80A

4. JP-4

CF6-80A

5. JET B

CF6-80A

NOTES Acceptable for use in all ATI aircraft. Primary fuel choice. Military Specification fuel. Kerosene type jet fuels. May not meet new fuel specifications in all respects, but are acceptable. Military Specification wide-cut kerosene/ naphtha mixed fuel. MAY ONLY BE USED SUBJECT TO SPECIAL REQUIREMENTS AND APPROVALS LISTED BELOW. JET B is the commercial equivalent of JP-4, subject to the same special handling as JP-4.

FUEL AND ENGINE TYPES Table 3.01-1 b. JP-4 or Jet B Fuel - Special Considerations (1) For purpose of this procedure, the terms JP-4 and Jet B refer to Wide-Cut (Kerosene and Naphtha mixture) type fuels. (2) These fuels, when mixed with Kerosene type fuels, may increase the risks of fire and explosion unless adequate precautions are taken to prevent electrostatic spark ignition of flammable fuel/air vapors in the fuel tanks. When Kerosene and Wide-Cut fuels are mixed, the resulting fuel/air vapor have new and usually broader flammability characteristics, thereby increasing chances of an ignitable mixture. (3) Electrostatic charges are generated as fuel passes through the servicing equipment and by agitation and splashing in the tank. The Filter/Separator on the Refueling Unit is normally the primary source of electrostatic charge on fuel. Original

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 03 - TURBINE ENGINE FUEL SUBSTITUTIONS 2. Fueling with JP-4/Jet B or When Aircraft Contains Residual JP-4/Jet B Fuel a. Advise Maintenance prior to fueling. b. Slow fueling is required whenever JP-4/Jet B is added to an aircraft and the fuel does not contain ASA-3 or other antistatic additives. Slow fueling is also required if aircraft tanks contain JP-4/ Jet B with or without antistatic additive and Jet A type fuels are being added. c. Slow fueling will continue for 20 flying hours after last fueling with JP-4/Jet B. Refer to paragraph 3 below for Slow Rate Pressure Fueling Procedures. d. All Aircraft Fueling Panels and Log Books will be placarded whenever an aircraft has been fueled with JP-4/Jet B. Refer to paragraph 5 for placarding details. 3. Slow Rate Pressure Fueling a. Slow Rate Pressure Fueling Procedures are the same for dispensing JP-4/Jet B or for dispensing Jet A type fuels into a tank containing residual JP-4/Jet B. CAUTION:

SLOW RATE FUELING IS MANDATORY WHEN AIRCRAFT CONTAINING RESIDUAL JP-4/JET B IN ITS TANKS IS TO BE FUELED BY FUELS NOT CONTAINING ANTISTATIC ADDITIVES.

b. Slow rate pressure fueling is accomplished by connecting only one fueling hose to the Underwing Fueling Adapter. Two fueling vehicles may be used, with each connected to a separate Fueling Adapter on the left wing. It may be necessary to regulate the hose Shutoff Valve to further reduce fuel flow so that flow does not exceed 50% of the rated flow. NOTE: Slow rate fueling refers to rate of flow, through fueling vehicle, not to flow rate in aircraft. CAUTION:

CLOSE THE MANUAL SHUTOFF VALVE AHEAD OF UNUSED HOSE ON FUELING VEHICLE WHEN ONLY USING ONE HOSE DURING FUELING.

4. Overwing Fueling Procedure a. The overwing fueling rate is limited to maximum 3 feet per second, as tabulated below in gallons per minutes:

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 03 - TURBINE ENGINE FUEL SUBSTITUTIONS

Nozzle Spout Diameter 2-1/2 inches 2-inches 1-1/2 inches

Maximum Flow Rate Per Nozzle 46 GPM 29 GPM 17 GPM

b. It is imperative that fuel not be allowed to "waterfall" into the tank. A nozzle spout long enough to reach the bottom of the tank must be used. 5. Placards a. Two placards are required for all aircraft. b. Placards will be worded as follows: "Fueled with JP-4/Jet B at TAT____ Slow fuel until TAT____". (1) The TAT when JP-4/Jet B was added will be entered in the first TAT space of the Placard. (2) The second TAT will be 20 hours after the first TAT. c. Place one Placard at Underwing Fueling Control Panel. d. Place one Placard in Flight Log. e. A carry-over item will be entered in Aircraft Log: "Fueled with JP-4/Jet B at TAT____. Remove all Slow Fuel Placards at TAT_____, or when tanks and sumps are drained". NOTE:

Placarding requirements serve as JP-4/Jet B hazard warnings for maintenance as well as for fueling operations.

f. Any time an airplane with JP-4/Jet B Placards is again fueled with JP-4 or Jet B, update the Placards and carry over item based on TAT of latest JP-4/Jet B fueling. g. After refueling exclusively with Jet A type fuels for 20 flying hours, all residual JP-4/Jet B is considered to be gone and restrictions are removed. Remove Placard from Underwing Fuel Panel, Cockpit and Log Book. Close out carry-over item in the Aircraft Logbook per the General Maintenance Manual.

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 03 - TURBINE ENGINE FUEL SUBSTITUTIONS h. Complete defueling and sump draining also allows removal of Placards and restrictions.

FUELING SITUATION Adding “Kerosene fuels” with or without antistatic additive to other Kerosene fuels. Adding “Wide-Cut fuels” to kerosene fuels if the wide-cut fuel contains antistatic additive. Adding wide-cut fuels to kerosene fuels if the wide-cut fuel does not contain antistatic additive. Adding kerosene fuels with antistatic additives to wide-cut fuels not containing antistatic additives. Adding kerosene fuels without antistatic additive to wide-cut fuels that also have antistatic additive. Adding kerosene fuels without antistatic additive to wide-cut fuels with or without antistatic additive. Adding wide-cut fuels to wide-cut fuels if both have antistatic additive. Adding wide-cut fuels to wide-cut fuels if only one or neither have antistatic additive.

NORMAL FUELING RATE

SLOW FUELING RATE

X X

X

X

X

X X X

* - Slow Fueling Rate is REQUIRED for the next 20 flight hours after last recorded fueling of JP-4/Jet B. FUELING STATION AND FUELING RATES Table 3.01-2 NOTE: For purpose of preceding Table 3.01-2: -Kerosene Fuels are Jet A, Jet A-1, JP-5 and JP-8 -Wide-cut Fuels are JP-4 and Jet B At most locations, Commercial Grade Jet A and A-1 Kerosene type fuels normally DO NOT contain antistatic additives. Military Grade JP-4 Wide Cut fuels DO normally contain antistatic additives. If in doubt, positive determination from fuel supplier must be received prior to loading to assure a safe fueling operation.

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 04 - SAFETY REQUIREMENTS TABLE OF CONTENTS 04.01 - SAFETY REQUIREMENTS 01. General Precautions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02. Bonding Instructions - All Airplanes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03. Fueling with Passengers or Employees Aboard . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 04. Precautions for the Operation of Equipment During Refueling . . . . . . . . . . . . . . . . . 05. Precautions During Inclement Weather . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 06. Photographs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 07. Fueling with an Engine Running . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 04 - SAFETY REQUIREMENTS 04.01 SAFETY REQUIREMENTS 1. General Precautions - The following procedures are standard and must be complied with. The only exception will be when there is a conflict with local airport or Port Authority regulations, in which case the local regulations will take precedence in those items where there is a conflict. a. Fire fighting equipment will be available. b. Only equipment that has been approved for use at the station will be used to fuel airplanes. c. Use of protective device when walking on wings or other metal structure: (1) It is most important that every precaution be taken when walking on aircraft wings or any other metal structure to prevent injury to the metal surface. (a) When a turbine airplane is involved it will be required without exception that a protective "sock" be pulled over the shoes before the surface is walked on. The protective socks will be furnished by local station management. If socks are not available, shoes must be removed. d. Airplane must be clear of nose docks and hangars when being fueled. e. No fueling or defueling should be done while electrical storms are within a 10 mile (16 kilometer) radius of the immediate area. f. No aircraft electrical switches shall be turned ON or OFF while refueling or defueling is being accomplished. g. Under no circumstances should battery master switch be disturbed or the outside power connection be changed during refueling operation. h. Checking of electrical equipment should not be done during refueling. i. No smoking and no fires or flames shall be permitted within 50 feet of the aircraft being serviced. WARNING:

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ALL DRAINED OR SPILLED FUEL MUST BE COLLECTED AND DISPOSED OF IN ACCORDANCE WITH EPA AND LOCAL ENVIRONMENTAL REGULATIONS. APPROVED CONTAINERS AND SPILL PADS MUST BE USED AND MUST BE DISPOSED OF IN ACCORDANCE WITH EPA AND LOCAL REGULATIONS. 07-14-08

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 04 - SAFETY REQUIREMENTS 2. Bonding Instructions - All Airplanes. Use these bonding procedures when servicing airplane from fuel truck or hydrant truck: a. After positioning truck, unreel sufficient bond cable to enable bonding connector to be firmly attached to aircraft. Next, connect bond wire connector to airplane ground plug. b. Whenever fuel is added through the overwing filler openings the bond wire on the nozzle must be connected to the special fixture on the airplane before the fuel tank cap covers are opened and must be left connected until these covers are again closed on the tank being fueled. 3. Fueling with Passengers or Employees Aboard a. Fueling may be accomplished with passengers or employees on board. (1) During fueling, a passenger exit must be available by providing a passenger stand, jet way, or by lowering the integral stairway. (2) If employees only are aboard, a stand or ladder must be provided at either the crew entrance or main cabin door.

b. Fueling during the period in which passengers are being deplaned or boarded: (1) Fueling of the aircraft may be accomplished during the boarding or deplaning of passengers when underwing fueling method is being used. (2) Overwing fueling will not be permitted during routine deplaning or boarding of passengers by passenger loading stand or integral stairs. (3) It is permissible to fuel the aircraft when a jet way is used. c. Minimum refuel crew for concurrent refueling shall be three persons; (1) ground supervisor using ground communication equipment, (2) one person on the fuel receptacle, and (3) the fuel truck operator. 4. Precautions for the Operation of Equipment During Refueling a. The following is a list of units and systems that must not be operated during the refueling operation: (1) Do not use heat guns and similar devices for thawing water service panels. (2) Do not operate integral heaters on de-icing units unless they are approved for use at plane side. (3) Do not use communication equipment during aircraft fuel servicing operations within 10 feet of fueling equipment or of the fill or vent points of aircraft fuel systems. 04.01.2

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 04 - SAFETY REQUIREMENTS b. Airplane Fueling Equipment (1) Airplane fueling equipment of any type will not be used to service ground equipment while the fueling equipment is connected to the airplane. (2) Do not leave fuel trucks unattended while the trucks are connected to the airplane unless the nozzle valves are closed and the truck engine is shut down and chocks are installed. (3) Do not transfer fuel from one airplane fuel truck to another while either is connected to the airplane. c. Electrical Connections. During the fueling operation, the ground power unit or airplane batteries will not be connected or disconnected. If maintenance work is to be performed during the fueling operation, it will be the responsibility of the mechanics performing such work to see that units or systems that may cause an unsafe operation are not operated. d. During fueling operations, if it becomes necessary to perform service or maintenance work on automotive or electrical equipment, such equipment will be moved a safe distance from the airplane to preclude the possibility of fire or damage to the airplane. e. The following units may be operated during fueling operation provided that all safety precautions listed here and for the operation of each unit are complied with. (1) It will be permissible to operate ground air conditioning units for the purpose of air conditioning the airplane during fueling or defueling. NOTE: The operation of Herman-Nelson unit, or portable heaters which is primarily an engine heating unit, is NOT permitted during fueling or defueling. (2) It is permissible for Diesel S & S Starter Trucks to be started or to operate during fueling or defueling. (3) The ground power unit may be left running and connected. (4) Vacuum cleaners may be operated, turned ON or OFF with the switch in the unit and extension cords connected or disconnected in the airplane. It is not permissible to connect or disconnect extension cord plugs with another cord, an external power supply, or an outlet outside of the airplane without checking first to see that the vacuum cleaner switch is in the OFF position.

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 04 - SAFETY REQUIREMENTS 5. Precautions During Inclement Weather a. During inclement weather when metal surfaces become wet and slippery, or whenever wind velocity is over 25 miles per hour, extreme care and good judgment must be exercised when overwing fueling is being accomplished. CAUTION:

THE MOVEMENT OF WINGS CAUSED BY STRONG GUSTS OF WIND MAY REQUIRE ADDITIONAL PRECAUTIONS TO PREVENT INJURY TO PERSONNEL OR DAMAGE TO AIRPLANE BY GROUND EQUIPMENT.

b. It is required to suspend fueling operations when severe electrical storms exist in the immediate vicinity. 6. Photographs a. Before allowing flash bulb pictures to be taken around airplanes, the employee contacted by the photographer will check with a Ground Services Ramp or Aircraft Maintenance Supervisor. The Supervisor will allow the use of flash bulbs only if no airplane is being refueled or is having its radar checked within 50 feet. Electronic flash equipment will be allowed at all times in all places except directly under a wing while refueling is being accomplished on that wing. The Supervisor permitting flash bulb photography around airplanes is responsible for monitoring the activities of the photographer to assure that these regulations are followed. (1) Electronic flash equipment can be identified by the continuous tube-like shape of the bulb with no internal foil or wires, as compared to the bulbular-shaped flash bulb which contains fine foil or wire. 7. Fueling with an Engine Running a. The following procedures apply whenever it is necessary to add fuel to an aircraft with an engine running. This procedure is only to be used to avoid a delay or a trip cancellation, or when necessary for the safety or welfare of passengers or cargo.

NOTE: When it becomes known that ground support equipment will be unavailable, every effort will be made to schedule aircraft that are self-supporting or to utilize an alternate location where ground support equipment is available.

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 04 - SAFETY REQUIREMENTS b. B767 (1) At least one pilot seat will be manned by a flight crew member. Radio contact will be maintained with tower or ground control. (2) A person will be posted forward of the operating engine to keep that area free of personnel and equipment. Whenever possible, this individual will maintain interphone contact with the cockpit. (3) The forward left entrance door must be open with stairs in place.

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 05 - BIOCIDE TREATMENT OF FUEL TANKS TABLE OF CONTENTS 05.01 - BIOCIDE TREATMENT OF AIRCRAFT FUEL TANKS 01. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 05.01.1

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 05 - BIOCIDE TREATMENT OF FUEL TANKS 05.01

BIOCIDE TREATMENT OF AIRCRAFT FUEL TANKS

1. General a. Reference Boeing B767 AMM 28-10-00 for testing, treatment, and removal of microbial growth.

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 06 - RESERVED 06.01 RESERVED FOR FUTURE USE

SECTION 02

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES TABLE OF CONTENTS 07.01 - B767 FUEL SYSTEM GENERAL 01. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 07.01.1 07.02 - FUEL LOADING REQUIREMENTS AND LIMITATIONS 01. Requirements ...............................................................................................................07.02.1 02. Limitations ...................................................................................................................07.02.1 07.03 - AUTOMATIC FUELING OPERATION 01. Prepare Fueling Station................................................................................................07.03.1 02. Begin Fueling...............................................................................................................07.03.2 07.04 - FUELING WITH ONE INOPERATIVE INDICATOR 01. Prepare to Fuel Using Cockpit Indicator or Measuring Stick......................................07.04.1 02. Begin Fueling Using Cockpit Indicator .......................................................................07.04.1 07.05 - FUELING WITH INOPERATIVE GAUGE 01. Procedure - Magnastick Method..................................................................................07.05.1 02. Procedure - Transfer Method .......................................................................................07.05.1 07.06 - MANUAL FUELING OPERATION 01. Manual Fueling Settings ..............................................................................................07.06.1 02. Begin Manual Fueling Operation ................................................................................07.06.1 07.07 - FUELING WITHOUT ELECTRICAL POWER 01. Prepare to Fuel Without Electrical Power....................................................................07.07.1 02. Begin Fueling Without Electrical Power .....................................................................07.07.2 07.08 - OVERWING FUELING 01. General.........................................................................................................................07.08.1 2. Begin Overwing Fueling..............................................................................................07.08.1 07.09 - DEFUELING AND TANK-TO-TANK TRANSFER 01. General.........................................................................................................................07.09.1 02. Defueling .....................................................................................................................07.09.1 03. Tank-to-Tank Transfer .................................................................................................07.09.2 04. Functional Description.................................................................................................07.09.2 05. Operation .....................................................................................................................07.09.3 07.10 - FUEL SUMP DRAINING 01. General.........................................................................................................................07.10.1 02. Drain Fuel Tank Sumps ...............................................................................................07.10.1 07.11 - STANDARD FUEL DISTRIBUTION 01. General.........................................................................................................................07.11.1

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES 07.01 B767 FUEL SYSTEM GENERAL 1.

General A.

The B-767 aircraft fuel system provides a means of storing fuel in the aircraft, distributing fuel to the engines, pressure refueling and defueling, and provides a fuel quantity indicating system.

B.

The fuel tanks are located in the interspar area of each wing outboard of the fuselage section. There are three fuel tanks; the left and right main tanks and the center auxiliary tank. A surge tank is located near the top of each wing. The surge tanks are designed to contain overflow and to prevent fuel spillage.

C.

The aircraft is normally fueled into the left and right main tanks, and into the center auxiliary tank when necessary, using the pressure fueling method.

D.

The pressure fueling is controlled by the Fuel Quantity Indicating System (FQIS) processor unit (automatic fueling), or by the fueling operator (manual fueling). The operator can override the processor unit at any time during the fueling procedure by operating the fueling control switches at the fueling control station.

E.

The fueling control station is located on the underside of the left wing to leading edge. The station contains pressure fueling adapters, grounding points, a reading light, an interphone jack and a control panel. The control panel contains valve switches (FUEL and DEFUEL), valve OPEN lights, power switch NORMAL or BATTERY, the LOAD SELECT indicators, LOAD SELECTOR and SET switches, and TEST switches. Aluminum placards mounted on the inner surface of the fueling station door provide fueling procedures and appropriate cautions. Opening the fueling station door applies electrical power, 28 VDC from the ground handling bus, to the panel. If the ground handling bus is not powered, the panel power switch can be moved to BATT position.

F.

If no electrical power is available, the fueling shutoff valves can be operated manually. Fuel quantity can be measured without electrical power by using the measuring sticks located in the wing’s lower skin and the dipstick calibration charts in Section 08.01.

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PRESSURE FUELING SYSTEM Figure 7.01-1

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FUELING STATION DOOR Figure 7.01-2

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES 07.02 FUEL LOADING REQUIREMENTS AND LIMITATIONS 1.

Requirements A.

Fuel must conform to jet fuel specifications listed in Section 3.01.

B.

The B-767-200 has two main wing tanks (left and right) and one integral center tank. The maximum fuel capacities shown below are based on a fuel density of 6.7 lb./gallon. Main Tanks

C.

2.

Volume - gal.

Weight - lb

Left

6,070

40,700

Right

6,070

40,700

Center

4,560

30,500

Total

l6,700

111,900

Left and right main fuel tanks must be loaded with approximately equal amounts of fuel to maintain a suitable center of gravity. Do not exceed a lateral imbalance of 1500 lbs.

Limitations A.

All B767-200 Aircraft The center tank can be loaded with any amount of fuel, provided the main tanks are scheduled to be filled to capacity. However, if the main tanks are not scheduled to be full, up to 22,050 pounds of fuel may remain in or may be loaded in the center tank, provided the Maximum Zero Fuel Weight Limit is reduced by this amount of center tank fuel. All tanks may be filled simultaneously or in any sequence.

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES WARNING:

AIRCRAFT AND FUELING SOURCE MUST BE PROPERLY BONDED BEFORE BEGINNING ANY FUELING OPERATION TO PREVENT POSSIBLE HAZARD OF ELECTRICAL DISCHARGE.

WARNING:

GROUND EQUIPMENT MUST NOT BE POSITIONED UNDER WING TIPS DURING FUELING OPERATION. WING DEFLECTION DOWNWARD UNDER THE FUEL LOAD IS GREATEST AT THE WING TIPS. FUEL TANKS ARE VENTED THROUGH THE WING TIPS, AND AN EXPLOSIVE AIR/FUEL MIXTURE CAN DEVELOP IN THIS AREA.

WARNING:

DO NOT OPERATE THE HF RADIOS OR WEATHER RADAR DURING FUELING OPERATIONS.

WARNING:

WHEN THUNDERSTORMS OR LIGHTENING ARE WITHIN A 10 MILE (16 KILOMETER) RADIUS OF THE IMMEDIATE AREA, THE REFUELING PROCEDURE SHOULD STOP.

CAUTION:

TO PREVENT DAMAGE TO FUELING SYSTEM COMPONENTS, DO NOT EXCEED 50 PSI FUEL PRESSURE AT THE FUELING NOZZLE.

CAUTION:

ATTACH BONDING CABLES ONLY TO SPECIFIED POINTS ON THE AIRPLANE. BONDING CABLES ATTACHED TO COMPOSITE DOORS OR FAIRINGS DO NOT GIVE AN ELECTRICAL BOND. INCORRECTLY ATTACHED BONDING CABLES CAN CAUSE SCRATHES. THESE SCRATHES CAN CAUSE CORROSION AND CRACKS ON STRESSED PARTS.

B.

Electrical power from the APU, external power or battery is needed to operate the panel, valves and fuel quantity indicating system. Do not switch power sources while refueling.

C.

If the EICAS message Fuel QTY IND is displayed, maintenance personnel should perform fuel quantity BITE procedure per the Aircraft Maintenance Manual. Fuel tanks may be refueled prior to performing BITE procedure using the fuel measuring sticks.

NOTE:

D.

The circuit breakers listed under the following panels must be closed during refueling: (1)

07.02.2

APU/EXT Power Panel, P34 (a)

FLNG CONTROL, L3

(b)

VALVES FLNG, L5

(c)

FUEL QTY REFUEL, L2 07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES (2)

(3)

Original

Main Power Panel, P6 (a)

FUELING CONTROL, E5

(b)

FUELING VALVES, E6

(c)

FUELING QTY, E4

Overhead Circuit Breaker Panel, P11 (a)

FUEL QTY NO. 1, C34

(b)

FUEL QTY NO. 2, M19

07-14-08

07.02.3

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES

INTENTIONAL BLANK

07.02.4

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES 07.03 AUTOMATIC FUELING OPERATION 1.

Prepare Fueling Station A.

Open fuel station door. Make sure that the panel light comes ON, indicating that 28 VDC power is present at the fueling control panel. NOTE:

B.

If panel light does not come on, place the power switch in the BATT position.

Insert fuel nozzle bonding plug into grounding jack and connect fueling nozzle(s) to either or both fueling adapters. NOTE:

Fueling adapters have two positions, FUEL and DEFUEL. It should be in the FUEL position.

C.

Test load select indicators by pressing the IND switch; 88.8 should be displayed on the upper and lower LCD displays.

D.

Test fueling valves by press-to-test indicator lights.

E.

Set thumbwheels on the load select control to desired amount of fuel for the LEFT and RIGHT main tanks. Press the SET switch for the LEFT and then the RIGHT main tanks. Hold the SET switch for a minimum of 1 second. If center auxiliary tank fuel is required, set the load select control to the desired amount and press the center auxiliary SET switch for a minimum of 1 second. NOTE:

F.

Set the fueling valve switches for the appropriate tanks to FUEL. After 4 to 5 PSI of fuel pressure have been applied to the fuel valve, the blue valve OPEN lights will illuminate, indicating that the fueling valves are open NOTE:

Original

If an error is made during the selection process, press the appropriate SET switch to clear the load select display, and repeat the above procedure.

If either fill valve in a tank is inoperative, the fueling rate for that tank will be reduced, The tank may be fueled to any quantity with either fill valve operative. Also, if necessary, an inoperative fill valve may be opened and closed manually or overwing fueling may be used.

07-14-08

07.03.1

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES 2.

Begin Fueling CAUTION:

A.

Start fueling source. NOTE:

B.

USE EXTREME CAUTION WHEN FUELING IF FUELING VALVE(S) HAS BEEN OPENED MANUALLY. NO ELECTRICAL SHUTDOWN PROTECTION EXISTS FOR MANUALLY OPENED VALVES.

The fueling quantity processor will close the fueling valves automatically when the tank quantity reaches the SET quantity. This occurs for each tank being fueled to a pre-selected SET amount.

When fueling reaches the desired quantity, stop the fueling source and return the fueling valve switches for all applicable tanks to off. NOTE:

When fueling has reached the desired quantities and the processor has closed all opened fueling valves, release the deadman switch and return the applicable fueling valve switches to OFF.

C.

Disconnect fueling nozzle(s) and bonding plug.

D.

If selected to BATT, return power switch to NORM.

E.

Close fueling station door.

07.03.2

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES 07.04 FUELING WITH ONE INOPERATIVE INDICATOR 1.

2.

Prepare to Fuel using Cockpit Indicator or Measuring Stick A.

It is permissible to use the cockpit indicator to fuel a tank with an inoperative fueling panel indicator. Automatic valve closing, except for overfill, will not be operative using this method. For this reason a qualified person, preferably a mechanic or crew member, must be in the cockpit and in interphone contact with the refueler at all times during the refueling operation. The refueler must be alert to position the fueling valve switch for the affected tank to OFF when advised by the person in the cockpit that the tank contains the desired amount of fuel.

B.

Prior to fueling a tank with an inoperative indicator, a magnastick measurement of the fuel remaining in that tank and pitch and roll must be taken (see Section 08.01). Check the stick chart to determine the amount of fuel remaining on arrival.

C.

Using the above pitch and roll, determine from the measuring stick tables which stick and the desired inches-indication the fueling personnel will use to provide the desired quantity of fuel in the affected tank.

D.

Ensure compliance with Section 07.02 and Section 07.03 paragraph 1.A. and 1.B.

E.

Test the operative load select indicator by pressing IND TEST switch; 88.8 should be displayed on upper and lower LCD displays.

F.

Press-to-test the fueling valve lights.

G.

Withdraw the measuring stick to be used on the affected tank to engage the magnet and the float.

H.

Set the load select quantity on the tank with operable indicator (see Section 07.03 paragraph 1.E.).

Begin Fueling using Cockpit Indicator A.

Open the tank valves and begin fueling. NOTE:

Tanks are fueled simultaneously until within approximately 1500 lbs of the desired level in each tank.

B.

Monitor the stick being used on the affected tank until within approximately two inches of desired indication. At that point, stop fueling. Reset the magnet and float on the measuring stick to assure proper reading.

C.

Restart the fueling source and continue fueling at reduced rate to desired quantities.

Original

07-14-08

07.04.1

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES D.

Shut down the fueling source when the required amount of fuel is loaded. Verify the stick reading and stow the stick.

E.

Close the fueling valves.

F.

Disconnect the fueling nozzle(s) and bonding plug.

G.

Close the fueling station door.

07.04.2

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES 07.05 FUELING WITH INOPERATIVE GAUGE 1. Procedure - Magnastick Method NOTE: For Magnastick tables, refer to Chapter 08 “Fuel Measuring Stick Tables for Off Attitude Conditions”. a. Obtain a magnastick reading of the fuel remaining in the tank with the inoperative gauge. Pound reading is obtained from Fueling Manual. NOTE: If quantity of fuel in tank is below magnastick level, add fuel from another tank(s) until a reading can be obtained. b. Record fuel quantity gauge reading for the other tanks. c. Prior to separate fueling of the tank with the inoperative gauge, determine the number of gallons to be added to that tank. Subtract "Before" figure from "Desired" and convert this number to gallons using stations actual density. NOTE: Prior to separate fueling, note gallon reading on the fuel vehicle meter or reset to zero. d. Fuel the tank having the inoperative gauge to the gallons calculated for the tank. e. Fuel the remaining tanks to the "Desired" quantities. f. Magnastick the tank having the inoperative gauge. 2. Procedures-Transfer Method a. Empty tanks having inoperative gauge. Use tank-to-tank transfer or pump into external container. Empty condition is indicated by (1) SHUTOFF CLOSED light illuminates. (2) FUEL PRESS gauge drops. (3) Gauge on receiving tank stops increasing. b. Enter fuel quantity gauge reading for all tanks. The sum of these amounts is "Total pre-service fuel." c. Record "Desired" fuel amounts and "Desired" magnastick reading and location. Complete "Fuel to be added" computations.

Original

07-14-08

07.05.1

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES d. Fuel tank having inoperative gauge by transferring from another tank or by filling from fueling vehicle, using its meter. NOTE: Prior to separate fueling from fueling vehicle record desired pounds to be added. Using stations actual density, divide density by pounds to be added to obtain gallons required from fueling vehicle. CAUTION:

FUEL QUANTITY GAUGES MUST BE CLOSELY MONITORED DURING ENTIRE FUELING OPERATION TO DETECT FAULTY GAUGE(S) (I.E., GAUGE LAGS OR COMPLETELY STOPS) WHICH COULD CAUSE A FUEL SPILL.

e. Fuel remaining tanks to desired gauge amounts. f. Check magnastick reading for tank having inoperative gauge. Fuel load must be stickable for tank with inoperative gauge.

07.05.2

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES 07.06 MANUAL FUELING OPERATION 1.

2.

Manual Fueling Settings A.

Ensure compliance with Section 07.02 and Section 07.03 paragraph 1.A. through 1.D.

B.

Place the applicable fueling valve switches to FUEL.

Begin Manual Fueling Operation A.

Start the fuel source.

B.

Monitor fuel quantity indicators for the amount of fuel in the tanks. Stop the fueling source and return applicable fueling valve switches to OFF when the desired fuel quantity has been reached. Verify that the blue fueling valve lights go out.

C.

Shut down the fueling source.

D.

Disconnect the fueling nozzle(s) and bonding plug.

E.

If selected to BATT, return the power switch to NORM.

F.

Close the fueling station door.

Original

07-14-08

07.06.1

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES

INTENTIONAL BLANK

07.06.2

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES 07.07 FUELING WITHOUT ELECTRICAL POWER 1.

Prepare to Fuel Without Electrical Power CAUTION:

NO AUTOMATIC SHUTDOWN OR OVERFILL PROTECTION EXISTS WITHOUT ELECTRICAL POWER.

CAUTION:

DO NOT USE MANUAL SHUTOFF VALVES TO REDUCE OR STOP FUELING. CLOSING THE MANUAL SHUTOFF VALVES DURING FUELING CAN CAUSE PRESSURE SURGES AND DAMAGE EQUIPMENT.

A.

Gain access to the main tank fueling valves by removing applicable access panels aft of the wing trailing edge spar (see Figure 1). (1)

Main tank inboard actuator, left wing, 551 TB.

(2)

Main tank inboard actuator, right wing, 651 TB.

(3)

Main tank outboard actuator, left wing, 561 GB.

(4)

Main tank outboard actuator, right wing, 661 GB.

B.

Gain access to the left or right center auxiliary fuel tank fueling valves.

C.

Manually open applicable shutoff valve, (see Figure 7.07-1): CAUTION:

(1)

Verify that the fueling manifold has been depressurized.

CAUTION:

D.

Original

MAKE SURE THERE IS NO MANIFOLD PRESSURE. DAMAGE COULD RESULT TO THE DIAPHRAM ON THE FUELING VALVE.

DO NOT REMOVE RETAINER PLATE LOCKWIRE, SCREWS OR RETAINER PLATE, FUEL LEAKAGE WILL OCCUR.

(2)

Remove the lockwire from knurled knob on the valve override screw.

(3)

Turn the override screw (knurled knob) 10-13 complete revolutions in a counterclockwise direction.

Ensure compliance with the warnings and cautions found in Section 07.02.

07-14-08

07.07.1

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES 2.

Begin Fueling Without Electrical Power A.

Open the fueling station door.

B.

Insert fuel nozzle bonding plug into grounding jack and connect the fueling nozzle(s) to fueling adapters.

CAUTION:

DO NOT EXCEED 50 PSI FUEL PRESSURE AT FUELING NOZZLE TO PREVENT DAMAGE TO FUELING SYSTEM COMPONENTS.

C.

Start the fueling source.

D.

Monitor fuel quantity in tanks with fuel quantity measuring sticks (see Stick Tables, Section 08.01).

E.

Shut down fueling source when required amount of fuel is loaded.

F.

Manually close applicable shutoff valve: (1)

Verify fueling manifold has been depressurized.

(2)

Turn the override screw 10-13 complete revolutions in clockwise direction.

(3)

Install lockwire to knurled knob or valve override screw.

G.

Disconnect fueling nozzle(s) and bonding plug.

H.

Close fueling station door.

I.

Install applicable wing access panels.

07.07.2

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES

A B

BOTTOM VIEW (LEFT WING) (TYP)

B

MAIN OUTBD FUEL SOV ACCESS PANEL 561GB, 661GB

A MAIN INBD FUEL SOV ACCESS PANEL 551TB, 651TB

DRY SIDE

AFT SPAR

MANUAL OVERRIDE THUMBSCREW KNURLED KNOB

ATTACH SCREWS

COVERPLATE FOR MANUAL OVERRIDE THUMBSCREW

COVERPLATE

C MANUAL OVERRIDE THUMBSCREW

C

FUELING SHUTOFF VALVE (SOV) (TYP)

FIGURE 1 MANUAL FUELING SHUTOFF VALVE (SOV)

MANUAL FUELING SHUTOFF VALVE (SOV) Figure 7.07-1 Original

07-14-08

07.07.3

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES

INTENTIONAL BLANK

07.07.4

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES 07.08 OVERWING FUELING 1.

Overwing Fueling - General A.

Overwing fueling of the left and right main tanks may be performed if pressure fueling equipment or electrical power is not available and is required when the outboard main tank is inoperative. With electrical power available fuel quantity can be monitored by load select indicators at the fueling station. With no electrical power available fuel quantity can be monitored with fuel quantity measuring sticks (see Section 08.01). NOTE:

B.

Ensure compliance with Section 07.02.

C.

Provide electrical power if available. If electrical power is not available, release and lower the applicable fuel measuring sticks.

D.

If available, place maintenance mats on wing where service personnel must walk.

WARNING:

E. 2.

Overwing fueling port directs fuel into the outboard section of the main fuel tanks.

DO NOT REMOVE FILLER CAPS BEFORE GROUNDING FUEL NOZZLES.

Bond fueling nozzles to ground jacks adjacent to fill ports with nozzle bonding cables.

Begin Overwing Fueling A.

Remove filler caps from main fuel tanks.

B.

Insert fueling nozzles into filler ports.

CAUTION:

DO NOT EXEED FUELING RATE OF 155 GPM.

C.

Start fueling source. Monitor fuel quantities loaded with load select indicators, or fuel measuring sticks as applicable.

D.

Stop fueling source when required amount of fuel is loaded.

E.

Remove fuel nozzle and install filler cap.

Original

07-14-08

07.08.1

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES F.

Disconnect bonding cable from ground jacks.

G.

Remove maintenance mats, if used.

H.

If opened, raise applicable fuel measuring sticks into stowed position and lock.

I.

If opened, close fueling station door.

OVERWING FUELING Figure 7.08-1

07.08.2

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES 07.09 DEFUELING AND TANK-TO-TANK TRANSFER 1.

General A.

Defueling is accomplished by using either the pressure or suction method. Fuel extraction is through the fueling adapters at the wing fueling station. Tank-to-tank transfer is accomplished using the pressure method. Both operations are accomplished only on the ground. There are no provisions for tank-to-tank transfer in flight.

B.

Tank valves for fueling and defueling are controlled from the fueling station and must be properly positioned to accomplish either of the above operations. The fueling adapter must be set to DEFUEL prior to attaching the vehicle hose to remove fuel from the aircraft.

WARNING:

DO NOT OPERATE THE HF RADIOS OR WEATHER RADAR DURING DEFUELING OPERATONS.

CAUTION:

DO NOT OPERATE HYDRAULIC SYSTEM IF FUEL IN EITHER TANK IS LESS THAN 600 U.S. GALLONS. HYDRAULIC SYSTEM OVERHEATING WILL RESULT IF THE HEAT EXCHANGER IS NOT SUBMERGED IN FUEL.

C.

The following procedures must be followed when ground transferring or defueling center tank fuel on airplanes with the center tank deactivated. (Ref. AD 2001-15-08 and AMM 28-26-00.) (1)

2.

Use scavenge system to defuel center tank below 1000 lbs. Use of the override pumps with less than 1000 lbs of fuel is prohibited.

Defueling A.

Main tank pressure defueling requires opening the Left or Right Defuel Valve and turning on the boost pump(s) in the tank. Center Aux pressure defueling require opening either or both main tank defuel valves and turning on the override pumps. Center Aux pressure defueling is not available with deactivated Aux tanks. NOTE:

Original

The Center Aux tank defueling valve, if installed, is used for suction defueling only. DO NOT OPEN Center Aux tank defuel valve for pressure defueling.

07-14-08

07.09.1

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES B.

3.

Suction defueling requires opening the applicable tank defuel valve (Left, Center Aux, Right) and applying vehicle suction to the fueling manifold. A boost pump bypass suction line connects each fuel tank to the fuel feed manifold. Boost pumps are not used.

Tank-To-Tank Fuel Transfer Transferring fuel to another fuel tank requires opening the receiving tank fueling valves, opening the supply tank fueling valves and turning on the boost pumps in the supply tank. When transferring out of the Center Aux tank, do not open the Center Aux Defuel Valve. Open both Main Tank Defuel Valves (or the opposite tank to which transfer is being made) and the Crossfeed valve. NOTE: Transferring fuel is the same as pressure defueling, EXCEPT fueling adapter is not set to DEFUEL position and fuel is not removed from aircraft.

4.

Functional Description A.

Defueling (1)

07.09.2

Pressure Defueling - For pressure defueling, the fuel system must be configured as follows: (a)

The fueling adapters must be in the defuel mode before connecting the fueling nozzles

(b)

The defueling valve for the tank being defueled must be open. (Center Aux Defueling Valve if installed is not required to be open for pressure defueling)

(c)

At least one boost pump for the tank being defueled must be on.

(2)

Suction Defueling - Suction defueling requires a configuration of the fuel system similar to pressure defueling, except that the boost pumps for the tank being defueled must be off, and Center Aux Defuel Valve opened for suction defueling.

(3)

Tank-To-Tank Fuel Transfer - For transfer of fuel between tanks, the fuel system must be configured as follows: (a)

The receiving tank pressure fueling shutoff valves must be open.

(b)

A main tank defueling valve must be open.

(c)

At least one supplier tank boost pump must be operating.

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES

B.

C.

(4)

If the defuel valve for the main tank being defueled (any method) fails closed and cannot be manually opened, opening the crossfeed valve and the opposite tank defueling valve still allows defueling. Suction defueling of Center Aux tank requires an operable defuel valve.

(5)

The fuel quantity indicating system allows monitoring of defueling.

Defuel Valve Operation (1)

Switches at the fueling station control the defueling valves. The ground handling bus or the hot battery bus provides 28 VDC power. Opening the fueling control panel door energizes the fueling power control relay. Twentyeight-volt DC power passes through the fueling power control relay to the defuel valve control switch. If the control switch is selected to OPEN, 28 VDC power passes through the control switch to energize the defuel valve control relay. The valve actuator receives 28 VDC power through the defuel valve control relay to open the valve.

(2)

The defuel valve control relay relaxes with the defuel valve control switch closed. The relaxed valve control relay provides a direct path for 28 VDC power to the valve actuator to close the valve. Inadvertently closing the fueling panel door before switching the defuel valve CLOSED creates the necessary condition for the direct flow of 28 VDC power to the valve actuator to close the valve.

Defuel Valve Indication A blue DEFUEL VALVE light on the fueling station control panel provides indication of defue1 valve position. THE DEFUEL VALVE lamp lights when the valve reaches full open. The full closed valve shuts off the DEFUEL VALVE light.

5.

Operation A.

Provide electrical power.

B.

Pressure Defueling (1)

The following circuit breakers must be closed for defueling: Circuit Breaker

Location

DEFUELING VALVES DEFUELING VALVES FUEL QTY No. 1 FUEL QTY No. 2 Original

07-14-08

P6 P34 P11 P11 07.09.3

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES Circuit Breaker

Location

FUEL PUMP L FWD/R AFT FUEL PUMP R FWD/L AFT R AFT FUEL BOOST PUMP R FWD FUEL BOOST PUMP L AFT FUEL BOOST PUMP L FWD FUEL BOOST PUMP (2)

Open fuel station door and check that panel light illuminates. This indicates presence of 28 VDC.

(3)

Set fueling adapters to DEFUEL.

(4)

Insert fuel nozzle bonding plug into grounding jack and connect fueling nozzle(s) to either or both fueling adapters.

(5)

Select the power source by using the power select switch located on the fueling panel.

(6)

Test load select indicators by pressing TEST IND switch; 88.8 should appear on upper and lower LCD display.

(7)

Test defueling valve by press-to-test indicator light.

(8)

Set defueling valve switches to OPEN. The blue valve open indicator light should illuminate. NOTE:

CAUTION:

07.09.4

P11 P11 P6 P6 P6 P6

The Center Aux tank defueling valve, if installed, is used for suction defueling. DO NOT OPEN Center Aux tank defueling valve for pressure defueling. IF PRESSURE DEFUELING CENTER TANK, FOLLOW CENTER TANK GROUND DEFUEL/TRANSFER PROCEDURES, PAR. 1.C. OF THIS SECTION.

(9)

Place applicable boost pump switch on pilot’s overhead panel to ON. Defueling will commence.

(10)

Watch load select indicators at fueling station for amount of fuel in tanks

(11)

Place applicable boost pump switch to OFF when required amount of fuel has been unloaded. The defueling operation can be stopped at any time by placing the defueling valve switch to CLOSE. 07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES

C.

(12)

Set defueling valve switches to CLOSE.

(13)

Disconnect fueling nozzle(s) and bonding plug.

(14)

Set fueling adapter to FUEL.

(15)

Close fueling station door.

(16)

If tank has to be completely defueled, drain remaining fuel through sump drain valve.

Suction Defueling (1)

Original

The following circuit breakers must be closed: DEFUELING VALVES

FUEL QTY NO. 1

DEFUELING VALVES

FUEL QTY NO. 2

(2)

Open fuel station door and check that panel light illuminates, indicating presence of 28 VDC.

(3)

Set fueling adapters to DEFUEL.

(4)

Insert fuel nozzle bonding plug into grounding jack and connect fueling nozzle(s) to either or both fueling adapters.

(5)

Select the power source by using the power select switch located on the fuel panel.

(6)

Test load select indicators by pressing TEST IND switch; 88.8 should appear on upper and lower LCD display.

(7)

Test defueling valve by press-to-test indicator light.

(8)

Set defueling valve switches to OPEN. The blue valve open indicator light should illuminate.

(9)

Start defueling truck. Defueling will commence.

(10)

Watch load select indicators at fueling station for amount of fuel in tanks.

(11)

Place defueling valve switch at fueling station in CLOSE position when required amount of fuel is unloaded. 07-14-08

07.09.5

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES

D.

(12)

Stop defueling truck.

(13)

Disconnect fueling nozzle(s) and bonding plug.

(14)

Set fueling adapter to FUEL.

(15)

Close fueling station door.

(16)

If tank has to be completely defueled, drain remaining fuel through sump drain valve.

Tank-To-Tank Transfer (1)

Provide electrical power.

(2)

The following circuit breakers must be closed: Circuit Breaker

07.09.6

Location

DEFUELING VALVES

P6

DEPUELING VALVES FUEL QTY NO. 1 PUEL QTY NO. 2 FUEL PUMP L FWD/R AFT FUEL PUMP R FWD/L AFT R AFT FUEL BOOST PUMP R FWD FUEL BOOST PUMP L AFT FUEL BOOST PUMP L FWD FUEL BOOST PUMP FUELING VALVES FUELING CONTROL FUELING VALVES FUELING CONTROL R OVRD FUEL BOOST PUMP L OVRD FUEL BOOST PUMP R OVRD FUEL BOOST PUMP L OVRD FUEL BOOST PUMP

P34 P11 P11 P11 P11 P6 P6 P6 P6 P34 P34 P6 P6 P11 P11 P6 P6

(3)

Open fuel station door.

(4)

Select power source at power select switch at fueling panel. 07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES (5)

Test load select indicators by pressing TEST IND switch; 88.8 should appear on upper and lower LCD displays.

(6)

Test fueling valve at press-to-test indicator light.

(7)

Test defueling valve by press-to-test indicator light.

(8)

Place fueling valve switch of receiving tank to FUEL.

CAUTION:

Original

IF TRANSFERRING FUEL FROM CENTER TANK, FOLLOW CENTER TANK GROUND DEFUEL/TRANSFER PROCEDURE, PAR. 1.C. OF THIS SECTION.

(9)

Place defueling valve switch of supplier tank to OPEN.

(10)

Place applicable boost pump switch on pilot’s overhead panel to ON. Transfer will commence.

(11)

Watch load select indicator for amount of fuel in tanks.

(12)

Place applicable boost pump switch to OFF when desired amount of fuel has been transferred.

(13)

Place refueling valve switch at fueling station to CLOSE.

(14)

Place fueling valve switch at fueling station to OFF.

(15)

If tank has to be completely defueled, drain remaining fuel through sump drain valve.

(16)

Close fuel station door.

(17)

Remove electrical power if no longer required.

07-14-08

07.09.7

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES

INTENTIONAL BLANK

07.09.8

07-14-08

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES 07.10 FUEL SUMP DRAINING 1.

2.

General A.

The fuel tanks are equipped with an integral water scavenging system which operates whenever fuel boost pumps are operating. Also, each fuel tank sump has a drain valve to enable water to be drained from the tank. The sumps may be drained before or after fueling, but not during fueling. Water suspended in fuel settles at the rate of one foot per hour, and the maximum practical period of time should be allowed between fueling and sump draining to allow the water to settle.

B.

Periodic draining of fuel tank sumps is essential for removal of free water from fuel tanks, and as a check on the integrity of the water scavenge system. Abnormal amounts of water drained from an individual tank prior to fueling may indicate a blocked ejector pump, which requires removal and inspection for orifice contamination.

C.

Maintenance personnel drain all fuel tank sumps as specified in the maintenance program.

Drain Fuel Tank Sumps A.

Unlock drain valve by rotating primary poppet 90 degrees with flat-blade screwdriver.

B.

Position fuel sampling equipment beneath sump drain valve with probe against primary poppet. Push upward against poppet until fuel flows into container.

C.

Drain each sump until fuel entering container is free of water (recommended minimum of approximately one quart).

D.

Release upward pressure on poppet and allow valve to close without leakage.

E.

Lock drain valve by rotating primary poppet 90 degrees.

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07.10.1

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES

FUEL SYSTEM DRAINS Figure 7.10-1

07.10.2

07-14-08

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES 07.11

STANDARD FUEL DISTRIBUTION

1.

General A.

Fuel left and right main tanks equally to required amount or until full.

B.

Fuel center auxiliary tank if additional fuel is required with both left and right main tanks full.

C.

All fuel weights given in this B-767 Fueling Procedures Manual are based on 6.7 pounds per U.S. Gallon.

D.

The fuel chart on the following pages is shown in tabular form in increasing levels of 1000-pound increments.

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07.11.1

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES . Table 1: ADJUSTED WEIGHTS - FUEL DISTRIBUTION Total Fuel On Board LBS

ADJ. WT.

L/R Mains Each

GALS

LBS

Center Aux

GALS

LBS

GALS

1000 2000 3000 4000 5000

999.9 1999.9 2999.8 3999.7 4999.6

149 299 448 597 746

500 1000 1500 2000 2500

75 149 224 299 373

0 0 0 0 0

0 0 0 0 0

6000 7000 8000 9000 10000

5999.6 6999.5 7999.5 8999.4 9999.3

896 1045 1194 1343 1493

3000 3500 4000 4500 5000

448 522 597 672 746

0 0 0 0 0

0 0 0 0 0

11000 12000 13000 14000 15000

10999.3 11999.2 12999.2 13999.1 14999.1

1642 1791 1940 2090 2239

5500 6000 6500 7000 7500

821 896 970 1045 1119

0 0 0 0 0

0 0 0 0 0

16000 17000 18000 19000 20000

15999.0 16999.0 17999.0 18998.9 19998.9

2388 2537 2687 2836 2985

8000 8500 9000 9500 10000

1194 1269 1343 1418 1493

0 0 0 0 0

0 0 0 0 0

21000 22000 23000 24000 25000

20998.9 21998.8 22998.8 23998.8 24998.8

3134 3284 3434 3582 3731

10500 11000 11500 12000 12500

1567 1642 1716 1791 1866

0 0 0 0 0

0 0 0 0 0

26000 27000 28000 29000 30000

25998.7 26998.7 27998.7 28998.7 29998.7

3881 4030 4179 4328 4478

13000 13500 14000 14500 15000

1940 2015 2090 2164 2239

0 0 0 0 0

0 0 0 0 0

07.11.2

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES Table 1: ADJUSTED WEIGHTS - FUEL DISTRIBUTION Total Fuel On Board LBS

ADJ. WT.

L/R Mains Each

GALS

LBS

Center Aux

GALS

LBS

GALS

31000 32000 33000 34000 35000

30998.7 31998.7 32998.6 33998.6 34998.6

4627 4776 4925 5075 5224

15500 16000 16500 17000 17500

2313 2388 2463 2537 2612

0 0 0 0 0

0 0 0 0 0

36000 37000 38000 39000 40000

35998.6 36998.6 37998.6 38998.6 39998.6

5373 5522 5672 5821 5970

18000 18500 19000 19500 20000

2687 2761 2836 2910 2985

0 0 0 0 0

0 0 0 0 0

41000 42000 43000 44000 45000

40998.6 41998.7 42998.7 43998.7 44998.8

6119 6269 6418 6567 6716

20500 21000 21500 22000 22500

3060 3134 3209 3284 3358

0 0 0 0 0

0 0 0 0 0

46000 47000 48000 49000 50000

45998.8 46998.9 47998.9 48999.0 49999.9

6866 7015 7164 7313 7463

23000 23500 24000 24500 25000

3433 3507 3582 3657 3731

0 0 0 0 0

0 0 0 0 0

51000 52000 53000 54000 55000

50999.2 51999.2 52999.3 53999.4 54999.5

7612 7761 7910 8060 8209

25500 26000 26500 27000 27500

3806 3881 3955 4030 4105

0 0 0 0 0

0 0 0 0 0

56000 57000 58000 59000 60000

55999.6 56999.7 57999.8 58999.9 60000.1

8358 8508 8657 8806 8955

28000 28500 29000 29500 30000

4179 4254 4328 4403 4478

0 0 0 0 0

0 0 0 0 0

61000 62000 63000 64000 65000

61000.2 62000.4 63000.5 64000.7 65000.9

9105 9254 9403 9552 9702

30500 31000 31500 32000 32500

4552 4627 4702 4776 4851

0 0 0 0 0

0 0 0 0 0

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07.11.3

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES Table 1: ADJUSTED WEIGHTS - FUEL DISTRIBUTION Total Fuel On Board LBS

ADJ. WT.

L/R Mains Each

GALS

LBS

Center Aux

GALS

LBS

GALS

66000 67000 68000 69000 70000

66001.0 67001.2 68001.4 69001.6 70001.7

9851 10000 10149 10299 10448

33000 33500 34000 34500 35000

4925 5000 5075 5149 5224

0 0 0 0 0

0 0 0 0 0

71000 72000 73000 74000 75000

71002.0 72002.2 73002.5 74002.7 75003.6

10597 10746 10896 11045 11194

35000 36000 36500 37000 37500

5299 5373 5448 5522 5597

0 0 0 0 0

0 0 0 0 0

76000 77000 78000 79000 80000

76003.2 77003.6 78003.9 79004.2 80004.7

11343 11493 11642 11791 11940

38000 38500 39000 39500 40000

5672 5746 5821 5896 5970

0 0 0 0 0

0 0 0 0 0

81000 81200

81004.9 81205.0

12090 12120

40500 40600

6045 6060

0 0

0 0

82000 83000 84000 85000 86000

82005.0 83004.9 84004.7 85004.6 86004.5

12239 12388 12537 12687 12836

40600 40600 40600 40600 40600

6060 6060 6060 6060 6060

800 1800 2800 3800 4800

119 268 417 567 716

87000 88000 89000 90000 91000

87004.4 88004.2 89004.1 90003.9 91003.7

12985 13134 13284 13433 13582

40600 40600 40600 40600 40600

6060 6060 6060 6060 6060

5800 6800 7800 8800 9800

865 1014 1164 1313 1462

92000 93000 94000

92003.7 93003.5 94003.4

13731 13881 14030

40600 40600 40600

6060 6060 6060

10800 11800 12800

1611 1761 1910

95000 96000 97000 98000 99000

95003.2 96003.1 97003.0 98002.7 99002.7

14179 14328 14478 14627 14776

40600 40600 40600 40600 40600

6060 6060 6060 6060 6060

13800 14800 15800 16800 17800

2059 2208 2358 2507 2656

07.11.4

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES Table 1: ADJUSTED WEIGHTS - FUEL DISTRIBUTION Total Fuel On Board LBS

ADJ. WT.

L/R Mains Each

GALS

LBS

Center Aux

GALS

LBS

GALS

100000 101000 102000 103000 104000

100002.6 101002.2 102002.2 103002.1 104001.9

14925 15075 15224 15373 15522

40600 40600 40600 40600 40600

6060 6060 6060 6060 6060

18800 19800 20800 21800 22800

2805 2955 3104 3253 3402

105000 106000 107000 108000 109000

105001.7 106001.7 107001.5 108001.4 109001.2

15672 15821 15970 16119 16269

40600 40600 40600 40600 40600

6060 6060 6060 6060 6060

23800 24800 25800 26800 27800

3552 3701 3850 4999 4149

110000 111000 112000 113000 114000

110001.1 111001.0 112000.7 113000.7 114000.6

16418 16567 16716 16866 17015

40600 40600 40600 40600 40600

6060 6060 6060 6060 6060

28800 29800 30800 31800 32800

4298 4447 4596 4746 4895

115000 116000 117000 118000 119000

115000.4 116000.2 117000.1 118000.0 118999.9

17164 17313 17463 17612 17761

40600 40600 40600 40600 40600

6060 6060 6060 6060 6060

33800 34800 35800 36800 37800

5044 5193 5343 5492 5641

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07.11.5

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 07 - B767 FUELING PROCEDURES

INTENTIONAL BLANK

07.11.6

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES TABLE OF CONTENTS 08.01 - FUEL MEASURING STICK TABLES FOR OFF-ATTITUDE CONDITIONS 01. General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 02. Airplane Attitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 03. Fuel Level Measurement . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 04. Description of Tables . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 05. Example . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

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08.01.1 08.01.1 08.01.2 08.01.2 08.01.3

08-i

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

INTENTIONAL BLANK

08-ii

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES 08.01 FUEL MEASURING STICK TABLES FOR OFF-ATTITUDE CONDITIONS (INCHES TO POUNDS) 1.

2.

General A.

The B-767 airplanes are equipped with magnetic type dripless fuel measuring sticks. Seven sticks are installed in each wing's main fuel tank and one in each side of the center auxiliary tank. They are referred to as "FUEL MEASURING STICK NUMBER 1" for the auxiliary tank and "FUEL MEASURING STICK NUMBER 2" through "FUEL MEASURING STICK NUMBER 8" in the main tanks from inboard on the wing to the farthest outboard, respectively.

B.

A qualified person, either the ATI Flight Crew or Ground/Maintenance Representative, will take stick readings of the tanks. These stick readings will then be entered on the Fuel Loading Sheet along with the stick position, as applicable (left, center, right, etc.).

C.

This section provides adequate information to determine fuel tank load by using measurements from the sticks and a measurement of airplane attitude.

Airplane Attitude A.

The airplane attitude must be known in addition to the fuel depth to determine the fuel quantity in any tank. Provisions for hanging a plumb bob and a fold down scale graduated from -6° to +4° pitch and -3° to +3° roll are mounted in the left wheel well of each airplane (see Figure 8.01-1).

B.

Also provided are two bubble type inclinometers, one mounted along the aircraft centerline to determine pitch, and another mounted laterally to determine roll (see Figure 8.01-2). The plumb bob provides the most accurate measurement of airplane pitch and roll.

C.

It should be noted that the method used in the tables is: positive roll is wing high, either right or left. When roll is positive for one wing, it is negative for the other.

D.

For example, if the plumb bob indicates 1° nose high and 2° left wing down, then fuel load in the left wing would be found on a page labeled "Pitch = 1.00 Degrees" and in the column labeled "-2.00". Fuel load in the right tank would be found on the same page in the column labeled "2.00".

Original

07-14-08

08.01.1

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES 3.

4.

Fuel Level Measurement A.

The fuel measuring stick consists of a float assembly, a stick housing, and the measuring stick graduated in inches. A cutaway of the fuel level measuring stick is shown on Figure 8.01-3. The float assembly, which always remains on the fuel surface, contains a magnet. The measuring stick contains a steel armature close to its top end and the stick is free to slide up and down inside the housing. When the armature engages the magnetic field of the float, the float will hold the stick suspended from its top end. Some length of stick, depending on fuel depth in the tank, will extend through the bottom of the tank. The stick is graduated in inches and gives a visual indication of fuel depth in the tank using the bottom surface of the tank as a measuring point.

B.

The measurable range of each stick is given in Figure 8.01-6. The “minimum reading” indicates the point at which the float comes to rest on the mounting hardware at the base of the stick housing. However, the measuring stick itself is not marked below 3.00 inches. The “maximum reading” is the point at which the float comes in contact with the float stop at the top end of the stick housing. The tables, as well as Figure 8.01-7, are based on a more limited range, from 3.0 in. as a minimum, to slightly less than that shown in Figure 8.01-6. This is to ensure meaningful measurements of the fuel level and to prevent the internal structure of the tank from interfering with the float.

C.

The measuring sticks are installed through the lower surface of the fuel tank at 16 different locations. Figure 8.01-4 shows basic mounting hardware and locations.

D.

The stick is unlocked from its base by pressing lightly and turning 90 degrees counterclockwise. It must be lowered through the magnet and then raised slowly on the fingertip or palm until it is captured by the float magnet. Once the stick is captured by the magnet, read it without touching. The stick is then read in line with the lower edge of its socket (see Figure 8.01-3).

E.

The whole procedure should be repeated a few times to verify the final reading. The stick is replaced by returning it into the housing, pushing and turning the base clockwise until it becomes locked in place.

F.

Figure 8.01-7 gives a listing of the usable range in pounds at nominal attitude (0o pitch & roll) for each of the eight sticks on each side of the airplane.

Description Of Tables A.

08.01.2

The tables making up the main body of this document give fuel load in pounds versus fuel depth in inches for each stick on the airplane. The tables were made by using a computer to mathematically simulate the fuel tanks and their contents at various airplane attitudes. The results are a determination of fuel depth at each fuel measuring stick and the corresponding fuel volume in the tank. The volume is converted to load in pounds by assuming it weighs 6.7 lbs/gallon. 07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES B.

5.

The tables cover the range of attitudes with the airplane parked on the ground from -2o to +2o of pitch in .5o intervals, and -2o to +2o of roll in .5o intervals. The results of the computer simulation were checked using calibration data and different computer calculations. Figure 8.01-5 shows a sample page of the tables (this figure will also be used in the following example).

Example A.

It has been decided that the total fuel load should be 53,600 lbs. and that measuring sticks must be used to measure tank fuel quantities. A recommended procedure is shown in the following series of steps. (1)

Determine the airplane attitude. (a)

This is done by climbing into the left wheel well and using plumb-bob and the fold-down scale to measure and record a reading of pitch and roll in degrees, using the inclinometers as a check. Attitude was found to be: Pitch = 1.0o nose down Roll = 1.5o left wing down NOTE:

(2)

Even when using the plumb-bob the airplane attitude reading is only accurate to within .5o.

Determine quantity of fuel to load into each tank. The certified usable volume of each main tank is 6070 U.S. gallons, so at 6.7 lb/gal, the maximum amount of fuel that can be loaded into each main tank is 40,670 pounds. If the total fuel load is less than two times that number (or 81,340 pounds), all the fuel can be loaded into the two mains. Otherwise, the two mains would be filled to that maximum, and the remaining fuel to be loaded would be put into the auxiliary tank. In this example the total fuel to be loaded is 53,600 pounds. This is somewhat less than the maximum fuel load for the main tank, so no fuel will be loaded into the auxiliary tank. Desired fuel load (left wing main tank) = 23,800 pounds Desired fuel load (right wing main tank) = 23,800 pounds Desired fuel load (auxiliary tank) = 0 pounds

(3) Original

Determine which measuring sticks to read to verify fuel quantity. 07-14-08

08.01.3

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES (a)

This is done by using Figure 8.01-7. In Figure 8.01-7, for 26,800 lbs, the fuel measuring sticks to read are numbers 3 and 4 (in the left and right main tanks). Since Figure 8.01-7 is based on nominal attitude, some differences can occur for the actual airplane attitude, such as the fuel load going out of range for one of the indicated sticks, or into range for a stick not indicated by Figure 8.01-7.

NOTE:

(4)

Use tables to determine what the measuring stick readings will be for the desired fuel quantity. (a)

Selecting stick number 4, turn to that section of the tables, then find the pages in the stick number 4 tables for a pitch angle of -1.0o (see Figure 8.01-5).

(b)

From step (1) we know that left wing fuel quantities are listed in the column for roll equal to -1.5o. Looking down the column for the fuel quantity most closely approximating 26,800 pounds, find 26,771 pounds. Now look left under “Stick Level in Inches” to find the reading on measuring stick number 4 in the left wing that will indicate 26,771 pounds of fuel in the left main tank (7.4 inches). For the right tank, fuel quantities are listed in the column for roll equal to +1.5o on the same page. The closest quantity to 26,800 pounds here is 26,787, and measuring stick number 4 in the right wing will read 4.6 inches with that quantity of fuel in the tank. Record these readings, and then go to the other stick that can measure 26,800 pounds.

(c)

In the section of the tables for stick number 3, on the pages for pitch equal to -1.0o in the column for roll equal to -1.5o, the fuel load closest to 26,800 is 26,752. The “Stick Level In Inches” on this row shows that stick number 3 in the left wing will read 19.4 inches with 26,752 pounds of fuel in the left main tank. In the column for roll equal to +1.5o, the fuel load closest to 26,800 is 26,023 (which is the highest fuel quantity stick number 3 in the right wing can measure at this attitude), so stick number 3 in the right wing cannot be used.

(d)

To verify fuel loading: 1

Left Wing Stick Number 3 = 19.0 inches

08.01.4

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Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES Stick Number 4 = 7.4 inches 2

Right Wing Stick Number 4 = 4.6 inches

(e)

If the fuel density is given by the supplier or can be measured, the values from the tables can be corrected. 1

Assume, the density of the fuel is 6.55 lb/gallons, then since the tables are based on a density of 6.7 lbs/gal: a

Left Wing Stick Number 4 = 19.0 inches will indicate: Corrected Fuel Load = 26,749 x 6.55/6.7 = 26,150 lbs. Stick Number 3 = 7.4 inches will indicate: Corrected Fuel Load = 26,771 x 6.55/6.7 = 26,172 lbs.

b

Right Wing Stick Number 4 = 4.6 will indicate: Corrected Fuel Load = 26,787 x 6.55/6.7 = 26,187 lbs.

NOTE:

If the specific gravity of the fuel is known, then the density can be determined. Assume S.G. = .786, then, Density = S.G. x 8.33722 = .786 x 8.33722 = 6.55 lbs/ gallon.

Then, proceed as above.

Original

07-14-08

08.01.5

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

PLUMB BOB SCALE Figure 8.01-1

08.01.6

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

INCLINOMETER LOCATIONS Figure 8.01-2

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07-14-08

08.01.7

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL LEVEL MEASURING STICK Figure 8.01-3

08.01.8

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

STICK MOUNTING AND LOCATIONS Figure 8.01-4

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07-14-08

08.01.9

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK TABLE EXAMPLE Figure 8.01-5

08.01.10

07-14-08

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

MEASURING STICK’S RANGES IN INCHES Figure 8.01-6

Original

07-14-08

08.01.11

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

STICK

TANK

MINIMUM MEASURABLE LOAD

MAXIMUM MEASURABLE LOAD

1

AUXILIARY

999

29776

2

MAIN

150

19373

3

MAIN

12968

27029

4

MAIN

24138

33083

5

MAIN

30817

36676

6

MAIN

34865

38823

7

MAIN

37841

40392

8

MAIN

39530

41174

NOTE: MAXIMUM CERTIFIED USABLE VOLUME IN EACH TANK IS 6070 U.S. GALLONS (FUEL LOAD WILL BE 40670 POUNDS IF FUEL DENSITY IS 6.7 LB/GAL). MAXIMUM CERTIFIED USABLE VOLUME IN CENTER AUXILIARY TANK IS 4560 U.S. GALLONS (FUEL LOAD WILL BE 30550 POUNDS IF FUEL DENSITY IS 6.7 LB/ GAL).

MEASURING STICK’S RANGES IN POUNDS AT NOMINAL AIRPLANE ATTITUDE ASSURMING FUEL DENSITY = 6.7 LB/GAL Figure 8.01-7

08.01.12

07-14-08

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AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHES

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

411

461

519

642

844

1148

1550

2058

2605

3.2

435

486

545

670

879

1200

1619

2140

2697

3.4

459

512

572

700

915

1251

1688

2222

2788

3.6

484

539

601

731

954

1305

1758

2304

2880

3.8

510

567

631

765

995

1359

1827

2386

2972

4.0

537

597

664

802

1039

1415

1897

2467

3063

4.2

565

628

699

843

1087

1474

1967

2548

3154

4.4

594

662

737

887

1139

1535

2037

2629

3245

4.6

626

697

778

936

1197

1598

2107

2709

3335

4.8

658

736

823

990

1259

1664

2177

2788

3425

5.0

693

776

871

1049

1326

1733

2248

2867

3514

5.2

730

819

922

1111

1397

1805

2320

2946

3604

5.4

769

865

976

1177

1472

1879

2393

3026

3694

5.6

810

913

1033

1245

1549

1956

2469

3107

3784

5.8

854

964

1092

1316

1629

2036

2546

3190

3875

6.0

899

1016

1153

1389

1711

2117

2627

3275

3967

6.2

948

1071

1216

1463

1793

2201

2710

3362

4060

6.4

999

1129

1281

1538

1877

2287

2797

3452

4154

6.6

1052

1188

1348

1613

1959

2375

2888

3545

4249

6.8

1108

1250

1415

1688

2042

2464

2983

3642

4346

7.0

1167

1313

1484

1762

2123

2555

3082

3742

4445

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07-14-08

08.01.13

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHES

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

1227

1378

1553

1836

2204

2648

3184

3845

4544

7.4

1289

1444

1623

1910

2285

2742

3289

3950

4646

7.6

1351

1511

1694

1984

2366

2837

3395

4057

4748

7.8

1414

1578

1764

2059

2447

2932

3503

4166

4852

8.0

1477

1645

1835

2133

2529

3029

3612

4275

4957

8.2

15.39

1711

1906

2208

2611

3125

3721

4385

5063

8.4

1600

1777

1976

2283

2694

3222

3829

4495

5170

8.6

1660

1841

2045

2358

2778

3318

3936

4604

5278

8.8

1717

1904

2115

2434

2863

3415

4042

4713

5386

9.0

1774

1966

2183

2511

2949

3511

4146

4821

5495

9.2

1829

2028

2253

2590

3037

3608

4250

4928

5605

9.4

1885

2090

2323

2670

3127

3705

4353

5035

5715

9.6

1942

2154

2395

2752

3219

3804

4456

5142

5825

9.8

2001

2220

2469

2836

3313

3904

4559

5249

5936

10.0

2062

2288

2546

2924

3410

4005

4663

5357

6046

10.2

2126

2360

2626

3014

3510

4109

4769

5464

6156

10.4

2194

2435

2711

3109

3613

4215

4875

5572

6266

10.6

2267

2516

2799

3207

3719

4324

4984

5681

6376

10.8

2345

2601

2893

3309

3829

4435

5095

5791

6485

11.0

2428

2691

2991

3416

3941

4550

5209

5902

6594

11.2

2515

2786

3093

3525

4056

4666

5324

6014

6703

11.4

2606

2883

3198

3637

4174

4785

5441

6127

6812

08.01.14

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHES

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.6

2699

2983

3305

3752

4293

4905

5559

6241

6921

11.8

2793

3085

3413

3867

4413

5026

5679

6357

7032

12.0

2890

3189

3523

3983

4533

5148

5800

6473

7143

12.2

2986

3292

3633

4100

4654

5271

5922

6590

7256

12.4

3083

3395

3743

4216

4775

5394

6044

6709

7371

12.6

3179

3498

3851

4330

4894

5516

6167

6829

7487

12.8

3273

3598

3958

4444

5013

5638

6290

6950

7606

13.0

3366

3698

4064

4556

5130

5759

6413

7072

7726

13.2

3454

3796

4168

4667

5247

5880

6536

7195

7848

13.4

3554

3893

4272

4777

5364

6001

6659

7318

7971

13.6

3641

3990

4375

4888

5480

6122

6783

7443

8096

13.8

3731

4088

4479

4998

5596

6243

6906

7567

8221

14.0

3822

4185

4583

5109

5713

6364

7030

7692

8346

14.2

3914

4284

4688

5221

5831

6485

7153

7817

8472

14.4

4006

4383

4795

5334

5949

6607

7277

7942

8598

14.6

4100

4484

4903

5449

6069

6729

7401

8066

8723

14.8

4194

4586

5013

5566

6191

6852

7524

8190

8848

15.0

4290

4690

5125

5685

6314

6976

7648

8314

8972

15.2

4387

4796

5239

5805

6438

7101

7771

8437

9096

15.4

4486

4903

5355

5927

6563

7226

7895

8561

9220

15.6

4586

5012

5472

6049

6689

7351

8018

8684

9343

15.8

4687

5122

5590

6173

6816

7477

8142

8807

9466

Original

07-14-08

08.01.15

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHES

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.0

4790

5234

5710

6298

6943

7603

8267

8930

9589

16.2

4894

5346

5830

6424

7071

7730

8391

9054

9712

16.4

4999

5460

5951

6550

7199

7857

8516

9178

9836

16.6

5106

5575

6073

6676

7327

7984

8641

9302

9959

16.8

5214

5690

6195

6802

7455

8111

8767

9426

10083

17.0

5324

5807

6318

6928

7582

8238

8893

9551

10207

17.2

5434

5924

6441

7055

7710

8365

9019

9677

10332

17.4

5545

6042

6565

7181

7837

8492

9146

9802

10456

17.6

5656

6160

6688

7307

7965

8620

9273

9928

10581

17.8

5768

6278

6812

7434

8092

8747

9400

10054

10706

18.0

5880

6396

6936

7560

8219

8875

9527

10180

10831

18.2

5991

6514

7060

7687

8347

9002

9654

10307

10957

18.4

6102

6632

7184

7813

8474

9130

9781

10433

11082

18.6

6212

6749

7307

7940

8601

9257

9909

10559

11208

18.8

6322

6866

7431

8066

8728

9384

10036

10686

11334

19.0

6431

6983

7554

8192

8856

9512

10163

10812

11459

19.2

6539

7099

7678

8319

8983

9639

10290

10938

11585

19.4

6648

7216

7801

8445

9110

9766

10417

11065

11711

19.6

6757

7333

7925

8572

9238

9894

10543

11191

11837

19.8

6866

7450

8048

8698

9365

10021

10670

11317

11963

20.0

6977

7568

8172

8825

9492

10148

10797

11443

12088

20.2

7089

7687

8297

8951

9619

10275

10923

11569

12214

08.01.16

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHES

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

20.4

7203

7807

8422

9078

9745

10401

11050

11696

12340

20.6

7319

7928

8547

9205

9873

10528

11176

11822

12466

20.8

7437

8050

8673

9332

10000

10655

11302

11948

12592

21.0

7557

8174

8800

9459

10127

10781

11429

12074

12718

21.2

7679

8299

8927

9587

10253

10907

11555

12200

12844

21.4

7802

8424

9055

9714

10380

11034

11681

12326

12970

21.6

7927

8551

9182

9842

10506

11160

11807

12452

13096

21.8

8052

8678

9311

9969

10633

11286

11933

12578

13222

22.0

8179

8805

9439

10097

10760

11412

12059

12704

13348

22.2

8305

8933

9567

10224

10886

11538

12185

12830

13473

22.4

8431

9061

9695

10352

11013

11664

12311

12955

13599

22.6

8558

9188

9824

10480

11139

11790

12437

13081

13724

22.8

8683

9315

9952

10607

11266

11917

12563

13206

13849

23.0

8809

9442

10080

10735

11393

12043

12688

13332

13975

23.2

8933

9569

10208

10862

11519

12169

12814

13457

14100

23.4

9058

9695

10336

10990

11646

12295

12940

13583

14224

23.6

9182

9821

10463

11117

11773

12421

13066

13708

14349

23.8

9306

9947

10591

11245

11900

12547

13191

13833

14474

24.0

9430

10073

10718

11372

12026

12674

13317

13958

14599

24.2

9555

10199

10846

11499

12153

12800

13443

14083

14723

24.4

9679

10325

10973

11626

12279

12926

13569

14209

14848

24.6

9803

10451

11100

11753

12406

13052

13694

14334

14973

Original

07-14-08

08.01.17

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHES

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

24.8

9928

10577

11227

11880

12532

13178

13820

14459

15098

25.0

10052

10703

11354

12007

12658

13304

13946

14585

15223

25.2

10178

10829

11481

12134

12784

13430

14072

14710

15348

25.4

10303

10955

11608

12260

12910

13555

14197

14835

15472

25.6

10428

11082

11735

12386

13036

13681

14323

14961

15597

25.8

10554

11208

11862

12513

13161

13807

14449

15086

15722

26.0

10680

11334

11988

12639

13287

13932

14574

15211

15847

26.2

10806

11461

12115

12765

13413

14058

14700

15337

15972

26.4

10932

11587

12241

12891

13538

14183

14825

15462

16097

26.6

11058

11714

12368

13017

13664

14309

14950

15587

16222

26.8

11185

11840

12494

13143

13790

14434

15075

15712

16346

27.0

11311

11966

12620

13269

13915

14559

15200

15836

16471

27.2

11438

12093

12747

13395

14041

14685

15325

15961

16595

27.4

11565

12219

12873

13521

14167

14810

15450

16086

16720

27.6

11691

12346

12999

13647

14292

14935

15575

16210

16844

27.8

11818

12472

13125

13773

14418

15060

15699

16335

16969

28.0

11945

12599

13251

13899

14544

15185

15824

16459

17093

28.2

12072

12725

13377

14025

14669

15310

15949

16583

17217

28.4

12199

12852

13504

14151

14795

15436

16073

16708

17341

28.6

12326

12979

13630

14277

14921

15561

16198

16832

17465

28.8

12453

13105

13756

14403

15046

15686

16323

16956

17589

29.0

12580

13232

13882

14529

15172

15811

16447

17081

17713

08.01.18

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHES

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

29.2

12707

13358

14009

14655

15297

15936

16572

17205

17837

29.4

12834

13485

14135

14781

15423

16062

16697

17330

17961

29.6

12961

13612

14261

14906

15548

16187

16822

17454

18085

29.8

13088

13738

14387

15032

15674

16312

16947

17578

18209

30.0

13214

13864

14513

15158

15799

16437

17072

17703

18333

30.2

13341

13991

14639

15283

15924

16562

17196

17827

18457

30.4

13468

14117

14765

15409

16049

16687

17321

17951

18580

30.6

13594

14243

14891

15534

16174

16812

17446

18076

18704

30.8

13720

14369

15017

15660

16299

16936

17570

18200

18828

31.0

13846

14495

15142

15785

16424

17061

17695

18324

18952

31.2

13972

14620

15267

15910

16549

17185

17819

18448

19077

31.4

14098

14746

15393

16035

16676

17310

17943

18572

19201

31.6

14224

14871

15518

16159

16798

17434

18067

18697

19325

31.8

14350

14997

15643

16284

16923

17558

18191

18821

19449

32.0

14475

15122

15768

16409

17047

17683

18315

18945

19572

32.2

14601

15248

15893

16534

17172

17807

18439

19068

19696

32.4

14727

15373

16018

16659

17296

17931

18563

19192

19820

32.6

14853

15499

16143

16784

17421

18056

18687

19316

19943

32.8

14978

15624

16269

16909

17546

18180

18811

19439

20067

33.0

15104

15749

16394

17034

17671

18304

18935

19563

20190

33.2

15230

15875

16519

17159

17795

18428

19059

19686

20313

33.4

15357

16001

16644

17284

17920

18553

19183

19810

20436

Original

07-14-08

08.01.19

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHES

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

33.6

15482

16126

16770

17409

18045

18677

19306

19933

20559

33.8

15608

16252

16895

17534

18170

18801

19430

20057

20681

34.0

15733

16377

17020

17659

18294

18925

19554

20180

20804

34.2

15859

16503

17146

17784

18419

19050

19678

20303

20927

34.4

15985

16628

17271

17909

18543

19174

19801

20427

21050

34.6

16111

16753

17396

18034

18668

19298

19925

20550

21173

34.8

16236

16879

17521

18158

18792

19422

20049

20674

21296

35.0

16362

17004

17646

18283

18916

19546

20173

20798

21419

35.2

16488

17129

17771

18407

19040

19670

20297

20921

21542

35.4

16613

17254

17895

18532

19164

19794

20421

21045

21665

35.6

16738

17379

18020

18656

19288

19918

20545

21169

21788

35.8

16864

17504

18145

18780

19412

20042

20668

21292

21911

36.0

16989

17629

18269

18904

19536

20165

20792

21416

22034

36.2

17114

17754

18394

19028

19660

20289

20915

21539

22157

36.4

17239

17879

18518

19152

19783

20412

21039

21662

22280

36.6

17365

18003

18642

19276

19907

20536

21162

21785

22402

36.8

17489

18128

18767

19400

20031

20659

21285

21908

22524

37.0

17614

18253

18891

19524

20155

20783

21408

22030

22646

37.2

17739

18377

19015

19648

20278

20906

21531

22153

22768

37.4

17864

18502

19139

19772

20402

21029

21654

22275

22889

37.6

17989

18626

19264

19896

20526

21153

21777

22397

23010

37.8

18114

18751

19388

20020

20649

21276

21899

22518

23131

08.01.20

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHES

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

38.0

18238

18875

19512

20144

20773

21399

22022

22640

23251

38.2

18363

18999

19636

20268

20897

21523

22145

22761

23370

38.4

18488

19124

19761

20392

21020

21646

22267

22883

23489

38.6

18613

19249

19885

20516

21144

21770

22390

23004

23608

38.8

18738

19373

20009

20640

21268

21893

22513

23125

23726

39.0

18863

19498

20134

20764

21392

22017

22637

23246

23844

39.2

18988

19622

20258

20888

21515

22141

22760

23367

23961

39.4

19113

19747

20382

21012

21639

22265

22883

23487

24078

39.6

19238

19872

20507

21136

21762

22388

23006

23608

24195

39.8

19363

19996

20631

21260

21886

22512

23129

23729

24313

40.0

19487

20120

20755

21384

22009

22635

23252

23850

24430

40.2

19612

20245

20879

21507

22133

22759

23374

23971

24549

40.4

19737

20369

21003

21631

22256

22882

23497

24092

24667

40.6

19861

20493

21127

21754

22379

23004

23619

24213

24787

40.8

19985

20617

21250

21877

22502

23127

23740

24335

24907

41.0

20110

20741

21374

22000

22624

23249

23862

24456

25028

41.2

20234

20864

21497

22124

22747

23371

23983

24577

25149

41.4

20358

20988

21620

22247

22869

23492

24104

24698

25270

41.6

20481

21111

21744

22370

22992

23614

24224

24818

25390

41.8

20605

21235

21867

22493

23115

23735

24344

24938

25509

42.0

20729

21358

21990

22616

23237

23857

24464

25056

25627

42.2

20853

21482

22113

22739

23360

23978

24584

25174

25742

Original

07-14-08

08.01.21

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHES

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

42.4

20977

21605

22236

22862

23483

24100

24703

25290

25855

42.6

21100

21729

22360

22986

23606

24221

24822

25405

25966

42.8

21224

21852

22483

23109

23729

24343

24940

25518

26074

43.0

21348

21976

22607

23233

23853

24464

25058

25629

26178

43.2

21472

22099

22730

23357

23976

24586

25176

25740

26281

43.4

21596

22223

22854

23481

24100

24708

25294

25850

26382

43.6

21720

22346

22977

23604

24223

24830

25412

25959

26481

43.8

21844

22470

23101

23728

24346

24952

25530

26068

26580

44.0

21968

22593

23224

23851

24468

25074

25649

26177

26677

44.2

22092

22717

23347

23974

24591

25196

25768

26287

26775

44.4

22215

22840

23470

24096

24712

25318

25887

26396

26873

44.6

22339

22963

23593

24218

24833

25440

26007

26507

26971

44.8

22462

23086

23715

24339

24954

25562

26128

26619

27071

45.0

22585

23208

23837

24459

25074

25683

26249

26731

27171

45.2

22708

23331

23959

24579

25193

25805

26370

26844

27272

45.4

22830

23453

24080

24699

25311

25925

26490

26956

27373

45.6

22953

21575

24201

24818

25430

26045

26610

27068

27474

45.8

23074

23696

24322

24937

25547

26164

26727

27178

27574

46.0

23196

23817

24442

25055

25665

26282

26844

27287

27674

46.2

23316

23937

24562

25174

25782

26398

26957

27394

27773

46.4

23437

24057

24682

25293

25899

26513

27069

27499

27870

46.6

23556

24177

24801

25411

26016

26626

27177

27601

27965

08.01.22

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHES

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

46.8

23675

24296

24920

25530

26133

26738

27281

27700

28059

47.0

23794

24414

25038

25649

26249

26847

27383

27796

28150

47.2

23912

24532

25157

25767

26366

26956

27483

27889

28239

47.4

24030

24650

25275

25886

26483

27063

27580

27979

28325

47.6

24149

24768

25394

26006

26599

27170

27676

28068

28409

47.8

24267

24886

25512

26125

26716

27277

27771

28155

28490

48.0

24385

25005

25631

26244

26832

27384

27867

28240

28567

48.2

24504

25124

25751

26364

26949

27491

27962

28324

28642

48.4

24624

25244

25871

26484

27066

27599

28058

28406

28712

48.6

24744

25364

25991

26604

27183

27708

28156

28489

28779

48.8

24866

25485

26113

26724

27299

27818

28255

28570

28843

49.0

24987

25607

26234

26844

27416

27929

28356

28652

28903

49.2

25109

25729

26356

26964

27531

28040

28457

28732

28960

49.4

25231

25850

26477

27082

27646

28150

28558

28812

29016

49.6

25352

25971

26597

27199

27759

28260

28659

28891

29070

49.8

25471

26091

26716

27314

27870

28368

28759

28969

29122

50.0

25590

26209

26832

27428

27979

28474

28857

29046

29175

50.2

25706

26324

26947

27538

28085

28577

28953

29122

29228

50.4

25821

26438

27059

27646

28187

28677

29045

29197

29281

50.6

25932

26548

27167

27750

28287

28773

29134

29270

29336

50.8

26041

26656

27273

27850

28382

28864

29220

29343

29392

51.0

26148

26760

27375

27948

28474

28952

29301

29413

29450

Original

07-14-08

08.01.23

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHES

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

51.2

26252

26863

27475

28042

28564

29036

29378

29481

29509

51.4

26354

26963

27572

28135

28651

29116

29451

29548

29567

51.6

27648

27062

27669

28227

28737

29194

29521

29612

29626

51.8

27649

27160

27765

28319

28823

29270

29587

29673

29683

52.0

27650

27257

27860

28411

28908

29344

29649

29731

29739

52.2

27651

27354

27956

28503

28994

29416

29708

29786

29793

52.4

27652

27452

28052

28597

29082

29487

29764

29838

29844

52.6

27653

27551

28150

28694

29172

29558

29817

29886

29892

52.8

27654

27651

28250

28793

29264

29629

29867

29930

29936

53.0

27655

27751

28351

28894

29357

29700

29915

29970

29977

53.2

27656

27853

28453

28995

29452

29769

29960

30008

30015

53.4

27657

27954

28555

29097

29546

29839

30004

30044

30050

53.6

27658

28055

28656

29199

29639

29907

30048

30079

30084

53.8

27659

28155

28756

29298

29731

29974

30090

30113

30116

54.0

27660

28255

28855

29395

29819

30039

30133

30146

30147

FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

3.0 08.01.24

426

-1.50 475

-1.00 534

-.50 656

0.00 865

07-14-08

.50 1173

1.00 1591

1.50 2111

2.00 2673 Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.2

452

503

562

687

903

1228

1664

2197

2767

3.4

479

532

592

719

943

1284

1737

2282

2861

3.6

506

561

623

753

985

1340

1810

2368

2955

3.8

534

591

656

789

1029

1398

1883

2453

3049

4.0

562

622

690

828

1076

1457

1956

2537

3143

4.2

592

655

727

870

1126

1518

2028

2621

3236

4.4

622

690

766

916

1180

1581

2101

2703

3329

4.6

654

726

808

966

1238

1646

2173

2785

3421

4.8

687

764

853

1020

1301

1713

2245

2867

3513

5.0

722

805

901

1079

1368

1783

2318

2947

3605

5.2

758

847

953

1141

1439

1856

2391

3028

3696

5.4

796

892

1006

1207

1513

1930

2465

3109

3788

5.6

836

940

1063

1276

1590

2008

2542

3191

3880

5.8

879

989

1122

1347

1670

2087

2620

3275

3973

6.0

924

1042

1184

1420

1752

2169

2701

3360

4066

6.2

972

1097

1248

1495

1835

2254

2786

3448

4161

6.4

1023

1155

1314

1571

1919

2341

2874

3539

4256

6.6

1078

1215

1382

1648

2004

2431

2966

3634

4352

6.8

1135

1279

1452

1725

2089

2523

3063

3732

4451

7.0

1196

1345

1523

1803

2174

2617

3164

3834

4550

7.2

1259

1412

1596

1881

2259

2713

3268

3939

4651

7.4

1323

1482

1670

1959

2344

2811

3375

4046

4753

Original

07-14-08

08.01.25

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.6

1389

1552

1744

2037

2430

2909

3484

4155

4857

7.8

1455

1623

1818

2115

2516

3009

3595

4266

4961

8.0

1522

1694

1893

2194

2602

3109

3706

4378

5067

8.2

1588

1764

1967

2272

2689

3210

3818

4490

5174

8.4

1653

1833

2041

2350

2776

3310

3930

4602

5283

8.6

1717

1901

2113

2428

2863

3410

4040

4715

5392

8.8

1778

1967

2184

2506

2950

3510

4149

4826

5502

9.0

1838

2032

2255

2584

3039

3609

4257

4937

5613

9.2

1898

2096

2325

2664

3128

3709

4363

5047

5724

9.4

1957

2161

2396

2744

3219

3808

4470

5157

5836

9.6

2018

2226

2469

2826

3311

3909

4576

5266

5948

9.8

2079

2294

2543

2911

3406

4011

4682

5376

6061

10.0

2143

2363

2621

2999

3504

4114

4789

5485

6173

10.2

2209

2436

2702

3090

3604

4219

4896

5595

6285

10.4

2279

2513

2787

3185

3707

4327

5005

5705

6397

10.6

2353

2595

2877

3285

3814

4437

5116

5816

6508

10.8

2432

2681

2972

3389

3926

4550

5228

5927

6619

11.0

2515

2773

3072

3498

4040

4666

5343

6039

6729

11.2

2602

2868

3177

3610

4157

4784

5459

6152

6839

11.4

2692

2967

3284

3725

4277

4905

5576

6266

6949

11.6

2785

3068

3394

3843

4399

5027

5695

6381

7060

11.8

2880

3172

3506

3962

4522

5150

5815

6496

7171

08.01.26

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

12.0

2975

3276

3619

4082

4646

5274

5937

6613

7284

12.2

3072

3382

3733

4202

4770

5398

6059

6731

7397

12.4

3169

3487

3846

4322

4894

5523

6182

6850

7513

12.6

3265

3591

3958

4440

5017

5648

6305

6970

7630

12.8

3361

3694

4068

4557

5139

5772

6429

7092

7749

13.0

3455

3796

4177

4673

5260

5895

6553

7215

7870

13.2

3549

3896

4285

4788

5380

6019

6677

7338

7993

13.4

3643

3997

4392

4901

5500

6142

6802

7463

8116

13.6

3736

4096

4498

5015

5619

6265

6927

7588

8242

13.8

3829

4196

4605

5128

5738

6388

7052

7714

8367

14.0

3923

4296

4712

5242

5858

6511

7177

7840

8494

14.2

4017

4397

4819

5356

5978

6634

7302

7966

8620

14.4

4111

4498

4928

5471

6098

6758

7427

8091

8747

14.6

4206

4601

5038

5588

6220

6882

7552

8217

8873

14.8

4302

4705

5150

5706

6342

7006

7677

8342

8998

15.0

4399

4810

5263

5826

6466

7131

7801

8467

9124

15.2

4497

4917

5378

5947

6591

7257

7926

8591

9248

15.4

4596

5025

5494

6070

6716

7382

8051

8715

9373

15.6

4696

5134

5612

6193

6843

7508

8175

8839

9497

15.8

4798

5244

5731

6318

6969

7635

8300

8963

9621

16.0

4901

5356

5850

6443

7097

7761

8425

9088

9745

16.2

5005

5469

5971

6569

7224

7888

8550

9212

9869

Original

07-14-08

08.01.27

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.4

5111

5584

6093

6695

7352

8015

8676

9336

9993

16.6

5219

5699

6216

6822

7480

8142

8801

9461

10117

16.8

5328

5816

6339

6949

7608

8270

8927

9586

10241

17.0

5439

5934

6463

7076

7736

8397

9054

9711

10366

17.2

5550

6052

6587

7203

7864

8524

9180

9837

10491

17.4

5663

6172

6712

7330

7991

8652

9307

9962

10616

17.6

5776

6291

6837

7457

8119

8779

9434

10088

10741

17.8

5890

6411

6962

7585

8247

8907

9561

10215

10866

18.0

6004

6531

7088

7712

8374

9034

9688

10341

10992

18.2

6117

6651

7213

7840

8502

9162

9815

10467

11117

18.4

6230

6771

7338

7967

8630

9289

9942

10594

11243

18.6

6343

6891

7463

8095

8758

9417

10069

10720

11369

18.8

6455

7010

7588

8222

8885

9544

10196

10846

11494

19.0

6566

7128

7713

8350

9013

9672

10323

10973

11620

19.2

6676

7247

7836

8477

9141

9799

10450

11099

11746

19.4

6787

7365

7963

8605

9268

9926

10577

11225

11871

19.6

6898

7484

8087

8732

9396

10054

10704

11352

11997

19.8

7009

7603

8212

8859

9524

10181

10831

11478

12123

20.0

7122

7722

8337

8987

9651

10308

10957

11604

12249

20.2

7235

7848

8462

9114

9778

10435

11084

11730

12375

20.4

7350

7963

8588

9241

9906

10562

11210

11856

12501

20.6

7467

8084

8714

9368

10033

10689

11337

11982

12627

08.01.28

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

20.8

7586

8207

8840

9496

10160

10815

11463

12108

12753

21.0

7706

8331

8967

9623

10287

10942

11590

12235

12879

21.2

7828

8456

9094

9750

10413

11068

11716

12361

13005

21.4

7951

8582

9221

9878

10540

11194

11842

12487

13130

21.6

8076

8708

9348

10005

10666

11321

11968

12613

13256

21.8

8201

8835

9476

10132

10793

11447

12094

12739

13382

22.0

8327

8962

9604

10260

10920

11573

12220

12864

13508

22.2

8453

9089

9732

10387

11046

11699

12346

12990

13633

22.4

8580

9217

9860

10514

11173

11825

12472

13116

13759

22.6

8706

9344

9987

10642

11299

11951

12597

13241

13884

22.8

8832

9471

10115

10769

11426

12077

12723

13367

14010

23.0

8958

9598

10243

10897

11553

12203

12849

13492

14135

23.2

9084

9725

10370

11024

11679

12329

12975

13618

14260

23.4

9209

9851

10498

11151

11806

12455

13100

13743

14384

23.6

9334

9978

10625

11279

11933

12582

13226

13868

14509

23.8

9459

10104

10753

11406

12059

12708

13352

13993

14634

24.0

8584

10231

10880

11533

12186

12834

13477

14118

14759

24.2

9710

10357

11007

11660

12313

12960

13603

14244

14883

24.4

9835

10484

11134

11787

12439

13086

13729

14369

15008

24.6

9960

10610

11261

11914

12566

13212

13854

14494

15133

24.8

10085

10736

11388

12041

12692

13338

13980

14619

15258

25.0

10211

10863

11515

12168

12818

13464

14106

14754

15383

Original

07-14-08

08.01.29

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

25.2

10336

10989

11642

12294

12944

13590

14232

14870

15507

25.4

10462

11116

11769

12421

13070

13716

14357

14996

15632

25.6

10588

11242

11896

12547

13196

13842

14483

15121

15757

25.8

10714

11369

12022

12674

13322

13967

14609

15246

15882

26.0

10840

11495

12149

12800

13448

14093

14734

15371

16007

26.2

10966

11621

12275

12926

13573

14218

14860

15497

16132

26.4

11093

11748

12402

13052

13699

14344

14985

15622

16257

26.6

11219

11874

12528

13178

13825

14469

15110

15747

16381

26.8

11346

12001

12654

13304

13950

14595

15235

15872

16506

27.0

11472

12127

12781

13430

14076

14720

15360

15996

16631

27.2

11599

12254

12907

13556

14202

14845

15485

16121

16755

27.4

11725

12380

13033

13682

14327

14970

15610

16246

16880

27.6

11852

12506

13159

13808

14453

15095

15735

16370

17004

27.8

11979

12633

13285

13934

14578

15220

15859

16494

17128

28.0

12106

12759

13411

14059

14704

15345

15984

16619

17253

28.2

12233

12886

13538

14185

14829

15471

16108

16743

17377

28.4

12360

13012

13664

14311

14955

15596

16233

16867

17501

28.6

12485

13139

13790

14437

15081

15721

16358

16992

17625

28.8

12613

13265

13916

14563

15206

15846

16482

17116

17749

29.0

12740

13392

14042

14689

15332

15971

16607

17240

17873

29.2

12867

13518

14169

14815

15457

16096

16732

17365

17997

29.4

12994

13645

14295

14941

15583

16221

16857

17489

18121

08.01.30

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

29.6

13121

13772

14421

15067

15708

16347

16981

17613

18244

29.8

13248

13898

14547

15193

15834

16472

17106

17738

18368

30.0

13374

14024

14673

15318

15959

16597

17231

17862

18492

30.2

13501

14151

14799

15444

16084

16722

17356

17986

18616

30.4

13627

14277

14925

15569

16209

16847

17480

18111

18740

30.6

13754

14403

15051

15695

16334

16971

17605

18235

18864

30.8

13880

14529

15177

15820

16459

17096

17729

18359

18987

31.0

14006

14655

15302

15945

16584

17221

17854

18483

19112

31.2

14132

14780

15427

16070

16709

17345

17978

18607

19236

31.4

14258

14906

15552

16195

16833

17470

18102

18732

19360

31.6

14384

15031

15678

16320

16958

17594

18227

18856

19484

31.8

14510

15157

15803

16444

17083

17718

18351

18980

19607

32.0

14635

15282

15928

16569

17207

17842

18475

19104

19731

32.2

14761

15408

16053

16694

17332

17967

18599

19227

19855

32.4

14887

15533

16178

16819

17456

18091

18723

19351

19979

32.6

15012

15658

16303

16944

17581

18215

18846

19475

20102

32.8

15138

15784

16428

17068

17705

18339

18970

19598

20225

33.0

15264

15909

16553

17193

17830

18463

19094

19722

20348

33.2

15390

16035

16678

17318

17955

18588

19218

19845

20471

33.4

15515

16160

16804

17443

18079

18712

19342

19969

20594

33.6

15641

16285

16929

17568

18204

18836

19465

20092

20717

33.8

15767

16411

17054

17693

18329

18960

19589

20215

20840

Original

07-14-08

08.01.31

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

34.0

15893

16536

17179

17818

18453

19084

19713

20339

20962

34.2

16018

16662

17304

17943

18578

19209

19836

20462

21085

34.4

16144

16787

17430

18068

18702

19333

19960

20585

21208

34.6

16270

16912

17555

18193

18827

19457

20084

20709

21330

34.8

16395

17038

17680

18317

18951

19581

20208

20833

21453

35.0

16521

17163

17804

18442

19075

19705

20332

20956

21576

35.2

16647

17288

17929

18566

19199

19829

20456

21080

21699

35.4

16772

17413

18053

18691

19323

19953

20580

21203

21822

35.6

16897

17538

18179

18815

19447

20077

20703

21327

21945

35.8

17023

17663

18303

18939

19571

20200

20827

21451

22068

36.0

17148

17788

18428

19063

19695

20324

20951

21574

22191

36.2

17273

17913

18552

19187

19819

20448

21074

21697

22313

36.4

17398

18038

18677

19311

19942

20571

21198

21820

22436

36.6

17523

18162

18801

19435

20066

20695

21321

21943

22558

36.8

17648

18287

18925

19559

20190

20818

21444

22066

22680

37.0

17773

18411

19049

19683

20313

20941

21567

22188

22802

37.2

17898

18536

19174

19807

20437

21065

21690

22310

22924

37.4

18023

18660

19298

19931

20561

21188

21812

22432

23045

37.6

18147

18785

19422

20055

20684

21311

21935

22554

23165

37.8

18272

18909

19546

20179

20808

21434

22057

22676

23285

38.0

18397

19033

19670

20303

20931

21558

22180

22797

23405

38.2

18521

19158

19794

20427

21055

21681

22303

22918

23524

08.01.32

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

38.4

18616

19282

19918

20550

21179

21804

22425

23038

23642

38.6

18771

19406

20043

20674

21302

21928

22548

23159

23759

38.8

18896

19531

20167

20798

21426

22052

22671

23279

23876

39.0

19020

19655

20291

20922

21550

22175

22794

23399

23992

39.2

19145

19780

20415

21046

21674

22299

22917

23519

24107

39.4

19270

19904

20540

21170

21797

22423

23040

23639

24222

39.6

19395

20029

20664

21294

21921

22547

23162

23759

24337

39.8

19520

20153

20788

21417

22044

22671

23285

23878

24452

40.0

19644

20278

20912

21541

22168

22794

23408

23998

24567

40.2

19769

20402

21036

21665

22291

22917

23530

24118

24683

40.4

19894

20526

21160

21788

22414

23040

23652

24238

24799

40.6

20018

20650

21283

21911

22537

23163

23774

24357

24916

40.8

20142

20774

21407

22034

22660

23285

23897

24477

25034

41.0

20266

20897

21530

22157

22782

23407

24017

24597

25152

41.2

20390

21021

21653

22280

22904

23529

24137

24717

25271

41.4

20514

21144

21776

22403

23027

23650

24257

24836

25389

41.6

20637

21268

21899

22526

23149

23771

24377

24954

25507

41.8

20761

21391

22022

22648

23271

23892

24496

25072

25623

42.0

20885

21514

22145

22771

23394

24013

24615

25189

25738

42.2

21008

21637

22268

22894

23516

24133

24733

25305

25852

42.4

21132

21761

22392

23018

23639

24254

24851

25419

25963

42.6

21256

21884

22515

23141

23762

24375

24968

25532

26072

Original

07-14-08

08.01.33

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

42.8

21379

22007

22638

23265

23885

24495

25084

25644

26179

43.0

21503

22136

22762

23389

24008

24616

25201

25754

26282

43.2

21627

22254

22885

23513

24132

24737

25316

25863

26384

43.4

21750

22377

23009

23637

24255

24858

25432

25971

26483

43.6

21874

22500

23132

23760

24378

24979

25548

26078

26582

43.8

21998

22624

23255

23884

24501

25100

25664

26185

26679

44.0

22121

22747

23378

24007

24624

25221

25780

26293

26776

44.2

22245

22870

23501

24129

24746

25342

25897

26400

26872

44.4

22368

22993

23624

24251

24868

25463

26014

26508

26968

44.6

22492

23116

23746

24373

24988

25584

26132

26617

27064

44.8

22615

23238

23868

24493

25108

25705

26251

26727

27161

45.0

22738

23361

23989

24613

25228

25825

26370

26837

27259

45.2

22860

23483

24111

24732

25346

25946

26490

26948

27357

45.4

22982

23604

24231

24851

25464

26066

26609

27058

27455

45.6

23104

23726

24351

24968

25581

26184

26727

27168

27553

45.8

23225

23846

24471

25086

25697

26302

26843

27277

27650

46.0

23346

23966

24590

25203

25813

26418

26958

27384

27747

46.2

23466

24086

24709

25320

25928

26533

27070

27489

27843

46.4

23585

24205

24827

25436

26043

26646

27180

27592

27938

46.6

23704

24323

24944

25552

26157

26757

27286

27692

28032

46.8

23821

24440

25061

25669

26270

26865

27389

27790

28125

47.0

23938

24556

25178

25785

26384

26972

27488

27884

28216

08.01.34

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

47.2

24054

24672

25294

25901

26497

27077

27584

27975

28305

47.4

24170

24788

25410

26017

26609

27181

27679

28064

28391

47.6

24285

24904

25526

26133

26722

27284

27772

28151

28475

47.8

24401

25019

25643

26250

26835

27387

27863

28236

28556

48.0

24517

25135

25759

26367

26948

27490

27955

28319

28634

48.2

24633

25252

25877

26484

27061

27593

28046

28401

28709

48.4

24750

25369

25994

26602

27175

27697

28138

28482

28780

48.6

24868

25487

26113

26720

27290

27803

28231

28561

28846

48.8

24986

25606

26233

26839

27405

27909

28326

28640

28909

49.0

25105

25725

26353

26958

27520

28017

28421

28718

28968

49.2

25224

25845

26473

27077

27634

28126

28518

28795

29024

49.4

25343

25965

26593

27194

27748

28234

28614

28872

29078

49.6

25462

26084

26712

27311

27861

28341

28710

28947

29130

49.8

25579

26201

26829

27425

27971

28447

28806

29022

29180

50.0

25696

26317

26944

27537

28079

28550

28900

29096

29230

50.2

25810

26432

27057

27646

28184

28652

28992

29169

29280

50.4

25923

26543

27167

27752

28285

28750

29081

29242

29331

50.6

26033

26652

27273

27854

28383

28844

29168

29313

29383

50.8

26140

26757

27376

27952

28476

28933

29252

29383

29437

51.0

26245

26860

27476

28046

28565

29019

29332

29452

29492

51.2

26348

26961

27573

28138

28651

29101

29409

29520

29548

51.4

26449

27059

27667

28227

28734

29180

29482

29585

29604

Original

07-14-08

08.01.35

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

51.6

26548

27155

27760

28314

28816

29256

29552

29648

29660

51.8

26647

27251

27852

28401

28897

29330

29619

29709

29715

52.0

26744

27346

27944

28488

28977

29401

29682

29766

29769

52.2

26841

27440

28035

28576

29058

29471

29742

29821

29821

52.4

26938

27535

28128

28665

29139

29539

29798

29872

29870

52.6

27036

27630

28221

28756

29222

29607

29851

29919

29916

52.8

27133

27726

28316

28849

29308

29674

29901

29962

29959

53.0

27231

27823

28413

28945

29395

29741

29947

30001

29999

53.2

27329

27920

28510

29042

29483

29807

29991

30037

30036

53.4

27428

28017

28607

29139

29570

29872

30037

30072

30071

53.6

27526

28114

28704

29235

29658

29936

30075

30104

30104

53.8

27624

28210

28801

29331

29743

29999

30115

30136

30135

54.0

27721

28306

28895

29424

29827

30060

30156

30167

30165

08.01.36

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

Original

07-14-08

08.01.37

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCH

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

439

490

555

687

907

1222

1648

2182

2759

3.2

468

521

587

721

949

1281

1726

2271

2855

3.4

497

552

620

756

992

1341

1804

2360

2950

3.6

526

584

654

793

1037

1401

1881

2448

3046

3.8

556

161

689

832

1084

1463

1958

2536

3141

4.0

587

650

726

874

1134

1525

2034

2623

3236

4.2

618

684

764

918

1187

1589

2110

2709

3331

4.4

649

720

805

966

1243

1655

2185

2794

3426

4.6

682

757

848

1017

1303

1722

2260

2878

3521

4.8

715

795

893

1072

1367

1791

2334

2962

3615

5.0

750

836

941

1131

1435

1862

2407

3044

3709

5.2

786

878

992

1194

1507

1935

2482

3127

3804

5.4

823

922

1045

1260

1582

2011

2557

3210

3898

5.6

863

969

1101

1328

1659

2088

2633

3294

3993

5.8

906

1019

1160

1399

1740

2169

2712

3379

4088

6.0

951

1071

1221

1473

1822

2251

2794

3466

4183

6.2

999

1126

1285

1549

1907

2337

2879

3555

4279

6.4

1051

1184

1352

1626

1993

2425

2968

3647

4376

6.6

1106

1246

1422

1705

2080

2517

3061

3743

4474

6.8

1165

1312

1494

1785

2167

2611

3160

3842

4573

7.0

1227

1380

1569

1866

2256

2708

3262

3945

4673

08.01.38

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCH

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

1293

1451

1646

1948

2345

2807

3369

4051

4773

7.4

1360

1524

1724

2031

2434

2908

3479

4159

4876

7.6

1429

1598

1802

2113

2524

3010

3591

4269

4979

7.8

1499

1673

1882

2196

2614

3114

3704

4381

5083

8.0

1569

1748

1961

2279

2704

3218

3819

4494

5189

8.2

1640

1822

2039

2361

2794

3322

3934

4608

5296

8.4

1709

1896

2116

2443

2884

3426

4049

4722

5404

8.6

1777

1967

2192

2524

2974

3529

4163

4836

5513

8.8

1843

2037

2266

2605

3064

3632

4275

4950

5624

9.0

1907

2105

2338

2685

3154

3734

4386

5063

5736

9.2

1971

2172

2410

2765

3245

3835

4496

5175

5849

9.4

2035

2240

2482

2846

3337

3937

4605

5287

5962

9.6

2099

2308

2556

2929

3430

4040

4714

5399

6076

9.8

2164

2377

2631

3015

3525

4143

4823

5511

6190

10.0

2231

2449

2709

3103

3623

4248

4932

5623

6305

10.2

2300

2523

2791

3194

3724

4354

5042

5735

6419

10.4

2372

2602

2877

3290

3828

4463

5153

5847

6532

10.6

2448

2685

2968

3390

3936

4574

5265

5960

6645

10.8

2527

2773

3064

3496

4049

4689

5378

6072

6758

11.0

2611

2865

3166

3607

4165

4806

5493

6185

6869

11.2

2698

2962

3272

3721

4284

4925

5609

6299

6981

11.4

2787

3061

3382

3839

4406

5046

5727

6413

7092

Original

07-14-08

08.01.39

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCH

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.6

2879

3164

3495

3958

4530

5169

5846

6529

7204

11.8

2973

3268

3610

4081

4656

5293

5966

6644

7316

12.0

3068

3374

3726

4204

4782

5418

6087

6761

7430

12.2

3164

3480

3842

4327

4909

5544

6209

6879

7544

12.4

3261

3587

3958

4451

5036

5670

6332

6999

7660

12.6

3358

3693

4073

4573

5162

5796

6455

7119

7778

12.8

3454

3798

4187

4693

5287

5922

6579

7241

7897

13.0

3550

3902

4299

4812

5411

6047

6704

7364

8019

13.2

3646

4005

4410

4930

5534

6172

6829

7488

8141

13.4

3742

4108

4520

5046

5656

6297

6954

7613

8266

13.6

3837

4210

4629

5163

5778

6421

7080

7738

8391

13.8

3933

4313

4738

5279

5900

6546

7206

7865

8517

14.0

4029

4415

4847

5395

6021

6671

7332

7991

8644

14.2

4125

4518

4957

5511

6143

6796

7458

8117

8770

14.4

4221

4621

5068

5628

6265

6920

7584

8244

8897

14.6

4318

4726

5179

5746

6388

7045

7710

8370

9024

14.8

4415

4831

5292

5866

6512

7171

7835

8496

9150

15.0

4513

4937

5406

5986

6636

7296

7961

8622

9276

15.2

4611

5045

5522

6108

6761

7422

8086

8747

9401

15.4

4711

5153

5639

6230

6887

7548

8212

8872

9527

15.6

4811

5263

5757

6354

7013

7675

8337

8997

9652

15.8

4913

5374

5876

6478

7139

7801

8462

9122

9777

08.01.40

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCH

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.0

5016

5486

5996

6603

7266

7927

8588

9246

9901

16.2

5121

5599

6117

6729

7393

8054

8713

9371

10026

16.4

5228

5714

6239

6855

7520

8181

8839

9496

10151

16.6

5336

5830

6363

6982

7648

8308

8965

9621

10276

16.8

5446

5948

6487

7109

7775

8435

9091

9747

10400

17.0

5557

6067

6611

7326

7902

8562

9217

9872

10526

17.2

5671

6187

6737

7363

8030

8689

9343

9998

10651

17.4

5785

6307

6862

7491

8157

8816

9470

10124

10776

17.6

5900

6428

6989

7619

8285

8943

9597

10250

10902

17.8

6015

6550

7115

7746

8412

9070

9723

10376

11027

18.0

6131

6672

7242

7874

8540

9197

9850

10502

11153

18.2

6246

6794

7368

8002

8667

9325

9977

10629

11278

18.4

6362

6915

7495

8130

8795

9452

10104

10755

11404

18.6

6476

7037

7622

8258

8922

9579

10231

10881

11530

18.8

5690

7158

7748

8386

9050

9706

10358

11007

11655

19.0

6704

7278

7874

8514

9177

9834

10484

11134

11781

19.2

6815

7398

8000

8642

9305

9961

10611

11260

11907

19.4

6929

7518

8126

8770

9432

10088

10738

11386

12032

19.6

7042

7638

8251

8897

9559

10215

10864

11512

12158

19.8

7155

7758

8377

9025

9687

10342

10991

11638

12284

20.0

7269

7879

8503

9152

9814

10469

11118

11764

12409

20.2

7384

8000

8629

9280

9941

10596

11244

11890

12535

Original

07-14-08

08.01.41

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCH

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

20.4

7500

8121

8755

9407

10068

10722

11370

12016

12661

20.6

7617

8244

8881

9534

10195

10849

11497

12142

12787

20.8

7736

8367

9007

9662

10322

10975

11623

12269

12913

21.0

7857

8491

9134

9789

10449

11102

11749

12395

13039

21.2

7979

8616

9261

9916

10575

11228

11876

12521

13165

21.4

8102

8741

9388

10043

10702

11354

12002

12647

13290

21.6

8227

8867

9515

10170

10828

11481

12128

12773

13416

21.8

8352

8994

9642

10297

10955

11607

12254

12899

13542

22.0

8477

9120

9770

10424

11081

11733

12380

13024

13668

22.2

8603

9247

9897

10551

11207

11859

12506

13150

13793

22.4

8730

9374

10024

10678

11334

11985

12632

13276

13919

22.6

8856

9501

10152

10805

11460

12111

12758

13402

14044

22.8

8982

9628

10279

10932

11587

12237

12883

13527

14169

23.0

9109

9755

10406

11059

11713

12363

13009

13652

14295

23.2

9235

9882

10533

11187

11840

12489

13135

13778

14420

23.4

9361

10009

10661

11314

11967

12615

13260

13903

14544

23.6

9487

10136

10788

11441

12093

12741

13386

14028

14669

23.8

9613

10262

10915

11568

12220

12868

13512

14153

14794

24.0

9739

10389

11042

11695

12346

12994

13637

14278

14919

24.2

9865

10516

11169

11821

12473

13120

13763

14403

15043

24.4

9991

10643

11296

11948

12599

13246

13888

14529

15168

24.6

10117

10769

11422

12075

12725

13372

14014

14654

15293

08.01.42

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCH

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

24.8

10243

10896

11549

12202

12852

13498

14140

14779

15417

25.0

10369

11022

11676

12328

12978

13624

14266

14904

15542

25.2

10495

11149

11803

12455

13104

13750

14391

15030

15667

25.4

10622

11276

11930

12581

13230

13875

14517

15155

15792

25.6

10748

11402

12056

12707

13356

14001

14643

15280

15917

25.8

10874

11529

12183

12834

13481

14127

14769

15406

16041

26.0

11001

11655

12309

12960

13607

14253

14894

15531

16166

26.2

11127

11782

12436

13086

13733

14378

15020

15656

16291

26.4

11253

11908

12562

13212

13859

14504

15145

15781

16416

26.6

11380

12035

12688

13338

13984

14629

15270

15906

16540

26.8

11506

12161

12815

13464

14110

14754

15395

16031

16665

27.0

11633

12288

12941

13590

14235

14879

15520

16156

16790

27.2

11759

12414

13067

13716

14361

15005

15645

16281

16914

27.4

11886

12540

13193

13841

14486

15130

15770

16405

17039

27.6

12013

12667

13319

13967

14612

15255

15894

16530

17163

27.8

12139

12793

13445

14093

14737

15380

16019

16654

17288

28.0

12266

12919

13571

14219

14863

15505

16143

16778

17412

28.2

12393

13046

13697

14345

14989

15630

16268

16903

17536

28.4

12520

13172

13823

14471

15114

15755

16392

17027

17660

28.6

12647

13299

13950

14597

15240

15880

16517

17151

17784

28.8

12773

13425

14076

14722

15365

16005

16642

17275

17908

29.0

12900

13552

14202

14848

15491

16130

16766

17400

18032

Original

07-14-08

08.01.43

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCH

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

29.2

13027

13678

14328

14974

15616

16255

16891

17524

18156

29.4

13154

13805

14455

15100

15742

16380

17016

17648

18280

29.6

13281

13931

14581

15226

15867

16505

17140

17772

18403

29.8

13407

14058

14707

15352

15993

16631

17265

17897

18527

30.0

13534

14184

14833

15478

16118

16756

17390

18021

18651

30.2

13660

14310

14959

15603

16243

16881

17514

18145

18775

30.4

13787

14437

15085

15729

16369

17005

17639

18269

18898

30.6

13913

14563

15211

15854

16494

17130

17764

18394

19022

30.8

14040

14689

15336

15979

16619

17255

17888

18518

19146

31.0

14166

14814

15462

16104

16743

17380

18013

18642

19270

31.2

14292

14940

15587

16229

16868

17504

18137

18766

19394

31.4

14418

15066

15712

16354

16993

17628

18261

18890

19518

31.6

14543

15191

15837

16479

17117

17753

18385

19014

19642

31.8

14669

15316

15962

16604

17241

17877

18510

19138

19766

32.0

14795

15442

16087

16728

17366

18001

18634

19262

19890

32.2

14921

15567

16212

16853

17490

18125

18758

19386

20013

32.4

15047

15693

16337

16978

17615

18250

18882

19510

20137

32.6

15172

15818

16462

17103

17739

18374

19005

19633

20260

32.8

15298

15943

16587

17227

17864

18498

19129

19757

20383

33.0

15424

16069

16712

17352

17988

18622

19253

19880

20506

33.2

15549

16194

16838

17477

18113

18746

19377

20004

20629

33.4

15675

16319

16963

17602

18238

18870

19500

20127

20752

08.01.44

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCH

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

33.6

15801

16445

17088

17727

18362

18995

19624

20250

20874

33.8

15926

16570

17213

17852

18487

19119

19747

20373

20997

34.0

16052

16696

17338

17977

18612

19243

19871

20497

21119

34.2

16178

16821

17463

18102

18736

19367

19995

20620

21242

34.4

16304

16946

17589

18227

18861

19491

20119

20743

21364

34.6

16429

17072

17714

18351

18985

19615

20242

20867

21487

34.8

16555

17197

17839

18476

19109

19739

20366

20990

21609

35.0

16680

17322

17964

18600

19234

19864

20490

21114

21732

35.2

16806

17448

18088

18725

19358

19988

20614

21237

21855

35.4

16932

17573

18213

18849

19482

20112

20738

21361

21977

35.6

17057

17698

18338

18973

19606

20235

20862

21484

22100

35.8

17183

17823

18463

19098

19730

20359

20986

21607

22222

36.0

17308

17948

18587

19222

19853

20483

21109

21731

22345

36.2

17433

18073

18712

19346

19977

20607

21233

21854

22467

36.4

17558

18197

18836

19470

20101

20730

21356

21977

22589

36.6

17683

18322

18960

19594

20225

20854

21479

22099

22711

36.8

17808

18447

19085

19718

20348

20977

21602

22222

22833

37.0

17933

18571

19209

19842

20472

21100

21725

22344

22955

37.2

18058

18696

19333

19966

20595

21223

21847

22466

23076

37.4

18183

18820

19457

20090

20719

21346

21970

22588

23196

37.6

18307

18944

19581

20213

20842

21469

22092

22709

23317

37.8

18432

19069

19705

20337

20966

21593

22214

22830

23436

Original

07-14-08

08.01.45

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCH

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

38.0

18556

19193

19829

20461

21090

21716

22337

22951

23555

38.2

18681

19317

19953

20585

21213

21839

22459

23071

23673

38.4

18806

19442

20078

20709

21337

21962

22581

23191

23789

38.6

18931

19566

20202

20833

21461

22086

22704

23311

23905

38.8

19055

19690

20326

20957

21584

22210

22827

23430

24020

39.0

19180

19815

20451

21081

21708

22333

22950

23549

24134

39.2

19305

19940

20575

21205

21832

22457

23072

23668

24247

39.4

19430

20064

20699

21329

21955

22581

23195

23786

24360

39.6

19555

20189

20824

21453

22079

22705

23318

23905

24472

39.8

19680

20313

20948

21576

22203

22829

23441

24023

24584

40.0

19804

20438

21072

21700

22326

22953

23563

24141

24697

40.2

19929

20562

21196

21824

22449

23076

23685

24259

24809

40.4

20053

20686

21320

21947

22572

23199

23807

24377

24923

40.6

20178

20810

21443

22070

22695

23322

23929

24495

25036

40.8

20302

20934

21567

22193

22817

23444

24050

24614

25151

41.0

20426

21057

21690

22316

22940

23565

24170

24732

25267

41.2

20550

21181

21813

22438

23062

23687

24290

24850

25382

41.4

20673

21304

21936

22561

23184

23808

24410

24967

25498

41.6

20797

21427

22059

22683

23306

23928

24529

25084

25613

41.8

20921

21551

22182

22806

23428

24049

24647

25200

25727

42.0

21044

21674

22305

22929

23550

24169

24765

25315

25840

42.2

21167

21797

22427

23051

23672

24289

24881

25429

25951

08.01.46

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCH

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

42.4

21291

21920

22550

23175

23794

24408

24997

25542

26061

42.6

21414

22043

22673

23298

23917

24528

25112

25653

26168

42.8

21538

22166

22796

23422

24040

24647

25227

25762

26272

43.0

21661

22289

22920

23546

24163

24766

25340

25870

26374

43.2

21785

22412

23043

23670

24286

24886

25453

25976

26475

43.4

21908

22535

23166

23793

24410

25005

25566

26082

26573

43.6

22032

22658

23289

23917

24532

25124

25678

26187

26670

43.8

22155

22781

23412

24041

24655

25243

25791

26292

26765

44.0

22279

22904

23535

24164

24777

25362

25905

26396

26860

44.2

22402

23027

23658

24286

24899

25481

26018

26501

26954

44.4

22525

23150

23780

24408

25019

25600

26133

26606

27048

44.6

22648

23273

23903

24529

25139

25719

26249

26712

27142

44.8

22771

23395

24024

24648

25258

25839

26366

26819

27235

45.0

22894

23517

24145

24768

25376

25958

26483

26927

27329

45.2

23017

23639

24266

24886

25492

26077

26601

27035

27423

45.4

23139

23761

24386

25003

25608

26195

26719

27142

27518

45.6

23250

23882

24506

25120

25723

26312

26835

27249

27611

45.8

23381

24002

24625

25235

25837

26427

26950

27355

27705

46.0

23501

24121

24743

25351

25950

26542

27063

27460

27799

46.2

23620

24240

24860

25465

26062

26654

27174

27563

27892

46.4

23739

24358

24977

25579

26174

26764

27281

27664

27985

46.6

23856

24474

25092

25693

26284

26872

27385

27763

28077

Original

07-14-08

08.01.47

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCH

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

46.8

23972

24590

25207

25806

26394

26977

27485

27858

28169

47.0

24086

24704

25321

25918

26504

27080

27582

27951

28259

47.2

24201

24818

25435

26031

26613

27181

27675

28041

28348

47.4

24314

24931

25548

26144

26721

27281

27766

28129

28436

47.6

24427

25044

25661

26256

26830

27379

27854

28214

28521

47.8

24540

25157

25774

26369

26939

27478

27942

28298

28603

48.0

24654

25270

25888

26483

27048

27576

28029

28379

28682

48.2

24767

25384

26002

26597

27157

27675

28115

28459

28757

48.4

24881

25498

26117

26711

27268

27774

28202

28537

28828

48.6

24995

25614

26233

26827

27379

27875

28290

28614

28895

48.8

25111

25730

26351

26943

27491

27977

28378

28689

28957

49.0

25227

25847

26469

27060

27603

28080

28468

28764

29015

49.2

25344

25964

26587

27177

27716

28184

28559

28837

29069

49.4

25460

26081

26705

27293

27827

28288

28650

28909

29121

49.6

25576

26198

26822

27408

27938

28391

28741

28981

29170

49.8

25691

26313

26937

27520

28046

28493

28831

29052

29218

50.0

25804

26427

27051

27631

28151

28594

28921

29122

29265

50.2

25917

26539

27162

27738

28254

28691

29009

29191

29312

50.4

26027

26649

27270

27842

28353

28786

29095

29260

29359

50.6

26135

26756

27374

27941

28447

28878

29180

29328

29408

50.8

26241

26859

27475

28036

28536

28965

29262

29396

29459

51.0

26345

26960

27572

28126

28621

29048

29342

29464

29511

08.01.48

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCH

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

51.2

26446

27059

27666

28214

28703

29128

29419

29530

29564

51.4

26546

27155

27757

28298

28782

29205

29493

29595

29617

51.6

26644

27249

27846

28381

28858

29279

29564

29657

29671

51.8

26741

27342

27935

28463

28933

29351

29631

29718

29724

52.0

26837

27435

28022

28544

29008

29420

29695

29776

29776

52.2

26933

27526

28109

28626

29083

29488

29756

29830

29826

52.4

27028

27617

28196

28709

29159

29553

29812

29881

29875

52.6

27122

27709

28284

28793

29236

29618

29865

29929

29921

52.8

27217

27801

28374

28881

29315

29682

29914

29972

29964

53.0

27312

27893

28464

28970

29396

29744

29959

30011

30004

53.2

27407

27986

28555

29060

29478

29806

30001

30048

30042

53.4

27502

28078

28647

29150

29560

29867

30041

30082

30078

53.6

27596

28171

28738

29241

29642

29927

30041

30114

30112

53.8

27691

28263

28829

29331

29723

29986

30080

30145

30144

54.0

27785

28354

28918

29419

29803

30044

30118

30176

30176

Original

07-14-08

08.01.49

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

08.01.50

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

458

512

583

722

950

1277

1718

2266

2856

3.2

489

545

618

759

996

1340

1798

2357

2953

3.4

521

578

653

798

1042

1403

1879

2448

3049

3.6

552

612

689

837

1091

1467

1959

2538

3145

3.8

584

647

727

879

1141

1532

2039

2627

3241

4.0

616

682

766

923

1193

1598

2118

2716

3337

4.2

648

718

806

969

1249

1664

2197

2805

3433

4.4

681

756

849

1019

1307

1733

2275

2892

3529

4.6

715

794

893

1072

1369

1802

2352

2978

3624

4.8

749

833

940

1128

1434

1873

2429

3063

3720

5.0

784

874

989

1188

1503

1946

2505

3148

3815

5.2

820

917

1041

1252

1576

2021

2582

3232

3910

5.4

858

962

1095

1318

1651

2098

2659

3317

4006

5.6

898

1009

1152

1388

1730

2177

2738

3403

4102

5.8

941

1059

1212

1460

1811

2259

2819

3490

4198

6.0

986

1112

1275

1535

1894

2343

2903

3578

4295

6.2

1035

1168

1340

1612

1980

2430

2990

3669

4392

6.4

1088

1228

1409

1691

2067

2520

3081

3763

4490

6.6

1144

1291

1480

1772

2156

2614

3176

3860

4589

6.8

1205

1358

1555

1855

2247

2710

3276

3960

4689

7.0

1269

1429

1632

1939

2339

2810

3380

4064

4790

Original

07-14-08

08.01.51

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

1337

1503

1712

2025

2431

2912

3488

4171

4892

7.4

1407

1579

1793

2111

2525

3016

3599

4280

4995

7.6

1479

1656

1875

2198

2619

3121

3712

4391

5099

7.8

1552

1734

1958

2284

2714

3228

3827

4504

5204

8.0

1626

1812

2040

2371

2808

3335

3944

4618

5310

8.2

1699

1890

2122

2458

2903

3442

4060

4733

5418

8.4

1772

1967

2203

2543

2997

3549

4176

4848

5527

8.6

1843

2043

2282

2628

3091

3655

4292

4964

5638

8.8

1912

2116

2360

2712

3184

3760

4406

5079

5750

9.0

1980

2187

2436

2795

3277

3865

4518

5194

5863

9.2

2047

2258

2511

2878

3370

3969

4630

5308

5978

9.4

2114

2328

2586

2961

3464

4073

4741

5422

6093

9.6

2181

2399

2663

3046

3559

4177

4852

5536

6209

9.8

2249

2472

2741

3133

3656

4282

4963

5650

6325

10.0

2318

2546

2821

3223

3755

4388

5074

5764

6441

10.2

2390

2623

2905

3316

3857

4496

5185

5878

6557

10.4

2464

2703

2993

3413

3962

4606

5298

5991

6672

10.6

2541

2788

3086

3515

4071

4719

5411

6105

6787

10.8

2622

2877

3185

3623

4185

4834

5526

6220

6901

11.0

2706

2971

3288

3734

4302

4952

5642

6334

7015

11.2

2794

3068

3395

3850

4422

5072

5759

6449

7128

11.4

2884

3169

3506

3969

4545

5194

5878

6564

7241

08.01.52

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.6

2976

3272

3620

4091

4670

5317

5997

6680

7355

11.8

3070

3377

3736

4214

4797

5442

6118

6797

7468

12.0

3166

3484

3853

4339

4925

5568

6239

6915

7583

12.2

3262

3591

3970

4464

5053

5694

6361

7033

7699

12.4

3360

3698

4088

4589

5181

5821

6484

7153

7815

12.6

3457

3806

4205

4713

5308

5948

6608

7274

7934

12.8

3554

3912

4320

4835

5435

6074

6733

7396

8054

13.0

3652

4018

4434

4956

5560

6200

6858

7519

8176

13.2

3749

4123

4547

5076

5684

6326

6983

7644

8299

13.4

3846

4228

4659

5194

5808

6452

7109

7769

8423

13.6

3943

4332

4771

5313

5931

6578

7235

7894

8548

13.8

4041

4437

4882

5431

6054

6703

7361

8020

8674

14.0

4138

4541

4994

5549

6177

6829

7488

8147

8800

14.2

4235

4646

5105

5667

6300

6954

7615

8274

8927

14.4

4333

4751

5218

5785

6423

7080

7741

8400

9054

14.6

4431

4857

5331

5905

6547

7206

7867

8527

9180

14.8

4529

4963

5445

6025

6671

7332

7994

8653

9307

15.0

4628

5071

5561

6146

6796

7458

8120

8779

9433

15.2

4728

5179

5677

6269

6921

7584

8246

8904

9558

15.4

4828

5288

5794

6392

7047

7710

8372

9030

9684

15.6

4929

5399

5913

6515

7173

7837

8497

9155

9809

15.8

5031

5510

6032

6640

7299

7963

8623

9281

9934

Original

07-14-08

08.01.53

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.0

5135

5623

6153

6765

7426

8090

8749

9406

10060

16.2

5241

5737

6274

6890

7553

8217

8875

9531

10185

16.4

5348

5852

6396

7017

7680

8343

9001

9656

10310

16.6

5457

5969

6520

7143

7807

8470

9127

9782

10435

16.8

5568

6087

6644

7270

7935

8597

9253

9908

10560

17.0

5681

6207

6769

7397

8062

8724

9379

10033

10685

17.2

5796

6327

6894

7525

8190

8851

9505

10159

10811

17.4

5911

6449

7020

7652

8317

8978

9632

10285

10936

17.6

6028

6571

7147

7780

8444

9105

9759

10411

11062

17.8

6145

6694

7274

7908

8572

9232

9885

10537

11187

18.0

6263

6817

7401

8036

8699

9359

10012

10663

11313

18.2

6381

6940

7528

8164

8827

9486

10139

10790

11439

18.4

6498

7053

7655

8292

8955

9613

10265

10916

11564

18.6

6615

7186

7782

8420

9082

9740

10392

11042

11690

18.8

6731

7308

7908

8548

9210

9867

10519

11168

11816

19.0

6846

7430

8035

8676

9337

9994

10645

11294

11941

19.2

6961

7551

8161

8804

9465

10121

10772

11420

12067

19.4

7075

7672

8287

8932

9592

10248

10898

11546

12193

19.6

7190

7793

8413

9060

9720

10375

11025

11672

12318

19.8

7305

7914

8539

9187

9847

10502

11151

11798

12444

20.0

7420

8036

8665

9315

9974

10629

11278

11924

12570

20.2

7537

8158

8791

9442

10101

10756

11404

12051

12695

08.01.54

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

20.4

7654

8280

8917

9570

10228

10882

11531

12177

12821

20.6

7772

8403

9043

9697

10355

11009

11657

12303

12947

20.8

7892

8526

9170

9824

10482

11135

11783

12429

13073

21.0

8013

8651

9296

9951

10609

11262

11910

12555

13199

21.2

8136

8776

9423

10078

10736

11388

12036

12681

13324

21.4

8259

8901

9550

10205

10862

11514

12162

12807

13450

21.6

8383

9027

9677

10332

10988

11641

12288

12933

13576

21.8

8508

9153

9804

10459

11115

11767

12414

13059

13702

22.0

8634

9280

9931

10586

11241

11893

12540

13184

13827

22.2

8760

9406

10058

10713

11368

12019

12666

13310

13953

22.4

8886

9533

10185

10840

11494

12145

12792

13436

14079

22.6

9012

9660

10312

10967

11620

12271

12918

13561

14204

22.8

9139

9787

10440

11094

11747

12397

13043

13687

14329

23.0

9265

9914

10567

11221

11873

12523

13169

13812

14454

23.2

9391

10041

10694

11347

12000

12649

13295

13937

14579

23.4

9518

10168

10821

11474

12126

12775

13420

14063

14704

23.6

9644

10295

10948

11601

12253

12901

13546

14188

14829

23.8

9770

10421

11075

11728

12380

13027

13671

14313

14954

24.0

9897

10548

11202

11855

12506

13153

13797

14438

15078

24.2

10023

10675

11329

11982

12632

13279

13922

14563

15203

24.4

10150

10802

11456

12108

12759

13405

14048

14688

15328

24.6

10276

10929

11582

12235

12885

13531

14174

14813

15452

Original

07-14-08

08.01.55

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

24.8

10422

11055

11709

12362

13011

13657

14299

14939

15577

25.0

10529

11182

11836

12488

13137

13783

14425

15064

15702

25.2

10655

11309

11963

12615

13263

13909

14551

15189

15826

25.4

10781

11436

12089

12741

13389

14035

14676

15315

15951

25.6

10908

11562

12216

12867

13515

14161

14802

15440

16076

25.8

11034

11689

12343

12993

13641

14286

14928

15565

16201

26.0

11161

11816

12469

13120

13767

14412

15053

15690

16325

26.2

11287

11942

12596

13246

13893

14538

15179

15815

16450

26.4

11414

12069

12722

13372

14018

14663

15304

15941

16575

26.6

11540

12195

12848

13498

14144

14788

15429

16065

16700

26.8

11667

12321

12974

13623

14269

14914

15554

16190

16824

27.0

11793

12448

13101

13749

14395

15039

15679

16315

16949

27.2

11920

12574

13227

13875

14521

15164

15804

16440

17073

27.4

12047

12700

13353

14001

14646

15289

15929

16564

17198

27.6

12173

12827

13479

14127

14771

15414

16053

16689

17322

27.8

12300

12953

13605

14252

14897

15539

16178

16813

17447

28.0

12426

13079

13731

14378

15022

15664

16302

16937

17571

28.2

12553

13206

13857

14504

15148

15789

16427

17062

17695

28.4

12680

13332

13983

14630

15273

15914

16551

17186

17819

28.6

12807

13458

14109

14756

15399

16039

16676

17310

17943

28.8

12933

13585

14235

14882

15524

16164

16800

17434

18067

29.0

13060

13711

14361

15008

15650

16289

16925

17559

18191

08.01.56

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

29.2

13187

13838

14488

15133

15775

16414

17050

17683

18315

29.4

13314

13964

14614

15259

15901

16539

17174

17807

18439

29.6

13440

14091

14740

15385

16027

16664

17299

17931

18562

29.8

13567

14217

14866

15511

16152

16789

17424

18055

18686

30.0

13694

14344

14992

15637

16277

16915

17548

18180

18810

30.2

13820

14470

15118

15762

16403

17039

17673

18304

18933

30.4

13946

14596

15244

15888

16528

17164

17798

18428

19057

30.6

14073

14722

15370

16013

16653

17289

17922

18552

19181

30.8

14199

14848

15495

16138

16778

17414

18047

18676

19305

31.0

14325

14974

15621

16263

16902

17538

18171

18801

19429

31.2

14451

15099

15746

16388

17027

17663

18295

18925

19553

31.4

14577

15225

15871

16513

17152

17787

18420

19049

19677

31.6

14703

15350

15996

16638

17276

17912

18544

19173

19801

31.8

14829

15476

16121

16763

17401

18036

18668

19297

19925

32.0

14955

15601

16246

16887

17525

18160

18792

19421

20048

32.2

15080

15727

16371

17012

17649

18284

18916

19545

20172

32.4

15206

15852

16496

17137

17774

18408

19040

19668

20295

32.6

15332

15977

16621

17261

17898

18532

19164

19792

20418

32.8

15457

16103

16746

17386

18023

18657

19288

19915

20541

33.0

15583

16228

16871

17511

18147

18781

19411

20039

20664

33.2

15709

16353

16996

17636

18272

18905

19535

20162

20786

33.4

15834

16479

17122

17761

18396

19029

19654

20285

20908

Original

07-14-08

08.01.57

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

33.6

15960

16604

17247

17886

18521

19153

19782

20408

21030

33.8

16086

16729

17372

18010

18645

19277

19906

20531

21152

34.0

16211

16855

17497

18135

18770

19401

20029

20654

21274

34.2

16337

16980

17622

18260

18895

19526

20153

20777

21396

34.4

16463

17105

17747

18385

19019

19650

20277

20900

21518

34.6

16588

17231

17872

18510

19143

19774

20401

21023

21639

34.8

16714

17356

17997

18634

19268

19898

20525

21146

21761

35.0

16840

17481

18122

18759

19392

20022

20648

21269

21883

35.2

16965

17607

18247

18883

19516

20146

20772

21392

22005

35.4

17091

17732

18372

19007

19640

20271

20896

21515

22127

35.6

17216

17857

18496

19132

19764

20395

21020

21638

22249

35.8

17342

17982

18621

19256

19888

20519

21144

21762

22370

36.0

17467

18107

18746

19380

20012

20642

21268

21884

22492

36.2

17592

18232

18870

19504

20136

20766

21391

22007

22614

36.4

17717

18357

18995

19628

20259

20890

21514

22130

22735

36.6

17843

18481

19119

19752

20383

21013

21637

22252

22857

36.8

17967

18606

19243

19876

20507

21136

21760

22374

22978

37.0

18092

18730

19367

20000

20630

21259

21882

22496

23099

37.2

18217

18855

19491

20124

20754

21382

22004

22617

23219

37.4

18342

18979

19615

20248

20877

21505

22126

22739

23339

37.6

18466

19103

19739

20372

21001

21628

22248

22859

23459

37.8

18591

19227

19864

20495

21124

21750

22370

22980

23578

08.01.58

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

38.0

18715

19352

19988

20619

21248

21873

22492

23100

23695

38.2

18840

19476

20112

20743

21371

21996

22614

23219

23812

38.4

18965

19600

20236

20867

21495

22120

22736

23338

23928

38.6

19089

19725

20360

20991

21619

22243

22857

23457

24042

38.8

19214

19849

20484

21115

21743

22367

22979

23575

24156

39.0

19339

19974

20609

21239

21867

22490

23102

23693

24268

39.2

19464

20098

20733

21364

21991

22614

23224

23810

24379

39.4

19589

20223

20857

21488

22115

22738

23346

23928

24490

39.6

19714

20348

20982

21612

22238

22862

23468

24044

24600

39.8

19834

20472

21106

21735

22362

22986

23590

24161

24710

40.0

19963

20596

21230

21859

22486

23109

23712

24278

24820

40.2

20088

20721

21354

21982

22609

23232

23833

24394

24930

40.4

20212

20845

21478

22106

22732

23355

23954

24511

25040

40.6

20336

20969

21601

22228

22854

23477

24075

24627

25152

40.8

20460

21092

21724

22351

22976

23599

24195

24744

25264

41.0

20584

21215

21847

22473

23098

23720

24315

24860

25377

41.2

20707

21339

21970

22595

23219

23841

24434

24977

25490

41.4

20831

21462

22092

22717

23341

23961

24553

25093

25604

41.6

20954

21585

22215

22839

23462

24081

24671

25208

25716

41.8

21077

21707

22337

22961

23583

24201

24788

25322

25828

42.0

21200

21830

22460

23083

23704

24320

24904

25435

25939

42.2

21323

21953

22582

23206

23825

24438

25019

25547

26048

Original

07-14-08

08.01.59

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

42.4

21446

22075

22705

23328

23947

24557

25133

25658

26156

42.6

21568

22198

22827

23451

24069

24675

25246

25767

26261

42.8

21691

22320

22950

23574

24191

24792

25358

25874

26364

43.0

21814

22443

23073

23698

24313

24910

25470

25979

26464

43.2

21937

22565

23196

23822

24435

25027

25580

26084

26563

43.4

22059

22688

23319

23945

24558

25144

25690

26187

26659

43.6

22182

22810

23442

24069

24680

25261

25800

26289

26754

43.8

22305

22933

23564

24192

24801

25378

25910

26391

26848

44.0

22427

23055

23687

24314

24923

25495

26020

26493

26941

44.2

22550

23178

23809

24436

25043

25612

26130

26595

27033

44.4

22673

23300

23931

24557

25163

25729

26242

26697

27125

44.6

22795

23422

24053

24678

25282

25846

26354

26800

27216

44.8

22918

23544

24174

24797

25400

25963

26468

26904

27308

45.0

23040

23666

24294

24915

25516

26080

26582

27009

27399

45.2

23162

23787

24414

25032

25632

26197

26696

27113

27491

45.4

23284

23908

24533

25148

25746

26312

26810

27218

27582

45.6

23405

24028

24652

25264

25860

26427

26923

27322

27673

45.8

23525

24148

24769

25378

25972

26540

27035

27425

27764

46.0

23645

24266

24886

25491

26083

26652

27145

27527

27855

46.2

23763

24384

25002

25603

26193

26761

27253

27628

27946

46.4

23880

24500

25116

25715

26301

26868

27357

27726

28036

46.6

23996

24615

25230

25826

26409

26973

27458

27822

28127

08.01.60

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

46.8

24110

24729

25342

25936

26515

27075

27556

27916

28217

47.0

24223

24841

25454

26045

26620

27174

27650

28007

28306

47.2

24335

24953

25565

26154

26725

27272

27741

28096

28394

47.4

24447

25064

25675

26263

26829

27368

27829

28182

28480

47.6

24558

25174

25785

26372

26933

27463

27916

28266

28565

47.8

24668

25284

25895

26481

27037

27557

28001

28348

28646

48.0

24779

25395

26006

26590

27142

27651

28086

28428

28724

48.2

24890

25506

26117

26700

27247

27746

28169

28506

28799

48.4

25001

25617

26229

26811

27353

27841

28253

28582

28870

48.6

25113

25730

26342

26923

27460

27937

28337

28656

28936

48.8

25226

25843

26456

27037

27568

28036

28423

28729

28997

49.0

25340

25957

26571

27151

27677

28135

28509

28801

29053

49.2

25454

26072

26686

27264

27786

28235

28595

28871

29106

49.4

25568

26186

26801

27378

27895

28334

28681

28940

29156

49.6

25681

26300

26915

27490

28002

28434

28768

29008

29204

49.8

25794

26413

27028

27600

28108

28532

28854

29075

29250

50.0

25906

26525

27138

27708

28211

28629

28939

29142

29295

50.2

26016

26634

27247

27812

28311

28723

29023

29208

29341

50.4

26125

26742

27352

27913

28407

28815

29106

29275

29386

50.6

26231

26846

27454

28010

28499

28903

29187

29340

29434

50.8

26335

26948

27551

28102

28586

28988

29267

29406

29482

51.0

26437

27047

27645

28189

28668

29069

29344

29472

29533

Original

07-14-08

08.01.61

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

51.2

26537

27143

27736

28273

28747

29147

29419

29537

29584

51.4

26635

27237

27825

28355

28823

29221

29491

29600

29636

51.6

26732

27329

27911

28434

28896

29293

29561

29662

29688

51.8

26827

27420

27997

28512

28968

29363

29627

29722

29740

52.0

26922

27510

28081

28589

29039

29430

29691

29779

29791

52.2

27015

27599

28164

28666

29110

29495

29751

29833

29840

52.4

27108

27687

28248

28745

29182

29559

29807

29884

29888

52.6

27200

27776

28333

28825

29254

29621

29859

29932

29933

52.8

27292

27865

28418

28907

29329

29682

29908

29975

29975

53.0

27384

27954

28505

28991

29404

29742

29953

30014

30015

53.2

27476

28043

28592

29076

29481

29801

29995

30051

30053

53.4

27568

28131

28679

29161

29558

29859

30035

30085

30088

53.6

27659

28220

28766

29247

29635

29916

30074

30117

30122

53.8

27750

28309

28853

29332

29711

29972

30111

30148

30154

54.0

27842

28397

28939

29416

29786

30028

30148

30179

30185

08.01.62

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

489

542

616

763

999

1338

1789

2358

2966

3.2

522

577

653

802

1047

1404

1873

2451

3063

3.4

555

613

690

843

1096

1470

1957

2543

3159

3.6

589

649

729

885

1146

1537

2041

2635

3256

3.8

622

686

769

928

1198

1605

2124

2727

3352

4.0

656

723

809

974

1253

1673

2206

2817

3448

4.2

690

761

852

1023

1310

1743

2288

2907

3545

4.4

724

800

896

1074

1370

1813

2368

2997

3641

4.6

759

840

942

1129

1434

1885

2448

3085

3738

4.8

795

880

991

1188

1502

1959

2527

3172

3834

5.0

831

923

1041

1249

1574

2034

2605

3258

3931

5.2

868

967

1094

1315

1649

2111

2684

3344

4027

5.4

908

1013

1150

1383

1727

2190

2763

3431

4124

5.6

949

1061

1208

1454

1808

2272

2844

3518

4222

5.8

993

1113

1269

1529

1892

2356

2927

3607

4319

6.0

1040

1167

1333

1605

1978

2443

3012

3697

4418

6.2

1090

1224

1400

1685

2067

2532

3101

3789

4516

6.4

1144

1286

1470

1766

2157

2624

3193

3884

4615

6.6

1202

1351

1544

1850

2249

2720

3290

3983

4715

6.8

1264

1420

1621

1935

2343

2819

3392

4084

4816

7.0

1331

1493

1701

2023

2437

2921

3498

4189

4918

Original

07-14-08

08.01.63

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

1400

1569

1783

2111

2533

3026

3608

4297

5020

7.4

1473

1647

1867

2200

2630

3132

3721

4407

5124

7.6

1547

1727

1952

2290

2727

3240

3837

4520

5228

7.8

1622

1808

2037

2381

2824

3349

3954

4634

5334

8.0

1698

1889

2123

2471

2921

3459

4072

4749

5441

8.2

1775

1970

2208

2561

3019

3569

4191

4865

5550

8.4

1850

2049

2292

2650

3116

3678

4309

4982

5660

8.6

1924

2128

2375

2738

3212

3787

4427

5098

5771

8.8

1996

2204

2455

2824

3308

3895

4543

5215

5884

9.0

2067

2278

2535

2911

3404

4002

4658

5331

5998

9.2

2137

2352

2613

2996

3499

4108

4772

5446

6114

9.4

2206

2425

2691

3083

3596

4214

4885

5562

6230

9.6

2276

2499

2771

3171

3693

4320

4998

5678

6347

9.8

2346

2574

2852

3261

3793

4427

5111

5793

6464

10.0

2418

2651

2935

3353

3894

4536

5223

5908

6582

10.2

2491

2730

3021

3448

3998

4645

5336

6024

6699

10.4

2567

2812

3111

3547

4105

4757

5450

6139

6816

10.6

2646

2899

3206

3651

4216

4871

5564

6255

6933

10.8

2728

2990

3306

3760

4331

4987

5680

6370

7049

11.0

2814

3085

3410

3873

4449

5106

5797

6486

7164

11.2

2902

3183

3519

3989

4571

5226

5915

6602

7279

11.4

2993

3285

3631

4109

4695

5349

6034

6719

7394

08.01.64

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.6

3086

3389

3745

4232

4821

5473

6154

6836

7509

11.8

3181

3495

3862

4356

4948

5598

6275

6954

7625

12.0

3277

3602

3980

4482

5076

5724

6396

7072

7741

12.2

3374

3710

4098

4607

5205

5850

6519

7191

7858

12.4

3472

3819

4217

4733

5334

5977

6642

7312

7975

12.6

3570

3927

4334

4858

5462

6104

6766

7433

8095

12.8

3669

4035

4451

4981

5589

6231

6890

7556

8215

13.0

3767

4142

4566

5103

5715

6357

7016

7679

8337

13.2

3865

4248

4681

5224

5840

6484

7141

7803

8460

13.4

3963

4355

4795

5344

5964

6610

7267

7928

8585

13.6

4062

4461

4908

5464

6088

6736

7393

8054

8709

13.8

4160

4567

5021

5583

6212

6862

7520

8180

8835

14.0

4259

4673

5134

5702

6335

6988

7646

8306

8961

14.2

4357

4779

5247

5821

6459

7113

7773

8433

9087

14.4

4456

4885

5361

5941

6583

7239

7900

8559

9214

14.6

4555

4992

5476

6061

6707

7365

8026

8686

9340

14.8

4654

5100

5592

6183

6832

7492

8153

8812

9466

15.0

4754

5208

5708

6305

6957

7618

8279

8938

9592

15.2

4854

5318

5825

6428

7083

7744

8405

9064

9718

15.4

4955

5428

5944

6551

7209

7871

8531

9189

9843

15.6

5057

5539

6063

6675

7335

7997

8657

9315

9969

15.8

5160

5651

6183

6800

7462

8124

8783

9440

10094

Original

07-14-08

08.01.65

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.0

5264

5764

6304

6925

7589

8250

8909

9566

10219

16.2

5371

5879

6426

7051

7716

8377

9035

9691

10344

16.4

5479

5995

6549

7178

7843

8504

9161

9816

10470

16.6

5589

6112

6673

7304

7970

8631

9287

9942

10595

16.8

5701

6231

6797

7431

8097

8758

9413

10068

10720

17.0

5815

6352

6923

7558

8225

8885

9539

10193

10846

17.2

5931

6473

7048

7686

8352

9011

9666

10319

10971

17.4

6048

6595

7175

7813

8479

9138

9792

10445

11097

17.6

6165

6719

7302

7941

8607

9265

9919

10571

11222

17.8

6284

6842

7429

8069

8734

9392

10045

10698

11348

18.0

6403

6966

7556

8197

8861

9519

10172

10824

11473

18.2

6522

7090

7683

8325

8989

9646

10298

10950

11599

18.4

6641

7214

7811

8453

9116

9773

10425

11076

11725

18.6

6759

7337

7938

8581

9244

9900

10552

11202

11850

18.8

6877

7460

8065

8709

9371

10027

10678

11328

11976

19.0

6993

7583

8192

8837

9498

10154

10805

11454

12101

19.2

7110

7705

8318

8965

9626

10281

10932

11580

12227

19.4

7226

7827

8445

9092

9753

10408

11058

11706

12353

19.6

7342

7949

8571

9220

9880

10535

11185

11832

12478

19.8

7458

8071

8697

9348

10008

10662

11311

11958

12604

20.0

7575

8193

8824

9475

10135

10789

11438

12084

12730

20.2

7629

8316

8950

9603

10262

10916

11564

12210

12855

08.01.66

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

20.4

7811

8439

9076

9730

10389

11042

11691

12336

12981

20.6

7930

8562

9203

9857

10516

11169

11817

12462

13107

20.8

8050

8686

9329

9984

10643

11295

11943

12588

13233

21.0

8172

8811

9456

10112

10769

11422

12069

12715

13358

21.2

8295

8936

9583

10239

10896

11548

12196

12841

13484

21.4

8418

9061

9710

10366

11022

11674

12322

12966

13610

21.6

8542

9187

9837

10492

11149

11800

12448

13092

13736

21.8

8667

9313

9964

10619

11275

11926

12574

13218

13861

22.0

8793

9440

10091

10746

11401

12053

12700

13344

13987

22.2

8919

9566

10218

10873

11528

12179

12826

13470

14112

22.4

9045

9693

10345

11000

11654

12305

12952

13595

14238

22.6

9171

9820

10472

11127

11780

12431

13077

13721

14363

22.8

9298

9947

10600

11254

11907

12557

13203

13846

14488

23.0

9424

10074

10727

11380

12033

12683

13329

13972

14613

23.2

9551

10201

10854

11507

12160

12809

13454

14097

14738

23.4

9677

10328

10981

11634

12286

12935

13580

14222

14863

23.6

9803

10454

11108

11761

12413

13061

13705

14347

14988

23.8

9930

10581

11235

11888

12539

13187

13831

14472

15113

24.0

10056

10708

11362

12015

12666

13313

13956

14597

15238

24.2

10183

10835

11489

12141

12792

13439

14082

14723

15362

24.4

10309

10962

11615

12268

12918

13565

14207

14848

15487

24.6

10436

11089

11742

12395

13045

13691

14333

14973

15612

Original

07-14-08

08.01.67

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

24.8

10562

11215

11869

12521

13171

13817

14459

15098

15736

25.0

10688

11342

11996

12648

13297

13942

14584

15223

15861

25.2

10815

11469

12123

12774

13423

14068

14710

15348

15986

25.4

10941

11596

12249

12901

13549

14194

14836

15474

16110

25.6

11068

11722

12375

13027

13675

14320

14962

15599

16235

25.8

11194

11849

12503

13153

13801

14446

15087

15724

16360

26.0

11321

11975

12629

13279

13926

14571

15213

15849

16484

26.2

11447

12102

12755

13405

14052

14697

15338

15975

16609

26.4

11574

12229

12882

13531

14178

14822

15464

16100

16734

26.6

11700

12355

13008

13657

14303

14948

15589

16225

16858

26.8

11827

12481

13134

13783

14429

15073

15714

16349

16983

27.0

11953

12608

13260

13909

14554

15198

15839

16474

17108

27.2

12080

12734

13386

14035

14680

15323

15963

16599

17232

27.4

12206

12860

13512

14160

14805

15448

16088

16723

17357

27.6

12333

12987

13638

14286

14931

15573

16213

16848

17481

27.8

12460

13113

13764

14412

15056

15698

16337

16972

17606

28.0

12586

13239

13890

14538

15181

15823

16461

17096

17730

28.2

12713

13365

11401 6

14663

15307

15948

16586

17221

17854

28.4

12839

13492

14142

14789

15432

16073

16710

17345

17978

28.6

12966

13618

14268

14915

15558

16198

16835

17469

18102

28.8

13093

13744

14395

15041

15683

16323

16959

17593

18226

29.0

13220

13871

14521

15167

15809

16448

17084

17717

18350

08.01.68

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

29.2

13346

13997

14647

15293

15935

16573

17209

17842

18473

29.4

13473

14124

14773

15418

16060

16698

17333

17966

18597

29.6

13600

14250

14899

15544

16186

16823

17458

18090

18721

29.8

13725

14376

15025

15670

16311

16948

17583

18214

18844

30.0

13853

14503

15151

15796

16436

17073

17707

18338

18968

30.2

13979

14629

15277

15921

16562

17198

17832

18462

19092

30.4

14106

14755

15403

16047

16687

17323

17956

18587

19215

30.6

14232

14881

15529

16172

16812

17448

18081

18711

19339

30.8

14358

15007

15654

16297

16937

17572

18205

18835

19463

31.0

14484

15133

15780

16422

17061

17697

18330

18959

19587

31.2

14610

15258

15905

16547

17186

17821

18454

19083

19711

31.4

14736

15384

16030

16672

17310

17946

18578

19208

19836

31.6

14862

15509

16155

16797

17435

18070

18703

19332

19960

31.8

14989

15635

16280

16921

17559

18194

18827

19456

20083

32.0

15114

15760

16405

17046

17684

18319

18951

19580

20207

32.2

15239

15886

16530

17171

17808

18443

19075

19703

20331

32.4

15365

16011

16655

17295

17932

18567

19199

19827

20454

32.6

15491

16136

16780

17420

18057

18691

19322

19950

20576

32.8

15616

16261

16905

17545

18181

18815

19446

20074

20699

33.0

15742

16387

17030

17669

18306

18939

19570

20196

20821

33.2

15868

16512

17155

17794

18430

19063

19693

20319

20943

33.4

15993

16637

17280

17919

18555

19187

19817

20442

21064

Original

07-14-08

08.01.69

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

33.6

16119

16763

17405

18044

18679

19312

19940

20565

21185

33.8

16244

16888

17530

18169

18804

19436

20064

20687

21306

34.0

16370

17013

17656

18294

18928

19560

20187

20810

21427

34.2

16496

17139

17781

18418

19053

19684

20311

20932

21548

34.4

16621

17264

17906

18543

19177

19808

20435

21055

21669

34.6

16747

17389

18031

18668

19301

19933

20558

21177

21790

34.8

16873

17515

18156

18792

19426

20057

20682

21300

21910

35.0

16998

17640

18281

18917

19550

20181

20806

21423

22031

35.2

17124

17765

18405

19041

19674

20306

20931

21545

22152

35.4

17249

17890

18530

19165

19798

20430

21055

21668

22273

35.6

17375

18015

18655

19290

19922

20554

21178

21791

22394

35.8

17500

18141

18780

19414

20046

20678

21302

21913

22514

36.0

17625

18265

18904

19538

20170

20802

21426

22036

22635

36.2

17751

18390

19029

19662

20294

20925

21549

22158

22756

36.4

17876

18515

19153

19786

20417

21049

21672

22280

22876

36.6

18001

18640

19277

19910

20541

21172

21795

22402

22997

36.8

18126

18764

19401

20034

20664

21295

21917

22523

23117

37.0

18250

18889

19526

20158

20788

21418

22039

22644

23237

37.2

18375

19013

19650

20281

20911

21540

22160

22765

23357

37.4

18500

19137

19774

20405

21035

21663

22282

22885

23476

37.6

18624

19261

19898

20529

21158

21785

22403

23005

23594

37.8

18749

19385

20021

20653

21281

21908

22524

23124

23712

08.01.70

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

38.0

18873

19510

20146

20777

21405

22030

22645

23243

23829

38.2

18998

19634

20270

20901

21529

22153

22766

23362

23944

38.4

19122

19758

20394

21025

21652

22276

22887

23480

24059

38.6

19247

19883

20518

21149

21776

22399

23008

23597

24171

38.8

19372

20007

20642

21273

21900

22522

23129

23714

24283

39.0

19497

20132

20767

21398

22024

22646

23251

23830

24393

39.2

19622

20257

20891

21522

22148

22769

23372

23946

24502

39.4

19747

20381

21016

21646

22272

22893

23494

24062

24611

39.6

19872

20506

21140

21770

22396

23017

23616

24178

24718

39.8

19997

20630

21264

21894

22519

23140

23737

24293

24826

40.0

20121

20755

21388

22017

22642

23263

23858

24408

24934

40.2

20246

20879

21512

22141

22765

23386

23979

24523

25042

40.4

20370

21003

21636

22264

22887

23508

24099

24638

25150

40.6

20494

21126

21759

22386

23009

23630

24219

24753

25259

40.8

20617

21249

21882

22508

23130

23751

24339

24868

25369

41.0

20740

21372

22004

22629

23251

23871

24458

24983

25480

41.2

20863

21495

22126

22751

23371

23991

24576

25097

25591

41.4

20985

21617

22248

22872

23491

24110

24693

25212

25701

41.6

21108

21739

22370

22992

23611

24228

24810

25325

25812

41.8

21231

21861

22491

23113

23731

24346

24925

25438

25922

42.0

21353

21983

22613

23234

23851

24464

25040

25549

26030

42.2

21474

22105

22734

23356

23971

24581

25153

25659

26138

Original

07-14-08

08.01.71

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

42.4

21596

22227

22856

23477

24091

24698

25266

25768

26243

42.6

21718

22348

22977

23599

24212

24814

25376

25874

26346

42.8

21840

22470

23099

23721

24333

24930

25486

25979

26447

43.0

21961

22591

23221

23844

24454

25045

25594

26082

26546

43.2

22083

22713

23343

23967

24576

25160

25702

26184

26643

43.4

22205

22835

23465

24090

24697

25275

25809

26284

26737

43.6

22326

22956

23587

24212

24818

25390

25916

26384

26831

43.8

22448

23078

23709

24335

24939

25505

26022

26484

26923

44.0

22570

23199

23831

24457

25059

25620

26129

26583

27013

44.2

22691

23320

23952

24578

25179

25734

26237

26682

27103

44.4

22813

23442

24073

24698

25297

25849

26345

26781

27193

44.6

22934

23563

24194

24817

25414

25964

26455

26881

27282

44.8

23056

23684

24314

24935

25530

26078

26565

26982

27371

45.0

23178

23805

24433

25052

25645

26193

26677

27084

27459

45.2

23299

23925

24552

25168

25758

26306

26788

27186

27548

45.4

23419

24045

24670

25282

25870

26419

26900

27287

27636

45.6

23539

24165

24788

25396

25981

26531

27010

27389

27724

45.8

23659

24283

24904

25508

26091

26642

27120

27489

27813

46.0

23777

24400

25019

25619

26199

26750

27227

27588

27901

46.2

23894

24516

25133

25729

26305

26857

27332

27686

27989

46.4

24009

24631

25246

25838

26411

26961

27434

27782

28077

46.6

24124

24744

25358

25946

26515

27063

27533

27876

28165

08.01.72

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

46.8

24236

24856

25468

26053

26618

27161

27628

27967

28253

47.0

24348

24966

25577

26159

26720

27258

27719

28056

28341

47.2

24458

25076

25685

26265

26821

27352

27807

28143

28427

47.4

24567

25184

25792

26370

26921

27444

27893

28227

28512

47.6

24676

25292

25899

26475

27022

27536

27976

28309

28595

47.8

24784

25400

26006

26581

27122

27626

28058

28389

28675

48.0

24892

25507

26114

26686

27223

27717

28139

28467

28753

48.2

25001

25615

26222

26793

27324

27808

28220

28543

28826

48.4

25110

25724

26330

26900

27427

27900

28301

28617

28896

48.6

25220

25834

26440

27009

27530

27992

28382

28689

28961

48.8

25330

25945

26551

27119

27635

28087

28463

28760

29021

49.0

25442

26056

26663

27229

27741

28182

28546

28829

29076

49.2

25553

26168

26775

27340

27847

28279

28629

28897

29128

49.4

25665

26280

26886

27450

27952

28375

28712

28963

29177

49.6

25776

26391

26998

27559

28056

28471

28795

29029

29224

49.8

25887

26501

27107

27666

28159

28565

28878

29094

29269

50.0

25996

26610

27215

27771

28258

28659

28960

29159

29313

50.2

26105

26718

27321

27873

28355

28750

29042

29223

29357

50.4

26211

26823

27423

27971

28448

28839

29122

29287

29401

50.6

26316

26925

27522

28064

28537

28924

29201

29351

29447

50.8

26418

27024

27617

28153

28620

29006

29279

29415

29494

51.0

26518

27121

27709

28238

28699

29085

29355

29479

29543

Original

07-14-08

08.01.73

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

51.2

26615

27215

27798

28319

28775

29160

29428

29542

29593

51.4

26712

27307

27884

28397

28847

29232

29499

29604

29643

51.6

26806

27397

27969

28474

28918

29302

29568

29665

29694

51.8

26900

27485

28051

28549

28986

29370

29634

29723

29744

52.0

26992

27573

28133

28623

29054

29435

29696

29780

29794

52.2

27083

27659

28214

28697

29122

29498

29755

29833

29842

52.4

27173

27745

28295

28772

29191

29560

29811

29884

29888

52.6

27263

27831

28377

28849

29260

29620

29862

29930

29933

52.8

27353

27917

28459

28927

29332

29679

29910

29973

29975

53.0

27443

28003

28542

29008

29405

29737

29954

30012

30014

53.2

27532

28089

28625

29089

29479

29794

29994

30048

30052

53.4

27621

28175

28709

29171

29554

29850

30033

30082

30087

53.6

27710

28261

28793

29253

29628

29905

30070

30114

30121

53.8

27799

28346

28876

29335

29703

29960

30106

30145

30153

54.0

27887

28431

28958

29416

29776

30014

30141

30175

30184

FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

3.0 08.01.74

524

-1.50 581

-1.00 661

-.50 814

0.00 1061

07-14-08

.50 1413

1.00 1882

1.50 2457

2.00 3068 Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.2

558

618

700

855

1111

1481

1967

2552

3167

3.4

593

656

739

897

1163

1550

2053

2646

3265

3.6

628

693

780

941

1215

1619

2138

2740

3363

3.8

663

732

821

987

1270

1688

2223

2833

3461

4.0

698

771

864

1035

1327

1759

2307

2926

3559

4.2

734

811

908

1086

1387

1831

2391

3018

3657

4.4

770

851

955

1139

1450

1904

2474

3109

3755

4.6

807

893

1003

1196

1516

1979

2556

3199

3852

4.8

844

936

1054

1257

1586

2055

2638

3288

3950

5.0

882

980

1107

1321

1660

2134

2719

3376

4048

5.2

921

1027

1162

1389

1737

2214

2801

3465

4145

5.4

963

1075

1220

1460

1818

2296

2884

3553

4243

5.6

1006

1126

1281

1534

1901

2380

2967

3642

4341

5.8

1051

1179

1345

1611

1987

2467

3053

3732

4439

6.0

1100

1235

1412

1691

2076

2557

3141

3824

4538

6.2

1152

1295

1482

1773

2167

2649

3233

3918

4637

6.4

1208

1358

1555

1857

2260

2744

3328

4015

4738

6.6

1268

1426

1631

1943

2354

2842

3426

4115

4838

6.8

1332

1497

1710

2032

2451

2944

3530

4218

4940

7.0

1401

1572

1792

2122

2548

3048

3637

4324

5043

7.2

1472

1650

1877

2213

2647

3154

3748

4433

5147

7.4

1546

1730

1963

2305

2746

3263

3862

4544

5252

Original

07-14-08

08.01.75

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.6

1622

1812

2050

2398

2847

3373

3978

4657

5358

7.8

1699

1895

2138

2491

2947

3484

4096

4772

5465

8.0

1777

1978

2226

2584

3048

3595

4214

4888

5574

8.2

1855

2061

2314

2677

3149

3707

4333

5005

5684

8.4

1932

2142

2400

2769

3249

3819

4452

5122

5795

8.6

2008

2222

2485

2860

3349

3929

4571

5240

5908

8.8

2081

2300

2568

2949

3448

4039

4687

5357

6022

9.0

2154

2377

2649

3038

3547

4148

4803

5474

6138

9.2

2225

2452

2730

3127

3645

4256

4918

5591

6254

9.4

2296

2528

2811

3217

3745

4365

5032

5707

6372

9.6

2367

2603

2892

3307

3845

4473

5146

5824

6490

9.8

2439

2680

2975

3400

3947

4582

5260

5940

6609

10.0

2512

2759

3061

3494

4051

4692

5374

6057

6727

10.2

2587

2840

3149

3592

4157

4804

5488

6173

6846

10.4

2665

2924

3241

3693

4266

4917

5603

6290

6964

10.6

2745

3013

3338

3799

4378

5032

5719

6406

7082

10.8

2829

3105

3440

3909

4494

5149

5835

6523

7199

11.0

2916

3202

3546

4023

4613

5268

5953

6640

7316

11.2

3006

3302

3657

4141

4734

5389

6072

6757

7432

11.4

3099

3406

3770

4262

4858

5512

6192

6875

7548

11.6

3193

3511

3886

4385

4984

5636

6313

6993

7664

11.8

3289

3619

4004

4510

5110

5761

6434

7112

7781

08.01.76

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

12.0

3387

3728

4124

4635

5238

5887

6557

7231

7898

12.2

3486

3837

4244

4762

5366

6013

6680

7351

8015

12.4

3585

3947

4364

4888

5494

6140

6803

7472

8134

12.6

3684

4057

4483

5013

5622

6267

6928

7594

8254

12.8

3784

4166

4601

5137

5749

6393

7052

7717

8375

13.0

3883

4274

4717

5259

5874

6519

7178

7841

8498

13.2

3982

4382

4833

5381

5999

6645

7303

7965

8621

13.4

4082

4490

4948

5501

6124

6771

7429

8090

8746

13.6

4181

4597

5062

5622

6248

6897

7555

8216

8871

13.8

4280

4704

5176

5741

6371

7023

7682

8342

8996

14.0

4380

4811

5291

5861

6495

7149

7808

8468

9122

14.2

4479

4918

5405

5981

6619

7274

7934

8594

9249

14.4

4579

5026

5520

6101

6743

7400

8061

8721

9375

14.6

4679

5134

5635

6222

6867

7526

8187

8847

9501

14.8

4779

5243

5752

6344

6992

7652

8314

8973

9627

15.0

4880

5352

5869

6467

7117

7778

8440

9099

9753

15.2

4981

5462

5987

6590

7242

7905

8566

9225

9879

15.4

5083

5573

6106

6714

7368

8031

8692

9350

10004

15.6

5186

5685

6226

6838

7495

8157

8817

9476

10129

15.8

5291

5799

6347

6963

7621

8284

8943

9601

10255

16.0

5397

5913

6468

7089

7748

8411

9069

9726

10380

16.2

5504

6028

6590

7215

7875

8537

9195

9852

10505

Original

07-14-08

08.01.77

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.4

5613

6145

6713

7341

8002

8664

9321

9977

10630

16.6

5724

6263

6837

7468

8130

8791

9447

10103

10755

16.8

5838

6383

6962

7595

8257

8918

9573

10228

10880

17.0

5953

6504

7087

7722

8384

9044

9700

10354

11006

17.2

6070

6625

7213

7849

8511

9171

9826

10480

11131

17.4

6188

6749

7339

7977

8639

9298

9952

10606

11257

17.6

6307

6872

7466

8104

8766

9425

10079

10732

11382

17.8

6427

6996

7593

8232

8893

9552

10205

10858

11508

18.0

6547

7120

7720

8360

9021

9679

10332

10984

11633

18.2

6667

7244

7847

8487

9148

9806

10459

11110

11759

18.4

6787

7369

7974

8615

9276

9933

10585

11236

11884

18.6

6907

7493

8101

8743

9403

10060

10712

11362

12010

18.8

7025

7616

8227

8871

9530

10187

10839

11488

12136

19.0

7143

7739

8354

8998

9658

10314

10965

11614

12261

19.2

7261

7862

8480

9126

9785

10441

11092

11740

12387

19.4

7378

7984

8607

9253

9913

10568

11218

11866

12512

19.6

7495

8107

8733

9381

10040

10695

11345

11992

12638

19.8

7613

8229

8859

9508

10167

10822

11471

12118

12764

20.0

7731

8352

8985

9636

10294

10948

11598

12244

12889

20.2

7849

8475

9111

9763

10421

11075

11724

12370

13015

20.4

7969

8598

9237

9890

10548

11202

11850

12496

13141

20.6

8089

8722

9364

10017

10675

11328

11977

12622

13266

08.01.78

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

20.8

8210

8846

9490

10144

10802

11455

12103

12748

13392

21.0

8332

8971

9617

10271

10929

11581

12229

12874

13518

21.2

8455

9096

9744

10398

11055

11708

12355

13000

13644

21.4

8579

9222

9870

10525

11182

11834

12481

13126

13769

21.6

8704

9348

9997

10652

11308

11960

12607

13252

13895

21.8

8829

9474

10124

10779

11434

12086

12733

13378

14021

22.0

8955

9601

10251

10906

11561

12212

12859

13504

14146

22.2

9081

9727

10378

11033

11687

12338

12985

13629

14272

22.4

9207

9854

10505

11160

11813

12464

13111

13755

14397

22.6

9333

9981

10633

11286

11940

12590

13237

13880

14523

22.8

9459

10108

10760

11413

12066

12716

13362

14006

14648

23.0

9586

10235

10887

11540

12193

12842

13488

14131

14773

23.2

9712

10362

11014

11667

12319

12968

13614

14256

14898

23.4

9838

10488

11141

11794

12446

13094

13739

14381

15023

23.6

9965

10615

11268

11921

12572

13220

13865

14506

15147

23.8

10091

10742

11395

12048

12699

13346

13990

14632

15272

24.0

10217

10869

11521

12174

12825

13472

14116

14757

15397

24.2

10344

10995

11648

12301

12951

13598

14241

14882

15521

24.4

10470

11122

11775

12428

13078

13724

14367

15007

15646

24.6

10596

11249

11902

12554

13204

13850

14492

15132

15771

24.8

10723

11376

12029

12681

13330

13976

14618

15257

15895

25.0

10849

11502

12156

12807

13456

14102

14743

15382

16020

Original

07-14-08

08.01.79

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

25.2

10975

11629

12282

12934

13582

14228

14869

15508

16145

25.4

11102

11756

12409

13060

13708

14353

14995

15633

16269

25.6

11228

11882

12535

13186

13834

14479

15121

15758

16394

25.8

11355

12009

12662

13312

13960

14605

15246

15883

16519

26.0

11481

12135

12788

13438

14086

14730

15372

16008

16643

26.2

11607

12262

12915

13564

14211

14856

15497

16133

16768

26.4

11734

12388

13041

13690

14337

14981

15622

16258

16893

26.6

11850

12515

13167

13816

14462

15107

15747

16383

17017

26.8

11987

12641

13293

13942

14588

15232

15872

16508

17142

27.0

12113

12767

13420

14068

14713

15357

15997

16633

17267

27.2

12240

12893

13546

14194

14839

15482

16122

16757

17391

27.4

12366

13020

13672

14319

14964

15607

16247

16882

17516

27.6

12493

13146

13797

14445

15090

15732

16371

17006

17640

27.8

12619

13272

13923

14571

15215

15857

16496

17131

17764

28.0

12746

13398

14049

14697

15340

15982

16620

17255

17889

28.2

12873

13525

14175

14822

15466

16107

16745

17379

18013

28.4

12999

13651

14301

14948

15591

16232

16869

17504

18137

28.6

13126

13777

14427

15074

15717

16357

16993

17628

18261

28.8

13252

13904

14553

15200

15842

16482

17118

17752

18385

29.0

13379

14030

14680

15326

15968

16607

17243

17876

18508

29.2

13506

14156

14806

15451

16093

16732

17367

18000

18632

29.4

13632

14283

14932

15577

16219

16857

17492

18124

18755

08.01.80

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

29.6

13759

14409

15058

15703

16344

16982

17616

18248

18879

29.8

13886

14536

15184

15829

16470

17107

17741

18372

19003

30.0

14012

14662

15310

15955

16595

17232

17866

18497

19126

30.2

14139

14788

15436

16080

16720

17357

17990

18621

19250

30.4

14265

14914

15562

16206

16845

17482

18115

18745

19374

30.6

14391

15040

15688

16331

16970

17606

18239

18869

19498

30.8

14518

15166

15813

16456

17095

17731

18364

18994

19622

31.0

14644

15292

15938

16581

17220

17855

18488

19118

19746

31.2

14770

15417

16064

16706

17344

17980

18612

19242

19871

31.4

14895

15543

16189

16831

17469

18104

18737

19366

19995

31.6

15021

15668

16314

16955

17593

18228

18861

19491

20119

31.8

15147

15794

16439

17080

17718

18353

18985

19615

20243

32.0

15273

15919

16564

17205

17842

18477

19109

19739

20367

32.2

15398

16044

16689

17329

17966

18601

19233

19862

20490

32.4

15524

16170

16814

17454

18091

18725

19357

19986

20613

32.6

15650

16295

16938

17578

18215

18849

19480

20109

20735

32.8

15775

16420

17063

17703

18339

18973

19604

20232

20857

33.0

15901

16645

17188

17828

18464

19097

19728

20354

20978

33.2

16026

16671

17313

17952

18588

19221

19851

20477

21099

33.4

16152

16796

17438

18077

18713

19346

19974

20599

21219

33.6

16278

16921

17563

18202

18837

19470

20098

20721

21339

33.8

16403

17047

17689

18327

18962

19594

20221

20843

21459

Original

07-14-08

08.01.81

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

34.0

16529

17172

17814

18452

19086

19718

20345

20964

21579

34.2

16654

17297

17939

18576

19211

19842

20468

21086

21698

34.4

16780

17422

18064

18701

19335

19967

20592

21208

21818

34.6

16906

17548

18189

18825

19459

20091

20716

21330

21937

34.8

17031

17673

18313

18950

19584

20216

20840

21452

22057

35.0

17157

17798

18438

19074

19708

20340

20964

21575

22176

35.2

17282

17923

18563

19199

19832

20465

21089

21697

22296

35.4

17408

18049

18688

19323

19956

20589

21213

21819

22415

35.6

17533

18174

18813

19447

20080

20714

21337

21941

22535

35.8

17659

18299

18937

19571

20204

20838

21461

22063

22654

36.0

17784

18424

19062

19695

20328

20962

21584

22185

22774

36.2

17909

18549

19186

19819

20452

21086

21707

22307

22893

36.4

18034

18673

19310

19943

20576

21209

21830

22428

23012

36.6

18159

18798

19435

20067

20699

21332

21952

22549

23131

36.8

18284

18922

19559

20191

20822

21455

22074

22669

23250

37.0

18409

19046

19683

20315

20946

21577

22195

22789

23369

37.2

18533

19171

19807

20439

21069

21699

22315

22908

23487

37.4

18658

19295

19930

20562

21192

21821

22435

23027

23605

37.6

18782

19419

20054

20686

21316

21943

22555

23145

23722

37.8

18907

19543

20178

20810

21439

22064

22675

23263

23838

38.0

19031

19667

20302

20934

21562

22186

22795

23381

23953

38.2

19156

19791

20426

21058

21686

22308

22914

23498

24067

08.01.82

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

38.4

19281

19916

20551

21182

21810

22430

23034

23614

24179

38.6

19405

20040

20675

21307

21933

22553

23154

23730

24291

38.8

19530

20165

20800

21431

22058

22676

23274

23845

24400

39.0

19655

20290

20924

21556

22182

22799

23394

23960

24509

39.2

19781

20415

21049

21680

22306

22922

23514

24074

24616

39.4

19906

20539

21174

21805

22430

23045

23635

24189

24723

39.6

20031

20664

21299

21929

22554

23169

23755

24302

24829

39.8

20156

20789

21423

22053

22677

23291

23875

24416

24935

40.0

20280

20913

21547

22177

22801

23414

23995

24530

25040

40.2

20404

21037

21671

22300

22923

23536

24114

24643

25147

40.4

20528

21161

21794

22422

23045

23657

24233

24756

25253

40.6

20652

21284

21916

22544

23166

23778

24352

24870

25361

40.8

20775

21407

22039

22665

23286

23897

24469

24983

25469

41.0

20897

21529

22160

22785

23406

24016

24587

25097

25578

41.2

21019

21651

22281

22905

23525

24134

24703

25210

25687

41.4

21141

21772

22402

23025

23643

24252

24819

25322

25797

41.6

21262

21893

22522

23144

23761

24368

24933

25434

25906

41.8

21384

22014

22643

23264

23879

24484

25047

25544

26014

42.0

21504

22135

22763

23383

23997

24599

25159

25654

26121

42.2

21625

22255

22883

23503

24114

24714

25270

25762

26226

42.4

21746

22375

23003

23623

24233

24829

25380

25868

26330

42.6

21866

22496

23124

23743

24351

24942

25489

25972

26431

Original

07-14-08

08.01.83

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

42.8

21986

22616

23244

23864

24470

25056

25596

26075

26530

43.0

22107

22737

23365

23985

24589

25169

25702

26175

26626

43.2

22227

22857

22486

24107

24709

25282

25807

26274

26720

43.4

22347

22977

23607

24228

24828

25395

25911

26372

26813

43.6

22468

23098

23728

24350

24948

25507

26015

26469

26903

43.8

22588

23218

23849

24471

25066

25620

26119

26566

26993

44.0

22708

23338

23969

24591

25184

25732

26223

26662

27081

44.2

22828

23458

24089

24711

25302

25844

26328

26758

27169

44.4

22949

23578

24209

24830

25418

25956

26433

26855

27255

44.6

23069

23698

24328

24947

25534

26068

26540

26952

27342

44.8

23189

23818

24447

25063

25647

26180

26648

27051

27429

45.0

23309

23937

24565

25178

25760

26292

26756

27150

27515

45.2

23429

24056

24682

25292

25871

26403

26865

27249

27602

45.4

23548

24175

24798

25404

25981

26513

26973

27348

27688

45.6

23667

24292

24914

25515

26089

26622

27081

27447

27774

45.8

23785

24409

25028

25625

26196

26730

27187

27545

27861

46.0

23901

24525

25141

25734

26302

26835

27291

27642

27947

46.2

24017

24639

25253

25841

26406

26939

27393

27737

28033

46.4

24131

24752

25363

25948

26508

27040

27492

27831

28118

46.6

24243

24863

25472

26053

26609

27139

27588

27922

28204

46.8

24354

24972

25579

26156

26709

27234

27680

28010

28290

47.0

24464

25080

25685

26260

26808

27327

27768

28097

28375

08.01.84

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

47.2

24572

25187

25791

26362

26905

27418

27854

28180

28459

47.4

24679

25293

25895

26464

27002

27508

27937

28262

28541

47.6

24785

25399

25999

26566

27099

27596

28017

28341

28621

47.8

24893

25504

26103

26668

27196

27683

28097

28418

28699

48.0

24999

25609

26208

26770

27293

27770

28175

28494

28774

48.2

25106

25715

26313

26873

27390

27858

28253

28567

28845

48.4

25213

25821

26418

26977

27489

27946

28331

28639

28913

48.6

25321

25929

26525

27082

27588

28036

28409

28709

28976

48.8

25429

26037

26633

27189

27689

28126

28489

28778

29035

49.0

25539

26146

26742

27296

27791

28219

28568

28845

29090

49.2

25649

26256

26852

27403

27893

28311

28649

28911

29141

49.4

25759

26366

26961

27510

27994

28404

28729

28976

29189

49.6

25869

26475

27069

27615

28095

28496

28810

29040

29235

49.8

25977

26583

27177

27719

28194

28588

28890

29104

29280

50.0

26085

26690

27282

27821

28290

28678

28969

29167

29323

50.2

26192

26795

27385

27919

28384

28766

29048

29230

29367

50.4

26296

26897

27484

28014

28474

28851

29125

29292

29411

50.6

26399

26997

27580

28105

28560

28934

29201

29354

29457

50.8

26499

27094

27673

28191

28641

29013

29276

29417

29504

51.0

26596

27188

27761

28273

28718

29089

29348

29479

29553

51.2

26692

27279

27847

28352

28792

29162

29419

29541

29602

51.4

26786

27368

27930

28428

28862

29232

29487

29601

29653

Original

07-14-08

08.01.85

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

51.6

26878

27455

28011

28502

28931

29299

29553

29660

29703

51.8

26969

27541

28090

28574

28998

29365

29616

29717

29753

52.0

27059

27626

28169

28646

29064

29428

29677

29772

29802

52.2

27148

27710

28247

28717

29130

29489

29734

29825

29849

52.4

27236

27793

28325

28790

29197

29549

29788

29874

29895

52.6

27323

27876

28403

28864

29264

29608

29838

29920

29939

52.8

27411

27959

28483

28939

29333

29665

29885

29962

29980

53.0

27498

28043

28563

29017

29403

29722

29929

30001

30019

53.2

27585

28126

28644

29095

29474

29778

29970

30037

30055

53.4

27671

28209

28725

29174

29545

29832

30009

30071

30090

53.6

27758

28293

28806

29254

29617

29887

30047

30103

30123

53.8

27844

28376

28887

29333

29688

29940

30084

30134

30154

54.0

27931

28458

28967

29411

29758

29993

30121

30165

30185

08.01.86

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH)

3.0

569

626

708

867

1128

1495

1979

2568

3186

3.2

604

664

748

909

1178

1564

2067

2665

3285

3.4

640

702

788

952

1230

1634

2154

2761

3385

3.6

676

741

830

996

1283

1704

2241

2856

3484

3.8

712

781

873

1043

1339

1775

2328

2951

3584

4.0

749

821

917

1093

1397

1848

2415

3046

3683

4.2

786

863

963

1145

1459

1922

2501

3139

3782

4.4

824

906

1012

1201

1524

1997

2586

3232

3881

4.6

863

950

1063

1261

1593

2075

2671

3323

3979

4.8

903

996

1116

1326

1667

2155

2755

3414

4078

5.0

944

1043

1173

1394

1745

2237

2839

3504

4176

5.2

986

1093

1232

1466

1827

2321

2923

3594

4274

5.4

1031

1145

1294

1541

1913

2407

3008

3684

4372

5.6

1077

1199

1358

1620

2001

2496

3095

3775

4471

5.8

1126

1256

1425

1701

2092

2587

3183

3866

4570

6.0

1178

1316

1496

1785

2186

2681

3274

3960

4670

6.2

1233

1379

1569

1872

2281

2777

3368

4056

4770

6.4

1292

1445

1645

1960

2379

2875

3465

4154

4871

6.6

1354

1515

1724

2050

2477

2977

3566

4255

4973

6.8

1421

1589

1806

2141

2576

3080

3671

4359

5075

7.0

1491

1666

1890

2233

2676

3187

3780

4467

5180

7.2

1563

1745

1976

2326

2777

3295

3893

4577

5285

Original

07-14-08

08.01.87

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH)

7.4

1639

1826

2064

2420

2878

3405

4008

4689

5391

7.6

1715

1909

2153

2515

2980

3516

4125

4803

5498

7.8

1793

1993

2242

2609

3082

3628

4244

4919

5607

8.0

1872

2076

2331

2704

3184

3740

4363

5036

5717

8.2

1950

2160

2420

2798

3286

3853

4483

5154

5828

8.4

2028

2242

2508

2892

3388

3965

4603

5272

5941

8.6

2104

2323

2594

2985

3490

4077

4722

5390

6055

8.8

2178

2402

2678

3077

3591

4189

4840

5508

6170

9.0

2251

2480

2762

3169

3693

4299

4956

5625

6286

9.2

2324

2557

2844

3261

3795

4409

5072

5743

6404

9.4

2396

2634

2927

3354

3898

4520

5187

5860

6522

9.6

2468

2711

3011

3448

4001

4630

5301

5977

6641

9.8

2541

2790

3096

3543

4107

4741

5416

6093

6760

10.0

2615

2870

3183

3641

4213

4853

5531

6210

6879

10.2

2692

2953

3274

3742

4322

4966

5646

6327

6998

10.4

2771

3040

3368

3846

4434

5081

5761

6444

7117

10.6

2853

3130

3467

3953

4548

5197

5878

6561

7235

10.8

2939

3225

3571

4065

4664

5315

5995

6679

7353

11.0

3028

3323

3679

4180

4784

5435

6114

6797

7471

11.2

3120

3426

3792

4299

4906

5557

6234

6915

7588

11.4

3214

3531

3907

4420

5030

5680

6354

7034

7705

11.6

3311

3639

4025

4544

5155

5804

6476

7153

7822

11.8

3409

3748

4144

4669

5281

5929

6598

7272

7940

08.01.88

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH)

12.0

3508

3859

4265

4794

5408

6054

6720

7393

8057

12.2

3608

3970

4386

4920

5535

6180

6844

7514

8176

12.4

3708

4081

4507

5046

5662

6307

6968

7635

8296

12.6

3809

4192

4628

5171

5789

6433

7092

7758

8416

12.8

3909

4302

4746

5295

5915

6559

7217

7881

8538

13.0

4009

4411

4864

5417

6040

6684

7342

8005

8661

13.2

4109

4520

4980

5539

6164

6810

7468

8130

8784

13.4

4209

4628

5096

5660

6288

6936

7593

8255

8909

13.6

4308

4736

5211

5780

6412

7061

7719

8380

9034

13.8

4408

4843

5326

5900

6535

7186

7845

8506

9160

14.0

4508

4951

5441

6020

6659

7312

7971

8632

9286

14.2

4608

5059

5556

6141

6782

7437

8098

8758

9412

14.4

4708

5169

5672

6261

6906

7563

8224

8885

9538

14.6

4809

5277

5788

6383

7030

7688

8350

9011

9664

14.8

4910

5386

5905

6505

7155

7814

8476

9136

9790

15.0

5012

5497

6024

6628

7280

7940

8601

9262

9916

15.2

5115

5609

6143

6751

7406

8066

8727

9387

10041

15.4

5219

5721

6263

6876

7532

8192

8853

9513

10167

15.6

5324

5835

6384

7001

7658

8318

8979

9638

10292

15.8

5430

5949

6505

7126

7784

8445

9104

9763

10417

16.0

5537

6065

6628

7252

7911

8571

9230

9888

10542

16.2

5646

6181

6751

7378

8038

8698

9356

10013

10666

16.4

5757

6299

6875

7505

8165

8825

9482

10138

10791

Original

07-14-08

08.01.89

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH)

16.6

5869

6418

6999

7632

8292

8951

9608

10264

10916

16.8

5984

6539

7124

7759

8420

9078

9734

10389

11042

17.0

6100

6660

7250

7886

8547

9205

9860

10515

11167

17.2

6218

6782

7375

8013

8674

9332

9986

10641

11292

17.4

6336

6905

7502

8140

8801

9459

10113

10766

11417

17.6

6456

7029

7628

8268

8928

9585

10239

10892

11543

17.8

6577

7153

7755

8395

9056

9712

10366

11018

11668

18.0

6697

7277

7881

8523

9183

9839

10492

11144

11794

18.2

6818

7402

8008

8650

9310

9966

10619

11270

11919

18.4

6939

7526

8135

8778

9437

10093

10745

11396

12045

18.6

7059

7650

8261

8905

9565

10220

10872

11522

12170

18.8

7178

7774

8388

9032

9692

10347

10999

11648

12296

19.0

7297

7897

8514

9160

9819

10474

11125

11774

12421

19.2

7415

8020

8640

9287

9946

10601

11252

11900

12547

19.4

7533

8143

8766

9414

10074

10728

11378

12026

12672

19.6

7652

8265

8893

9542

10201

10855

11505

12152

12798

19.8

7770

8388

9019

9669

10328

10982

11631

12278

12923

20.0

7889

8511

9145

9796

10455

11108

11758

12404

13049

20.2

8008

8634

9271

9923

10582

11235

11884

12530

13175

20.4

8128

8758

9397

10050

10709

11362

12010

12656

13300

20.6

8248

8882

9523

10177

10835

11488

12137

12782

13426

20.8

8370

9007

9650

10304

10962

11615

12263

12908

13552

21.0

8493

9132

9777

10431

11089

11741

12389

13034

13677

08.01.90

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH)

21.2

8616

9257

9903

10558

11215

11867

12515

13160

13803

21.4

8741

9383

10030

10685

11341

11993

12641

13286

13929

21.6

8866

9509

10157

10812

11468

12119

12767

13412

14055

21.8

8991

9636

10284

10939

11594

12246

12893

13537

14180

22.0

9117

9762

10411

11065

11720

12372

13019

13663

14306

22.2

9243

9889

10528

11192

11847

12498

13145

13789

14431

22.4

9370

10016

10666

11319

11973

12624

13270

13914

14557

22.6

9496

10143

10793

11446

12099

12750

13396

14040

14682

22.8

9622

10269

10920

11573

12226

12876

13522

14165

14807

23.0

9748

10396

11047

11700

12352

13002

13647

14290

14932

23.2

9875

10523

11174

11827

12479

13128

13773

14415

15057

23.4

10001

10650

11301

11954

12605

13254

13898

14540

15182

23.6

10127

10776

11428

12080

12732

13380

14024

14666

15306

23.8

10253

10903

11555

12207

12858

13506

14149

14791

15431

24.0

10379

11030

11681

12334

12985

13631

14275

14916

15556

24.2

10505

11156

11808

12461

13111

13757

14400

15041

15680

24.4

10631

11283

11935

12587

13237

13883

14526

15166

15805

24.6

10757

11409

12062

12714

13364

14009

14651

15291

15929

24.8

10883

11536

12189

12840

13490

14135

14777

15416

16054

25.0

11010

11662

12315

12967

13616

14261

14903

15541

16179

25.2

11136

11789

12442

13093

13742

14389

15028

15666

16303

25.4

11262

11915

12568

13219

13867

14513

15154

15792

16428

25.6

11388

12042

12695

13346

13993

14638

15280

15917

16553

Original

07-14-08

08.01.91

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH)

25.8

11515

12168

12821

13472

14119

14764

15405

16042

16677

26.0

11641

12295

12948

13598

14245

14889

15531

16167

16802

26.2

11767

12421

13074

13724

14370

15015

15656

16292

16927

26.4

11893

12548

13200

13850

14496

15140

15781

16417

17051

26.6

12020

12674

13327

13975

14621

15266

15906

16542

17176

26.8

12146

12800

13453

14101

14747

15391

16031

16667

17300

27.0

12273

12927

13579

14227

14872

15516

16156

16791

17425

27.2

12399

13053

13705

14353

14998

15641

16281

16916

17550

27.4

12526

13179

13831

14478

15123

15766

16405

17041

17674

27.6

12652

13305

13957

14604

15248

15891

16530

17165

17798

27.8

12779

13431

14083

14730

15374

16016

16654

17289

17923

28.0

12905

13558

14209

14856

15499

16141

16779

17413

18047

28.2

13032

13684

14335

14981

15625

16266

16903

17538

18171

28.4

13159

13810

14461

15107

15750

16390

17028

17662

18295

28.6

13285

13937

14587

15233

15876

16515

17152

17786

18419

28.8

13412

14063

14713

15359

16001

16640

17276

17910

18542

29.0

13538

14189

14839

15485

16127

16765

17401

18034

18666

29.2

13665

14316

14965

15610

16252

16890

17526

18158

18789

29.4

13792

14442

15091

15736

16377

17016

17650

18282

18913

29.6

13918

14569

15217

15862

16503

17141

17775

18406

19036

29.8

14045

14695

15343

15988

16628

17266

17899

18530

19160

30.0

14171

14821

15469

16113

16753

17390

18024

18654

19284

30.2

14298

14947

15595

16239

16879

17515

18149

18779

19407

08.01.92

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH)

30.4

14424

15073

15721

16364

17004

17640

18273

18903

19531

30.6

14550

15199

15847

16489

17128

17765

18398

19027

19655

30.8

14677

15325

15972

16615

17253

17889

18522

19152

19780

31.0

14803

15451

16097

16739

17378

18014

18646

19276

19904

31.2

14928

15576

16223

16864

17502

18138

18771

19400

20029

31.4

15054

15702

16348

16989

17627

18262

18895

19525

20153

31.6

15180

15827

16473

17114

17751

18387

19019

19649

20277

31.8

15306

15952

16597

17238

17876

18511

19143

19773

20401

32.0

15431

16078

16722

17363

18000

18635

19267

19896

20525

32.2

15557

16203

16847

17488

18124

18759

19391

20020

20648

32.4

15683

16328

16972

17612

18249

18883

19515

20143

20770

32.6

15808

16453

17097

17737

18373

19007

19638

20266

20892

32.8

15934

16579

17222

17861

18498

19131

19762

20388

21013

33.0

16059

16704

17347

17986

18622

19256

19885

20510

21133

33.2

16185

16829

17472

18111

18746

19380

12000 8

20632

21253

33.4

16311

16955

17597

18236

18871

19504

20132

20753

21372

33.6

16436

17080

17722

18361

18996

19628

20255

20875

21490

33.8

16562

17205

17847

18485

19120

19753

20379

20996

21609

34.0

16687

17331

17972

18610

19244

19877

20502

21117

21727

34.2

16813

17456

18097

18735

19369

20002

20626

21238

21844

34.4

16939

17581

18222

18859

19493

20126

20750

21359

21962

34.6

17064

17706

18347

18984

19618

20251

20874

21481

22080

34.8

17190

17832

18472

19108

19742

20376

20998

21602

22198

Original

07-14-08

08.01.93

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH)

35.0

17315

17957

18597

19233

19866

20500

21123

21724

22316

35.2

17441

18082

18722

19357

19990

20625

21247

21846

22434

35.4

17566

18207

18847

19481

20114

20750

21371

21967

22553

35.6

17692

18332

18971

19605

20238

20874

21496

22089

22671

35.8

17817

18457

19096

19729

20362

20998

21619

22210

22789

36.0

17942

18582

1922

19853

20485

21122

21743

22331

22907

36.2

18067

18707

19345

19977

20609

21246

21866

22452

23025

36.4

18192

18831

19469

20101

20733

21369

21988

22572

23142

36.6

18317

18956

19593

20225

20856

21492

22109

22691

23260

36.8

18442

19080

19717

20349

20979

21614

22230

22810

23377

37.0

18566

19204

19841

20473

21103

21736

22350

22928

23494

37.2

18691

19328

19965

20597

21226

21857

22469

23046

23610

37.4

18815

19452

20088

20720

21349

21978

22588

23163

23726

37.6

18940

19576

20212

20844

21473

22099

22706

23279

23840

37.8

19064

19701

20336

20969

21596

22221

22824

23395

23954

38.0

19189

19825

20460

21093

21719

22342

22942

23511

24067

38.2

19313

19949

20584

21217

21843

22463

23060

23625

24179

38.4

19438

20073

20709

21341

21967

22584

23178

23740

24290

38.6

19563

20198

20833

21466

22091

22706

23297

23854

24399

38.8

19688

20323

20958

21590

22215

22829

23416

23968

24507

39.0

19813

20448

21083

21715

22339

22951

23535

24081

24613

39.2

19939

20573

21208

21840

22463

23074

23654

24194

24719

39.4

20064

20698

21333

21964

22587

23197

23774

24307

24823

08.01.94

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH)

39.6

20189

20823

21457

22088

22710

23319

23893

24419

24928

39.8

20314

20947

21581

22212

22833

23441

24012

24532

25032

40.0

20438

21072

21705

22335

22955

23563

24131

24644

25136

40.2

20562

21195

21829

22457

23077

23683

24249

24756

25241

40.4

20686

21319

21951

22579

23198

23803

24366

24868

25346

40.6

20809

21441

22073

22700

23317

23922

24483

24979

25452

40.8

20931

21563

22195

22820

23436

24040

24599

25091

25558

41.0

21052

21684

22315

22939

23554

24157

24714

25203

25666

41.2

21173

21805

22435

23057

23670

24272

24829

25314

25774

41.4

21294

21925

22554

23175

23787

24387

24942

25424

25882

41.6

21414

22045

22673

23293

23902

24501

25054

25533

25989

41.8

21533

22164

22792

23410

24018

24614

25165

25642

26095

42.0

21653

22283

22911

23528

24133

24727

25274

25749

26200

42.2

21772

22402

23029

23646

24249

24839

25383

25854

26304

42.4

21891

22521

23148

23764

24365

24950

25490

25958

26405

42.6

22010

22640

23267

23883

24482

25062

25595

26059

26504

42.8

22129

22759

23386

24002

24599

25173

25699

26159

26601

43.0

22248

22878

23506

24122

24717

25284

25803

26257

26694

43.2

22367

22998

23626

24243

24835

25395

25905

26353

26786

43.4

22486

23117

23745

24363

24953

25506

26006

26448

26876

43.6

22605

23236

23865

24483

25071

25616

26107

26542

26963

43.8

22724

23355

23985

24603

25188

25726

26209

26636

27050

44.0

22843

23474

24104

24722

25304

25836

26310

26729

27136

Original

07-14-08

08.01.95

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH)

44.2

22962

23593

24222

24840

25420

25946

26412

26823

27220

44.4

23080

23711

24341

24956

25534

26056

26515

26917

27305

44.6

23199

23829

24458

25072

25646

26165

26619

27012

27389

44.8

23317

23947

24575

25185

25757

26274

26724

27108

27473

45.0

23435

24065

24691

25298

25866

26383

26830

27205

27558

45.2

23553

24182

24805

25408

25974

26490

26937

27302

27642

45.4

23670

24298

24919

25517

26079

26597

27043

27399

27727

45.6

23787

24413

25032

25625

26184

26703

27148

27496

27811

45.8

23902

24527

25144

25732

26287

26807

27252

27592

27896

46.0

24017

24640

25254

25837

26388

26909

27354

27686

27980

46.2

24130

24752

25363

25941

26488

27009

27453

27779

28064

46.4

24242

24863

25471

26044

26587

27107

27550

27870

28147

46.6

24352

24972

25577

26146

26685

27202

27643

27959

28230

46.8

24461

25079

25682

26247

26782

27295

27731

28044

28313

47.0

24569

25185

25786

26347

26878

27385

27816

28127

28395

47.2

24675

25289

25888

26447

26973

27473

27898

28208

28476

47.4

24781

25393

25990

26547

27067

27560

27978

28286

28555

47.6

24886

25497

26092

26646

27162

27645

28055

28362

28632

47.8

24991

25600

26192

26746

27256

27730

28131

28436

28707

48.0

25096

25703

26295

26846

27351

27814

28206

28508

28779

48.2

25201

25807

26398

26946

27446

27899

28281

28579

28848

48.4

25307

25911

26501

27047

27542

27985

28356

28648

28913

48.6

25413

26017

26605

27149

27638

28071

28432

28716

28975

08.01.96

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH)

48.8

25521

26123

26711

27252

27736

28159

28509

28783

29032

49.0

25629

26231

26817

27355

27834

28248

28586

28849

29086

49.2

25738

26338

26924

27458

27932

28338

28665

28914

29136

49.4

25846

26446

27030

27561

28029

28428

28743

28979

29185

49.6

25954

26553

27136

27663

28125

28517

28822

29043

29231

49.8

26061

26659

27240

27763

28220

28605

28901

29106

29276

50.0

26167

26763

27342

27861

28312

28692

28979

29169

29320

50.2

26272

26866

27442

27955

28402

28777

29055

29231

29365

50.4

26374

26966

27539

28047

28488

28859

29131

29293

29409

50.6

26474

27063

27632

28134

28570

28938

29205

29354

29455

50.8

26572

27157

27722

28218

28648

29014

29278

29416

29503

51.0

26667

27248

27807

28297

28722

29087

29348

29477

29552

51.2

26759

27336

27890

28373

28794

29157

29416

29537

29602

51.4

26850

27422

27970

28447

28862

29225

29482

29596

29652

51.6

26940

27506

28048

28518

28929

29290

29545

29653

29702

51.8

27028

27588

28125

28589

28994

29353

29606

29709

29752

52.0

27115

27670

28200

28659

29059

29414

29664

29762

29800

52.2

27201

27751

28275

28729

29123

29474

29720

29813

29848

52.4

27286

27832

28351

28800

29189

29532

29772

29861

29893

52.6

27371

27912

28427

28872

29255

29590

29821

29906

29936

52.8

27457

27993

28504

28947

29323

29646

29867

29947

29977

53.0

27542

28075

28583

29022

29393

29703

29910

29986

30015

53.2

27627

28156

28661

29099

29463

29758

29950

30021

30051

Original

07-14-08

08.01.97

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH)

53.4

27712

28238

28740

29177

29534

29813

29989

30055

30084

53.6

27797

28320

28820

29254

29605

29867

30027

30087

30117

53.8

27882

28401

28898

29332

29675

29921

30064

30119

30147

54.0

27967

28482

28976

29408

29744

29974

30101

30150

30177

08.01.98

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

3.0

617

677

759

922

1193

1585

2094

2696

3318

3.2

652

714

798

963

1243

1653

2181

2793

3419

3.4

687

752

837

1005

1294

1722

2268

2889

3519

3.6

723

791

878

1050

1347

1792

2355

2985

3619

3.8

760

830

920

1097

1403

1864

2442

3081

3719

4.0

798

872

967

1148

1463

1938

2529

3175

3819

4.2

836

915

1015

1202

1527

2013

2616

3270

3918

4.4

877

960

1066

1261

1595

2091

2703

3363

4017

4.6

918

1008

1120

1324

1668

2172

2790

3456

4115

4.8

962

1058

1178

1393

1746

2256

2877

3547

4212

5.0

1007

1110

1240

1467

1829

2343

2965

3639

4310

5.2

1054

1165

1305

1545

1917

2432

3053

3730

4407

5.4

1104

1222

1373

1627

2009

2524

3142

3821

4505

5.6

1155

1282

1445

1713

2104

2619

3233

3914

4602

5.8

1209

1345

1519

1801

2202

2715

3326

4007

4701

6.0

1266

1410

1595

1891

2301

2814

3421

4102

4800

6.2

1325

1478

1674

1983

2403

2915

3519

4200

4900

6.4

1387

1548

1755

2076

2505

3019

3619

4299

5001

6.6

1453

1621

1837

2170

2607

3123

3723

4402

5104

6.8

1521

1697

1922

2264

2709

3230

3830

4508

5209

7.0

1593

1775

2007

2358

2811

3338

3940

4617

5315

7.2

1666

1855

2094

2452

2913

3447

4053

4729

5423

Original

07-14-08

08.01.99

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

7.4

1741

1936

2182

2547

3015

3557

4168

4843

5532

7.6

1818

2019

2270

2641

3117

3668

4285

4958

5642

7.8

1895

2101

2358

2736

3219

3780

4403

5075

5754

8.0

1972

2184

2447

2830

3322

3892

4522

5193

5867

8.2

2049

2267

2536

2925

3424

4004

4641

5312

5981

8.4

2126

2349

2624

3019

3527

4116

4760

5430

6096

8.6

2201

2430

2711

3114

3630

4228

4878

5549

6212

8.8

2275

2510

2798

3209

3733

4340

4995

5666

6329

9.0

2347

2589

2884

3304

3838

4451

5111

5784

6446

9.2

2419

2667

2970

3400

3943

4563

5226

5901

6564

9.4

2491

2746

3057

3497

4049

4675

5341

6017

6682

9.6

2563

2826

3145

3595

4156

4787

5455

6134

6800

9.8

2637

2907

3235

3695

4264

4900

5570

6250

6919

10.0

2714

2990

3327

3797

4375

5013

5685

6367

7038

10.2

2790

3075

3422

3901

4486

5128

5800

6484

7157

10.4

2870

3164

3520

4009

4600

5244

5917

6601

7275

10.6

2955

3257

3622

4119

4716

5362

6034

6718

7394

10.8

3043

3354

3728

4232

4834

5481

6153

6836

7512

11.0

3134

3455

3838

4349

4955

5602

6272

6955

7630

11.2

3229

3559

3951

4468

5076

5724

6393

7074

7748

11.4

3326

3666

4066

4589

5200

5847

6515

7194

7865

11.6

3425

3775

4184

4711

5324

5971

6637

7314

7983

11.8

3526

3886

4303

4835

5449

6096

6760

7435

8102

12.0

3628

3998

4423

4959

5575

6221

6884

7556

8221

08.01.100

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

12.2

3730

4110

4543

5084

5701

6347

7009

7678

8340

12.4

3833

4222

4664

5208

5826

6473

7133

7801

8460

12.6

3935

4333

4783

5332

5952

6598

7258

7924

8582

12.8

4036

4443

4901

5455

6076

6724

7383

8048

8704

13.0

4136

4553

5018

5576

6200

6849

7509

8172

8827

13.2

4236

4661

5134

5697

6324

6974

7634

8297

8951

13.4

4336

4769

5250

5818

6447

7099

7760

8422

9076

13.6

4435

4877

5365

5938

6570

7224

7885

8547

9201

13.8

4535

4984

5480

6058

6693

7349

8011

8673

9326

14.0

4634

5092

5595

6178

6816

7473

8136

8798

9452

14.2

4735

5201

5710

6298

6940

7598

8262

8924

9578

14.4

4835

5310

5827

6419

7063

7723

8387

9050

9704

14.6

4937

5420

5944

6541

7188

7849

8513

9175

9830

14.8

5040

5531

6062

6664

7312

7974

8639

9301

9955

15.0

5144

5643

6181

6787

7438

8100

8764

9426

10080

15.2

5249

5756

6302

6912

7564

8226

8889

9551

10205

15.4

5355

5871

6423

7037

7690

8352

9015

9676

10330

15.6

5463

5986

6545

7162

7816

8478

9140

9801

10455

15.8

5572

6103

6668

7288

7943

8605

9266

9925

10579

16.0

5682

6220

6791

7415

8070

8731

9391

10050

10704

16.2

5794

6339

6915

7542

8198

8858

9517

10175

10829

16.4

5907

6458

7040

7668

8325

8985

9643

10300

10953

16.6

6021

6578

7164

7796

8452

9112

9769

10425

11078

Original

07-14-08

08.01.101

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

16.8

6137

6699

7290

7923

8580

9238

9895

10551

11203

17.0

6254

6821

7415

8050

8707

9365

10021

10676

11328

17.2

6373

6944

7541

8177

8834

9492

10147

10802

11453

17.4

6492

7067

7667

8304

8962

9619

10274

10927

11578

17.6

6612

7190

7793

8431

9089

9746

10400

11053

11703

17.8

6732

7314

7919

8558

9216

9873

10526

11179

11829

18.0

6852

7438

8045

8685

9343

10000

10563

11305

11954

18.2

6973

7562

8171

8812

9470

10127

10780

11431

12080

18.4

7093

7686

8297

8939

9597

10254

10906

11557

12205

18.6

7213

7809

8424

9067

9724

10380

11033

11683

12331

18.8

7333

7932

8550

9194

9851

10507

11159

11809

12456

19.0

7451

8056

8676

9321

9979

10634

11286

11935

12582

19.2

7570

8178

8802

9448

10106

10761

11412

12061

12707

19.4

7689

8301

8928

9575

10233

10888

11539

12187

12833

19.6

7807

8424

9053

9702

10360

11015

11665

12313

12958

19.8

7926

8547

9179

9829

10487

11142

11792

12439

13084

20.0

8045

8670

9305

9956

10614

11268

11918

12565

13209

20.2

8165

8794

9432

10083

10741

11395

12044

12691

13335

20.4

8285

8918

9558

10210

10868

11521

12171

12816

13460

20.6

8407

9042

9684

10337

10994

11648

12297

12942

13586

20.8

8529

9167

9810

10464

11121

11774

12423

13068

13712

21.0

8653

9292

9937

10591

11248

11900

12549

13194

13837

21.2

8777

9418

10064

10718

11374

12027

12675

13320

13963

21.4

8902

9544

10191

10845

11500

12153

12801

13445

14089

08.01.102

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

21.6

9027

9670

10318

10971

11627

12279

12927

13571

14214

21.8

9153

9797

10445

11098

11753

12405

13052

13697

14340

22.0

9280

9924

10572

11225

11880

12531

13178

13822

14465

22.2

9406

10051

10699

11352

12006

12657

13304

13948

14591

22.4

9533

10178

10826

11479

12132

12783

13429

14073

14716

22.6

9659

10304

10953

11605

12259

12909

13555

14199

14841

22.8

9785

10431

11080

11732

12385

13035

13681

14324

14966

23.0

9912

10558

11207

11859

12512

13161

13806

14449

15091

23.2

10038

10685

11334

11986

12638

13287

13932

14574

15216

23.4

10163

10811

11461

12113

12765

13413

14057

14699

15340

23.6

10289

10938

11588

12240

12891

13539

14183

14824

15465

23.8

10415

11064

11715

12367

13018

13665

14308

14949

15590

24.0

10541

11190

11842

12494

13144

13791

14434

15074

15714

24.2

10666

11317

11968

12621

13271

13917

14559

15199

15839

24.4

10792

11443

12095

12747

13397

14043

14685

15325

15963

24.6

10918

11570

12222

12874

13523

14169

14811

15450

16088

24.8

11044

11696

12348

13000

13649

14295

14936

15575

16213

25.0

11170

11822

12475

13126

13775

14420

15062

15700

16337

25.2

11296

11949

12602

13253

13901

14546

15187

15825

16462

25.4

11422

12075

12728

13379

14027

14672

15313

15950

16587

25.6

11548

12202

12854

13505

14153

14797

15438

16076

16711

25.8

11674

12328

12981

13631

14278

14923

15564

16201

16836

26.0

11801

12454

13107

13757

14404

15048

15689

16326

16961

Original

07-14-08

08.01.103

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

26.2

11927

12581

13233

13883

14529

15174

15814

16451

17086

26.4

12053

12707

13359

14008

14655

15299

15940

16576

17210

26.6

12180

12833

13485

14134

14780

15424

16065

16701

17335

26.8

12306

12960

13612

14260

14906

15549

16190

16825

17459

27.0

12432

13086

13738

14386

15031

15674

16314

16950

17584

27.2

12559

13212

13864

14512

15157

15800

16439

17074

17708

27.4

12685

13338

13990

14637

15282

15925

16564

17199

17832

27.6

12812

13464

14116

14763

15408

16049

16688

17323

17956

27.8

12938

13591

14242

14889

15533

16174

16813

17447

18080

28.0

13065

13717

14368

15015

15658

16299

16937

17571

18204

28.2

13192

13843

14494

15140

15784

16424

17061

17695

18328

28.4

13318

13970

14620

15266

15909

16549

17186

17819

18452

28.6

13445

14096

14746

15392

16035

16674

17310

17943

18576

28.8

13571

14222

14872

15518

16160

16799

17435

18067

18699

29.0

13698

14349

14998

15644

16286

16924

17560

18191

18822

29.2

13825

14475

15124

15769

16411

17049

17684

18315

18946

29.4

13951

14601

15250

15895

16536

17174

17809

18439

19069

29.6

14078

14728

15376

16021

16662

17300

17934

18564

19192

29.8

14205

14854

15502

16146

16787

17424

18058

18688

19316

30.0

14331

14980

15628

16272

16912

17549

18183

18812

19439

30.2

14457

15106

15754

16397

17037

17674

18307

18936

19563

30.4

14584

15232

15879

16522

17162

17799

18432

19060

19687

30.6

14710

15358

16005

16648

17287

17923

18556

19184

19811

30.8

14836

15484

16130

16773

17412

18048

18681

19309

19935

08.01.104

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

31.0

14962

15609

16256

16898

17536

18172

18805

19433

20059

31.2

15088

15735

16381

17022

17661

18297

18929

19557

20184

31.4

15213

15860

16506

17147

17785

18421

19053

19681

20308

31.6

15339

15986

16631

17272

17910

18545

19177

19805

20432

31.8

15465

16111

16756

17397

18034

18669

19301

19929

20555

32.0

15590

16236

16881

17521

18158

18793

19425

20052

20678

32.2

15716

16361

17006

17646

18283

18917

19548

20175

20801

32.4

15841

16487

17131

17771

18407

19041

19672

20298

20922

32.6

15967

16612

17256

17895

18532

19166

19795

20420

21043

32.8

16093

16737

17381

18020

18656

19290

19919

20542

21163

33.0

16218

16863

17506

18145

18781

19414

20042

20663

21281

33.2

16344

16988

17631

18270

18906

19539

20166

20784

21399

33.4

16469

17113

17756

18395

19031

19663

20289

20905

21517

33.6

16595

17239

17881

18520

19155

19788

20413

21025

21634

33.8

16721

17364

18006

18645

19280

19913

20536

21145

21750

34.0

16846

17489

18131

18769

19405

20037

20660

21266

21866

34.2

16972

17615

18256

18894

19529

20162

20783

21386

21983

34.4

17098

17740

18381

19019

19654

20287

20907

21506

22099

34.6

17223

17865

18506

19143

19778

20411

21031

21627

22215

34.8

17349

17991

18631

19267

19902

20536

21155

21748

22332

35.0

17474

18116

18756

19392

20026

20661

21279

21869

22449

35.2

17600

18241

18880

19516

20150

20785

21403

2199

22567

35.4

17725

18366

19005

19640

20274

20909

21527

22111

22684

Original

07-14-08

08.01.105

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

35.6

17850

18491

19129

19764

20398

21033

21650

22232

22801

35.8

17976

18616

19254

19888

20522

21157

21773

22352

22918

36.0

18101

18740

19378

20012

20645

21281

21895

22472

23035

36.2

18225

18865

19502

20136

20769

21404

22017

22591

23152

36.4

18350

18989

19627

20259

20893

21526

22138

22710

23268

36.6

18475

19114

19751

20383

21016

21649

22259

22828

23383

36.8

18599

19238

19875

20508

21140

21770

22378

22945

23498

37.0

18724

19362

19999

20632

21263

21892

22496

23061

23612

37.2

18848

19486

20123

20756

21387

22013

22614

23176

23726

37.4

18972

19610

20247

20880

21510

22133

22731

23291

23839

37.6

19095

19734

20371

21004

21633

22254

22848

23405

23950

37.8

19221

19858

20495

21129

21757

22374

22965

23518

24061

38.0

19345

19982

20619

21253

21880

22495

23082

23631

24171

38.2

19470

20106

20743

21377

22004

22616

23198

23744

24280

38.4

19595

20231

20868

21502

22127

22736

23315

23856

24388

38.6

19720

20355

20992

21626

22251

22858

23433

23969

24495

38.8

19845

20480

21117

21750

22374

22979

23551

24081

24601

39.0

19971

20605

21241

21874

22498

23101

23669

24193

24705

39.2

20096

20730

21366

21998

22621

23223

23787

24305

24809

39.4

20222

20855

21490

22122

22743

23345

23906

24416

24913

39.6

20347

20980

21614

22245

22866

23466

24024

24528

25016

39.8

20472

21105

21738

22368

22987

23587

24142

24639

25119

40.0

20596

21228

21861

22490

23108

23707

24259

24750

25223

40.2

20720

21352

21984

22611

23228

23826

24376

24861

25326

08.01.106

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

40.4

20843

21474

22106

22731

23347

23944

24491

24971

25432

40.6

20965

21596

22226

22850

23465

24060

24605

25081

25536

40.8

21086

21717

22346

22969

23581

24175

24719

25191

25642

41.0

21206

21836

22465

23086

23697

24289

24830

25301

25749

41.2

21325

21955

22584

23203

23812

24401

24941

25409

25856

41.4

21444

22074

22702

23319

23926

24513

25050

25517

25963

41.6

21562

22192

22819

23435

24039

24623

25158

25624

26069

41.8

21680

22310

22936

23551

24153

24733

25265

25729

26174

42.0

21797

22427

23054

23667

24266

24843

25370

25833

26277

42.2

21914

22545

23171

23784

24380

24952

25475

25936

26379

42.4

22032

22662

23289

23901

24494

25061

25579

26036

26478

42.6

22149

22780

23407

24018

24609

25170

25681

26135

26574

42.8

22267

22898

23525

24137

24724

25279

25783

26232

26667

43.0

22385

23016

23644

24255

24841

25388

25884

26327

26757

43.2

22503

23134

23763

24375

24957

25497

25985

26420

26845

43.4

22621

23253

23882

24494

25074

25606

26085

26512

26931

43.6

22739

23371

24001

24613

25190

25715

26184

26604

27015

43.8

22857

23489

24119

24731

25305

25824

26284

26695

27097

44.0

22974

23607

24237

24848

25419

25932

26384

26786

27180

44.2

23092

23724

24355

24964

25533

26040

26484

26877

27261

44.4

23209

23841

24471

25079

25644

26147

26585

26968

27343

44.6

23326

23957

24586

25191

25753

26254

26687

27061

27425

44.8

23443

24073

24700

25302

25861

26359

26789

27155

27508

Original

07-14-08

08.01.107

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

45.0

23559

24188

24812

25410

25966

26464

26891

27250

27592

45.2

23674

24302

24923

25517

26069

26568

26994

27345

27676

45.4

23789

24415

25033

25622

26171

26670

27096

27440

27760

45.6

23902

24527

25142

25725

26271

26771

27197

27534

27845

45.8

24015

24638

25250

25827

26369

26870

27296

27628

27929

46.0

24127

24747

25356

25928

26467

26968

27394

27720

28012

46.2

24238

24856

25461

26028

26563

27064

27489

27811

28095

46.4

24347

24964

25566

26128

26658

27158

27582

27899

28177

46.6

24456

25070

25669

26227

26753

27250

27671

27984

28258

46.8

24562

25175

25771

26325

26847

27339

27756

28066

28337

47.0

24668

25279

25872

26424

26941

27427

27839

28146

28415

47.2

24773

25381

25973

26522

27034

27513

27918

28223

28491

47.4

24877

25484

26074

26620

27127

27598

27996

28297

28565

47.6

24981

25586

26174

26717

27220

27682

28071

28369

28637

47.8

25085

25688

26274

26815

27313

27765

28146

28440

28707

48.0

25189

25789

26374

26913

27406

27849

28220

28509

28774

48.2

25293

25892

26474

27012

27499

27932

28294

28577

28839

48.4

25398

25995

26575

27110

27592

28016

28368

28645

28901

48.6

25504

26099

16677

27209

27685

28101

28443

28711

28960

48.8

25611

26204

26780

27308

27779

28187

28519

28777

29016

49.0

25719

26309

26883

27407

27873

28273

28597

28843

29069

49.2

25827

26415

26986

27506

27966

28360

28675

28909

29120

49.4

25934

26520

27088

27604

28059

28447

28753

28974

29169

49.6

26042

26625

27190

27701

28150

28533

28831

29038

29217

08.01.108

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

49.8

26148

26729

27290

27796

28239

28618

28909

29102

29264

50.0

26252

26830

27388

27888

28327

28702

28985

29166

29311

50.2

26355

26930

27484

27979

28412

28783

29061

29229

29358

50.4

26455

27027

27577

28066

28494

28862

29134

29291

29406

50.6

26553

27121

27666

28150

28573

28938

29206

29353

29454

50.8

26647

27211

27752

28230

28648

29011

29274

29414

29505

51.0

26739

27299

27835

28307

28721

29080

29341

29474

29556

51.2

26828

27383

27915

28381

28790

29147

29404

29533

29608

51.4

26914

27466

27992

28453

28858

29211

29466

29590

29660

51.6

27000

27547

28068

28524

28924

29274

29526

29646

29712

51.8

27083

27626

28143

28594

28989

29334

29581

29699

29763

52.0

27166

27705

28217

28664

29054

29393

29636

29751

29812

52.2

27249

27783

28291

28734

29119

29451

29688

29800

29860

52.4

27331

27861

28365

28805

29185

29509

29737

29846

29905

52.6

27414

27940

28441

28877

29252

29566

29785

29890

29947

52.8

27498

28020

28518

28952

29320

29623

29831

29930

29986

53.0

27581

28100

28595

29027

29390

29680

29875

29968

30022

53.2

27666

28181

28674

29104

29461

29736

29917

30003

30055

53.4

27750

28262

28753

29181

29531

29793

29958

30037

30086

53.6

27834

28343

28832

29258

29602

29848

29999

30069

30115

53.8

27919

28424

28910

29334

29671

29903

30039

30101

30143

54.0

28002

28504

28987

29409

29739

29958

30079

30132

30170

Original

07-14-08

08.01.109

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

3.0

677

743

831

1009

1287

1701

2220

2829

3453

3.2

711

779

869

1049

1335

1768

2307

2925

3553

3.4

746

816

908

1091

1385

1836

2393

3020

3652

3.6

782

855

949

1135

1437

1906

2480

3115

3752

3.8

819

895

992

1183

1493

1978

2567

3210

3852

4.0

857

937

1039

1235

1553

2052

2654

3305

3951

4.2

898

982

1088

1291

1618

2128

2742

3399

4049

4.4

940

1030

1142

1352

1689

2208

2831

3493

4148

4.6

985

1080

1200

1419

1765

2292

2920

3586

4246

4.8

1033

1135

1262

1493

1848

2379

3009

3679

4343

5.0

1083

1192

1329

1572

1938

2470

3100

3772

4440

5.2

1135

1253

1400

1656

2032

2564

3192

3865

4537

5.4

1190

1316

1474

1744

2130

2662

3285

3958

4635

5.6

1248

1383

1551

1836

2232

2761

3379

4053

4732

5.8

1307

1451

1631

1930

2337

2863

3476

4149

4831

6.0

1369

1522

1713

2026

2443

2967

3574

4246

4931

6.2

1434

1595

1797

2123

2550

3073

3675

4346

5032

6.4

1500

1670

1882

2221

2657

3180

3778

4448

5134

6.6

1569

1747

1968

2318

2764

3288

3884

4552

5239

6.8

1640

1825

2054

2414

2869

3396

3993

4660

5345

7.0

1712

1904

2141

2510

2972

3505

4104

4770

5453

7.2

1786

1984

2228

2604

3074

3614

4218

4883

5563

7.4

1862

2065

2315

2698

3176

3724

4333

4998

5675

08.01.110

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

7.6

1937

2147

2403

2792

3277

3834

4449

5114

5787

7.8

2014

2229

2490

2886

3378

3944

4567

5231

5902

8.0

2090

2310

2578

2980

3479

4055

4685

5350

6017

8.2

2166

2392

2666

3074

3581

4166

4803

5468

6133

8.4

2241

2474

2754

3169

3683

4277

4920

5587

6249

8.6

2315

2555

2842

3264

3786

4388

5037

5705

6366

8.8

2388

2635

2931

3361

3891

4500

5153

5823

6484

9.0

2460

2715

3019

3459

3997

4612

5269

5940

6602

9.2

2531

2795

3109

3557

4104

4724

5383

6056

6720

9.4

2603

2876

3200

3658

4213

4836

5498

6173

6838

9.6

2676

2958

3292

3760

4323

4950

5612

6289

6956

9.8

2751

3041

3386

3864

4435

5064

5726

6405

7075

10.0

2827

3127

3482

3969

4548

5179

5841

6521

7193

10.2

2906

3215

3580

4077

4663

5295

5956

6638

7312

10.4

2988

3307

3681

4187

4779

5412

6073

6755

7431

10.6

3074

3402

3786

4299

4897

5530

6191

6873

7549

10.8

3165

3501

3893

4414

5016

5650

6310

6991

7667

11.0

3259

3604

4004

4531

5136

5772

6430

7110

7786

11.2

3356

3709

4118

4650

5258

5894

6552

7230

7904

11.4

3455

3817

4233

4770

5381

6017

6675

7351

8023

11.6

3557

3927

4350

4891

5504

6141

6798

7472

8142

11.8

3660

4039

4468

5014

5628

6266

6922

7594

8261

12.0

3764

4151

4587

5136

5752

6391

7047

7717

8381

Original

07-14-08

08.01.111

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

12.2

3868

4263

4706

5259

5876

6516

7172

7839

8501

12.4

3972

4375

4825

5381

6000

6641

7298

7963

8622

12.6

4075

4486

4943

5503

6123

6766

7423

8087

8744

12.8

4176

4596

5060

5624

6246

6891

7548

8211

8866

13.0

4277

4705

5176

5744

6369

7015

7674

8335

8990

13.2

4376

4813

5292

5864

6491

7140

7799

8460

9114

13.4

4475

4920

5406

5983

6613

7264

7924

8585

9238

13.6

4574

5027

5521

6103

6735

7388

8049

8710

9363

13.8

4673

5134

5636

6222

6857

7512

8174

8835

9488

14.0

4772

5242

5751

6342

6980

7636

8299

8960

9614

14.2

4872

5350

5867

6462

7103

7760

8424

9086

9739

14.4

4973

5459

5983

6583

7226

7885

8549

9211

9865

14.6

5075

5570

6101

6704

7350

8009

8674

9336

9990

14.8

5179

5682

6220

6827

7474

8135

8799

9461

10116

15.0

5285

5795

6340

6951

7600

8260

8924

9586

10240

15.2

5392

5910

6461

7076

7726

8386

9049

9711

10365

15.4

5501

6026

6584

7201

7852

8512

9175

9835

10490

15.6

5611

6144

6707

7327

7979

8638

9300

9960

10614

15.8

5722

6262

6830

7454

8106

8765

9426

10085

10739

16.0

5835

6381

6955

7580

8234

8892

9551

10210

10863

16.2

5949

6501

7080

7708

8361

9018

9677

10335

10988

16.4

6064

6622

7205

7835

8489

9145

9803

10460

11112

16.6

6180

6743

7330

7962

8616

9272

9928

10585

11237

16.8

6297

6865

7456

8089

8743

9399

10054

10710

11362

08.01.112

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

17.0

6415

6987

7581

8216

8871

9526

10181

10835

11487

17.2

6534

7110

7707

8343

8998

9653

10307

10961

11612

17.4

6653

7232

7832

8470

9125

9779

10433

11087

11737

17.6

6773

7355

7958

8596

9252

9906

10560

11213

11862

17.8

6893

7479

8083

8723

9379

10033

10686

11338

11988

18.0

7013

7602

8209

8850

9506

10160

10813

11464

12113

18.2

7133

7725

8335

8976

9632

10287

10939

11590

12239

18.4

7252

7848

8460

9103

9759

10414

11066

11716

12364

18.6

7372

7971

8586

9229

9886

10540

11192

11842

12490

18.8

7491

8094

8711

9356

10013

10667

11319

11968

12615

19.0

7609

8216

8837

9483

10140

10794

11445

12094

12741

19.2

7728

8339

8963

9610

10267

10921

11572

12220

12866

19.4

7846

8462

9088

9736

10393

11047

11698

12346

12992

19.6

7965

8584

9214

9863

10520

11174

11825

12472

13117

19.8

8084

8707

9340

9990

10647

11301

11951

12598

13243

20.0

8203

8830

9466

10117

10774

11427

12078

12724

13368

20.2

8323

8954

9592

10244

10900

11554

12204

12850

13494

20.4

8444

9078

9718

10370

11027

11680

12330

12976

13620

20.6

8566

9202

9844

10497

11154

11807

12456

13102

13745

20.8

8689

9327

9971

10624

11280

11933

12582

13227

13871

21.0

8813

9453

10097

10751

11407

12059

12708

13353

13996

21.2

8938

9579

10224

10877

11533

12185

12834

13479

14122

21.4

9063

9705

10351

11004

11660

12312

12960

13604

14248

Original

07-14-08

08.01.113

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

21.6

9189

9832

10478

11131

11786

12438

13086

13730

14373

21.8

9315

9958

10605

11258

11912

12564

13211

13856

14499

22.0

9442

10085

10732

11385

12039

12690

13337

13981

14624

22.2

9569

10212

10859

11511

12165

12816

13463

14107

14749

22.4

9696

10339

10986

11638

12292

12942

13588

14232

14875

22.6

9822

10466

11113

11765

12418

13068

13714

14357

15000

22.8

9948

10593

11240

11892

12545

13194

13839

14482

15125

23.0

10074

10720

11367

12019

12671

13320

13965

14608

15249

23.2

10200

10846

11494

12146

12798

13446

14091

14733

15374

23.4

10326

10973

11621

12273

12924

13572

14216

14858

15499

23.6

10451

11099

11748

12400

13051

13698

14342

14983

15624

23.8

10577

11225

11875

12527

13177

13824

14467

15108

15748

24.0

10702

11351

12001

12653

13304

13950

14593

15233

15873

24.2

10827

11477

12128

12780

13430

14076

14718

15358

15997

24.4

10953

11604

12255

12907

13557

14202

14844

15483

16122

24.6

11078

11730

12381

13033

13683

14328

14969

15608

16246

24.8

11204

11856

12508

13159

13809

14453

15095

15733

16371

25.0

11330

11982

12634

13286

13934

14579

15220

15859

16496

25.2

11456

12108

12761

13412

14060

14705

15346

15984

16621

25.4

11582

12235

12887

13538

14186

14830

15471

16109

16745

25.6

11708

12361

13013

13664

14311

14956

15597

16234

16870

25.8

11834

12487

13140

13789

14437

15081

15722

16359

16995

26.0

11960

12613

13266

13915

14562

15206

15847

16484

17120

26.2

12086

12740

13392

14041

14688

15332

15973

16609

17244

08.01.114

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

26.4

12213

12866

13518

14167

14813

15457

16098

16734

17369

26.6

12339

12992

13644

14293

14938

15582

16223

16859

17493

26.8

12466

13118

13770

14418

15064

15707

16347

16983

17618

27.0

12592

13245

13896

14544

15189

15832

16472

17108

17742

27.2

12718

13371

14022

14670

15315

15957

16597

17232

17866

27.4

12845

13497

14148

14796

15440

16082

16721

17356

17990

27.6

12971

13623

14274

14921

15566

16207

16846

17481

18114

27.8

13098

13750

14400

15047

15691

16332

16970

17605

18238

28.0

13224

13876

14526

15173

15817

16457

17095

17729

18362

28.2

13351

14002

14652

15299

15942

16582

17219

17853

18485

28.4

13477

14128

14778

15425

16068

16707

17344

17977

18609

28.6

13604

14255

14904

15550

16193

16832

17468

18101

18732

28.8

13731

14381

15030

15676

16318

16957

17593

18225

18855

29.0

13857

14507

15156

15802

16444

17082

17718

18349

18979

29.2

13984

14634

15283

15927

16569

17207

17842

18472

19102

29.4

14111

14760

15408

16053

16694

17332

17967

18596

19225

29.6

14237

14886

15534

16178

16819

17457

18092

18720

19348

29.8

14364

15013

15660

16304

16944

17582

18216

18844

19471

30.0

14490

15139

15786

16429

17070

17707

18341

18968

19594

30.2

14617

15265

15912

16555

17194

17832

18466

19092

19718

30.4

14743

15391

16037

16680

17319

17957

18590

19217

19842

30.6

14869

15517

16163

16805

17444

18081

18714

19341

19966

30.8

14995

15642

16288

16930

17569

18205

18838

19465

20090

Original

07-14-08

08.01.115

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

31.0

15121

15768

16413

17055

17693

18330

18963

19589

20214

31.2

15246

15893

16538

17180

17818

18454

19086

19713

20338

31.4

15372

16018

16664

17304

17942

18578

19210

19837

20462

31.6

15498

16144

16789

17429

18067

18702

19334

19960

20586

31.8

15623

16269

16913

17554

18191

18826

19458

20084

20709

32.0

15749

16394

17038

17679

18316

18950

19581

20207

20831

32.2

15874

16519

17163

17803

18440

19074

19705

20329

20953

32.4

15999

16645

17288

17928

18564

19198

19828

20452

21074

32.6

16125

16770

17413

18053

18689

19322

19952

20573

21193

32.8

16251

16895

17538

18178

18814

19447

20075

20694

21312

33.0

16376

17020

17664

18302

18938

19571

20198

20815

21429

33.2

16502

17146

17789

18427

19063

19696

20322

20935

21545

33.4

16628

17271

17914

18552

19188

19820

20445

21054

21661

33.6

16753

17397

18039

18677

19312

19945

20568

21174

21776

33.8

16879

17522

18164

18802

19437

20069

20692

21293

21891

34.0

17005

17647

18289

18927

19561

20194

20815

21412

22005

34.2

17130

17773

18414

19051

19686

20318

20939

21532

22120

34.4

17256

17898

18539

19176

19810

20442

21062

21651

20234

34.6

17381

18023

18664

19300

19934

20567

21185

21771

22349

34.8

17507

18148

18789

19424

20058

20691

21309

21891

22465

35.0

17632

18273

18913

19548

20181

20815

21432

22011

22581

35.2

17757

18398

19038

19672

20305

20939

21556

22131

22697

35.4

17882

18523

19162

19796

20428

21062

21679

22251

22814

35.6

18007

18647

19286

19919

20552

21186

21801

22371

22930

08.01.116

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

35.8

18132

18772

19410

20043

20675

21309

21923

22490

23046

36.0

18257

18896

19534

20167

20798

21431

22045

22609

23162

36.2

18382

19021

19658

20290

20921

21554

22166

22727

23277

36.4

18506

19145

19782

20414

21044

21676

22285

22844

23392

36.6

18630

19269

19906

20538

21168

21797

22404

22960

23505

36.8

18755

19393

20030

20662

21291

21918

22522

23076

23618

37.0

18879

19517

20154

20786

21415

22038

22639

23190

23730

37.2

19003

19640

20278

20910

21538

22159

22755

23303

23841

37.4

19127

19764

20401

21034

21661

22279

22871

23415

23951

37.6

19251

19888

20525

21158

21785

22398

22986

23527

24060

37.8

19375

20012

20649

21282

21908

22518

23101

23639

24168

38.0

19499

20136

20773

21406

22031

22638

23216

23749

24276

38.2

19623

20260

20897

21530

22154

22757

23332

23860

24382

38.4

19748

20384

21021

21654

22277

22877

23447

23971

24487

38.6

19873

20509

21145

21778

22400

22997

23564

24081

24592

38.8

19999

20633

21269

21901

22522

23118

23681

24192

24695

39.0

20124

20758

21393

22024

22644

23238

23798

24302

24798

39.2

20250

20883

21517

22147

22766

23359

23916

24413

24901

39.4

20375

21008

23641

22269

22887

23479

24033

24523

25003

39.6

20501

21132

21764

22391

23007

23599

24150

24633

25105

39.8

20625

21256

21887

22512

23127

23718

24267

24743

25207

40.0

20749

21379

22009

22633

23246

23836

24383

24853

25309

40.2

20873

21502

22130

22752

23363

23953

24498

24963

25412

Original

07-14-08

08.01.117

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

40.4

20995

21623

22251

22871

23480

24068

24611

25072

25516

40.6

21116

21744

22370

22989

23596

24182

24723

25180

25620

40.8

21235

21863

22489

23105

23710

24295

24833

25288

25725

41.0

21353

21981

22606

23221

23823

24406

24942

25395

25831

41.2

21471

22098

22723

23336

23936

24515

25048

25502

25938

41.4

21587

22215

22839

23450

24047

24623

25154

25607

26044

41.6

21703

22331

22955

23564

24159

24731

25258

25711

26149

41.8

21819

22447

23070

23678

24270

24838

25361

25814

26252

42.0

21934

22562

23186

23793

24382

24944

25463

25915

26354

42.2

22049

22678

23302

23907

24494

25050

25564

26015

26454

42.4

22165

22794

23418

24022

24606

25157

25664

26113

26551

42.6

22280

22910

23534

24138

24719

25263

25764

26209

26644

42.8

22397

23027

23652

24255

24833

25370

25863

26303

26734

43.0

22513

23144

23769

24373

24948

25478

25962

26395

26821

43.2

22630

23261

23887

24490

25063

25585

26060

26486

26905

43.4

22748

23379

24005

24608

25178

25692

26158

26576

26988

43.6

22865

23496

24123

24725

25292

25800

26256

26664

27068

43.8

22982

23613

24240

24842

25406

25906

26355

26753

27147

44.0

23098

23729

24356

24957

25518

26013

26453

26841

27226

44.2

23215

23845

24472

25071

25628

26118

26551

26930

27304

44.4

23330

23960

24586

25182

25737

26223

26650

27019

27383

44.6

23445

24074

24698

25292

25843

26326

26749

27110

27463

44.8

23560

24187

24809

25399

25946

26428

26848

27201

27545

45.0

23673

24299

24918

25503

26047

26528

26947

27293

27627

08.01.118

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

45.2

23785

24410

25026

25606

26145

26627

27046

27386

27710

45.4

23897

24519

25132

25706

26241

26725

27144

27478

27793

45.6

24008

24628

25237

25805

26336

26821

27241

27570

27877

45.8

24117

24735

25341

25903

26430

26916

27337

27661

27960

46.0

24226

24841

25443

26000

26522

27009

27431

27750

28043

46.2

24334

24947

25545

26097

26614

27101

27522

27838

28124

46.4

24441

25051

25646

26193

26706

27191

27611

27923

28204

46.6

24546

25154

25746

26288

26797

27280

27697

28005

28282

46.8

24651

25257

25846

26384

26889

27367

27779

28084

28359

47.0

24755

25358

25945

26481

26981

27452

27858

28161

28433

47.2

24858

25459

26044

26577

27073

27536

27935

28234

28504

47.4

24961

25560

26143

26673

27165

27620

28011

28305

28574

47.6

25063

25661

26241

26769

27257

27702

28084

28375

28642

47.8

25166

25761

26340

26866

27349

27785

28157

28443

28707

48.0

25269

25862

26438

26962

27440

27867

28230

28509

28770

48.2

25373

25963

26537

27058

27532

27949

28302

28575

28831

48.4

25477

26065

26636

27154

27623

28032

28376

28641

28890

48.6

25582

26167

26735

27250

27714

28115

28450

28706

28946

48.8

25689

26270

26835

27346

27804

28199

28526

28771

29000

49.0

25796

26374

26935

27441

27894

28283

28603

28836

29053

49.2

25903

26478

27034

27536

27983

28368

28681

28902

29103

49.4

26010

26581

27133

27629

28070

28452

28759

28967

29153

49.6

26117

26684

27231

27721

28157

28535

28837

29032

29202

Original

07-14-08

08.01.119

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER ONE (WSTA 189.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) STICK LEVEL IN INCHS

USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

49.8

26221

26785

27327

27811

28241

28617

28914

29096

29251

50.0

26325

26884

27421

27900

28324

28697

28989

29160

29300

50.2

26426

26981

27513

27986

28404

28775

29063

29223

29349

50.4

26524

27075

27603

28069

28482

28851

29135

29286

29398

50.6

26618

27165

27689

28149

28557

28923

29204

29347

29450

50.8

26710

27253

27772

28227

28630

28993

29270

29407

29502

51.0

26797

27337

27852

28302

28700

29059

29333

29466

29555

51.2

26883

27418

27929

28374

28768

29123

29393

29524

29609

51.4

26966

27497

28004

28445

28834

29185

29450

29580

29663

51.6

27047

27575

28078

28515

28900

29245

29505

29634

29716

51.8

27127

27652

28152

28585

28965

29303

29558

29686

29768

52.0

27206

27728

28224

28654

29030

29361

29609

29736

29818

52.2

27286

27804

28297

28724

29096

29418

29658

29784

29866

52.4

27365

27880

28371

28795

29163

29474

29705

29829

29911

52.6

27446

27957

28445

28867

29231

29531

29751

29871

29953

52.8

27528

28036

28522

28942

29301

29589

29796

29911

29991

53.0

27611

28116

28599

29018

29372

29646

29840

29948

30025

53.2

27694

28197

28677

29095

29443

29704

29883

29984

30056

53.4

27779

28277

28756

29172

29515

29762

29926

30018

30085

53.6

27863

28358

28834

29248

29586

29819

29968

30050

30112

53.8

27946

28438

28911

29323

29655

29875

30011

30083

30138

54.0

28030

28518

28987

29396

29722

29930

30053

30115

30163

08.01.120

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

103

100

97

95

94

92

90

89

88

3.2

115

112

110

108

107

105

104

103

101

3.4

129

126

124

122

120

119

118

117

115

3.6

143

140

138

136

134

133

132

131

130

3.8

158

155

153

151

149

148

146

146

144

4.0

174

171

169

167

165

163

162

161

159

4.2

192

188

186

184

182

180

178

177

175

4.4

211

207

205

202

199

197

195

194

192

4.6

232

228

225

221

218

215

213

211

209

4.8

255

250

246

242

239

235

232

230

227

5.0

280

274

269

265

260

256

252

249

246

5.2

306

299

294

288

283

277

273

269

265

5.4

333

325

318

312

306

300

294

290

285

5.6

361

351

344

336

329

322

316

311

305

5.8

389

378

369

361

352

345

338

332

325

6.0

416

404

395

385

376

367

359

353

346

6.2

444

430

419

409

399

389

381

374

366

6.4

470

456

444

432

421

411

402

394

385

6.6

496

480

467

454

442

432

422

414

405

6.8

520

503

488

475

463

451

442

433

424

7.0

543

525

509

495

482

471

461

452

442

Original

07-14-08

08.01.121

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

565

546

530

515

502

490

480

471

461

7.4

588

568

551

535

522

509

499

490

480

7.6

612

590

572

556

542

530

519

510

499

7.8

637

614

595

578

564

551

540

531

520

8.0

663

639

619

602

587

574

563

553

542

8.2

692

667

646

628

612

599

587

577

566

8.4

724

698

676

656

640

626

614

604

592

8.6

759

732

708

688

671

656

644

632

620

8.8

798

769

745

724

706

690

676

664

651

9.0

840

810

785

762

743

726

711

698

684

9.2

886

854

828

804

783

765

749

735

719

9.4

933

901

873

847

825

805

788

773

756

9.6

983

949

920

893

869

847

828

812

793

9.8

1034

999

968

939

914

891

870

852

832

10.0

1087

1049

1017

987

960

934

912

893

871

10.2

1140

1100

1066

1034

1005

978

955

933

911

10.4

1192

1151

1116

1082

1051

1022

997

974

950

10.6

1245

1202

1164

1129

1096

1065

1038

1014

988

10.8

1296

1251

1212

1174

1140

1107

1078

1053

1026

11.0

1347

1300

1258

1219

1182

1148

1118

1091

1062

11.2

1397

1347

1304

1263

1225

1189

1157

1128

1098

11.4

1446

1395

1349

1306

1266

1229

1195

1166

1134

08.01.122

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.6

1496

1442

1394

1349

1308

1269

1234

1203

1170

11.8

1545

1489

1439

1393

1349

1309

1272

1240

1206

12.0

1595

1537

1485

1436

1391

1349

1311

1278

1242

12.2

1645

1585

1531

1480

1433

1390

1351

1316

1279

12.4

1696

1633

1577

1525

1476

1431

1391

1355

1317

12.6

1747

1682

1624

1570

1521

1474

1432

1395

1356

12.8

1799

1733

1673

1617

1566

1518

1475

1437

1397

13.0

1853

1784

1723

1666

1613

1563

1519

1480

1438

13.2

1907

1837

1774

1715

1661

1610

1565

1524

1481

13.4

1963

1891

1826

1766

1710

1658

1611

1570

1526

13.6

2021

1947

1880

1818

1761

1707

1659

1617

1571

13.8

2079

2003

1935

1872

1813

1758

1709

1665

1618

14.0

2140

2062

1992

1927

1867

1810

1759

1714

1666

14.2

2202

2122

2050

1984

1922

1864

1811

1765

1716

14.4

2265

2183

2110

2042

1978

1918

1865

1817

1766

14.6

2331

2247

2172

2101

2036

1975

1919

1870

1817

14.8

2398

2312

2235

2162

2095

2032

1975

1924

1870

15.0

2467

2378

2299

2225

2156

2091

2032

1979

1923

15.2

2537

2446

2365

2288

2217

2150

2089

2035

1977

15.4

2609

2515

2432

2353

2279

2210

2147

2091

2032

15.6

2681

2584

2499

2418

2342

2271

2206

2148

2087

15.8

2753

2654

2566

2483

2405

2332

2265

2205

2142

Original

07-14-08

08.01.123

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.0

2826

2724

2634

2548

2468

2392

2323

2262

2197

16.2

2898

2794

2701

2613

2530

2453

2382

2318

2251

16.4

2970

2863

2768

2677

2593

2513

2440

2374

2305

16.6

3041

2932

2834

2741

2654

2572

2497

2429

2358

16.8

3111

2999

2899

2804

2715

2630

2553

2484

2411

17.0

3180

3066

2963

2866

2774

2688

2609

2538

2463

17.2

3249

3132

3027

2927

2834

2745

2664

2591

2514

17.4

3318

3199

3091

2989

2894

2803

2720

2645

2566

17.6

3387

3265

3155

3051

2954

2861

2776

2699

2618

17.8

3457

3333

3221

3114

3015

2920

2833

2754

2671

18.0

3528

3401

3287

3178

3076

2980

2891

2810

2726

18.2

3601

3471

3354

3244

3140

3041

2950

2868

2782

18.4

3675

3543

3424

3311

3205

3104

3011

2927

2839

18.6

3751

3617

3495

3380

3272

3169

3075

2989

2899

18.8

3830

3693

3569

3452

3342

3237

3141

3053

2962

19.0

3912

3772

3646

3526

3414

3307

3209

3119

3026

19.2

3995

3852

3724

3602

3487

3378

3279

3188

3093

19.4

4080

3934

3803

3679

3563

3452

3350

3258

3161

19.6

4156

4017

3884

3758

3639

3526

3423

3329

3230

19.8

4253

4102

3966

3837

3717

3602

3496

3401

3301

20.0

4341

4187

4049

3918

3795

3678

3571

3474

3372

20.2

4430

4273

4132

3998

3873

3754

3645

3547

3443

08.01.124

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

20.4

4519

4358

4215

4079

3952

3831

3720

3620

3514

20.6

4608

4444

4298

4160

4030

3907

3794

3692

3585

20.8

4696

4529

4381

4240

4108

3983

3868

3764

3655

21.0

4784

4615

4463

4320

4185

4058

3941

3836

3724

21.2

4872

4699

4545

4399

4262

4133

4014

3907

3794

21.4

4964

4784

4627

4478

4339

4207

4087

3978

3862

21.6

5048

4869

4708

4557

4416

4282

4159

4048

3931

21.8

5136

4953

4790

4636

4492

4356

4232

4119

4000

22.0

5224

5038

4872

4715

4569

4431

4304

4189

4068

22.2

5312

5123

4954

4795

4646

4506

4377

4260

4137

22.4

5400

5208

5036

4875

4724

4581

4450

4331

4206

22.6

5489

5294

6119

4955

4801

4656

4523

4403

4276

22.8

5578

5380

5202

5035

4879

4732

4597

4475

4346

23.0

5668

5466

5286

5116

4958

4809

4672

4548

4417

23.2

5759

5553

5370

5198

5038

4886

4747

4621

4488

23.4

5850

5641

5456

5281

5118

4964

4823

4696

4561

23.6

5943

5731

5542

5365

5199

5043

4900

4771

4634

23.8

6037

5821

5629

5449

5282

5123

4978

4847

4708

24.0

6132

5912

5718

5535

5365

5204

5057

4924

4783

24.2

6230

6005

5808

5622

5449

5286

5137

5002

4859

24.4

6328

6100

5899

5711

5535

5369

5218

5081

4936

24.6

6429

6197

5992

5800

5622

5454

5300

5161

5014

Original

07-14-08

08.01.125

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

24.8

6532

6295

6087

5892

5710

5539

5383

5243

5093

25.0

6637

6395

6183

5984

5800

5626

5468

5325

5173

25.2

6743

6496

6280

6078

5891

5714

5553

5408

5254

25.4

6851

6598

6378

6172

5982

5802

5639

5492

5335

25.6

6959

6701

6476

6267

6074

5891

5725

5576

5417

25.8

7067

6805

6575

6362

6166

5980

5812

5660

5499

26.0

7176

6908

6674

6458

6258

6070

5898

5745

5581

26.2

7284

7011

6773

6553

6350

6159

5985

5829

5663

26.4

7391

7113

6871

6647

6441

6247

6071

5913

5744

26.6

7498

7215

6968

6741

6532

6335

6156

5996

5825

26.8

7603

7315

7064

6834

6622

6423

6241

6079

5906

27.0

7708

7415

7160

6926

6712

6510

6326

6161

5986

27.2

7811

7514

7255

7018

6801

6596

6410

6244

6066

27.4

7915

7613

7351

7111

6890

6683

6494

6326

6145

27.6

8020

7713

7446

7203

6980

6769

6578

6408

6225

27.8

8125

7813

7543

7296

7070

6857

6663

6491

6306

28.0

8232

7915

7641

7390

7161

6945

6749

6574

6387

28.2

8341

8019

7740

7486

7253

7034

6836

6659

6469

28.4

8452

8124

7841

7583

7347

7125

6924

6745

6552

28.6

8567

8232

7944

7682

7442

7217

7013

6832

6637

28.8

8684

8343

8050

7783

7540

7311

7104

6921

6723

29.0

8805

8457

8158

7886

7639

7407

7197

7012

6811

08.01.126

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

29.2

8928

8573

8268

7992

7740

7504

7292

7103

6900

29.4

9053

9691

8380

8098

7842

7603

7387

7196

6990

29.6

9181

8811

8494

8207

7946

7702

7484

7290

7081

29.8

9310

8932

8608

8316

8050

7803

7581

7385

7173

30.0

9441

9055

8724

8426

8156

7904

7679

7480

7266

30.2

9573

9178

8841

8537

8262

8006

7777

7576

7358

30.4

9705

9302

8958

8648

8368

8108

7876

7672

7452

30.6

9838

9426

9075

8759

8474

8210

7975

7768

7545

30.8

9971

9551

9192

8870

8580

8312

8074

7865

7638

31.0

10104

9675

9309

8981

8687

8414

8172

7961

7731

31.2

10237

9799

9426

9092

8793

8516

8271

8056

7824

31.4

10370

9924

9544

9203

8899

8618

8370

8152

7917

31.6

10503

10048

9661

9314

9005

8720

8468

8248

8010

31.8

10636

10173

9778

9426

9111

8822

8567

8344

8103

32.0

10769

10297

9895

9537

9217

8924

8665

8440

8196

32.2

10902

10422

10012

9648

9323

9026

8764

8536

8289

32.4

11036

10547

10130

9759

9429

9128

8862

8632

8381

32.6

11169

10671

10247

9871

9536

9230

8961

8728

8474

32.8

11303

10796

10365

9982

9642

9333

9060

8824

8568

33.0

11437

10921

10483

10094

9749

9435

9159

8921

8661

33.2

11571

11047

10602

10207

9857

9539

9259

9018

8755

33.4

11708

11174

10722

10321

9966

9642

9359

9115

8849

Original

07-14-08

08.01.127

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

33.6

11845

11303

10843

10436

10075

9747

9461

9214

8944

33.8

11985

11434

10966

10552

10186

9854

9563

9313

9040

34.0

12127

11566

11091

10671

10299

9961

9667

9413

9137

34.2

12272

11701

11218

10791

10413

10070

9772

9515

9235

34.4

12421

11839

11348

10914

10530

10182

9878

9618

9334

34.6

12572

11981

11481

11039

10648

10295

9987

9723

9435

34.8

12728

12126

11616

11167

10770

10410

10097

9830

9537

35.0

12887

12274

11755

11297

10893

10527

10209

9938

9641

35.2

13049

12424

11896

11430

11018

10646

10323

10047

9746

35.4

13214

12577

12038

11564

11145

10766

10437

10158

9851

35.6

13379

12731

12182

11699

11273

10888

10553

10269

9958

35.8

13546

12885

12327

11835

11401

11009

10669

10380

10065

36.0

13714

13041

12472

11971

11530

11131

10785

10492

10172

36.2

13881

13196

12617

12108

11659

11253

10901

10604

10279

36.4

14048

13351

12762

12244

11787

11375

11017

10715

10385

36.6

14213

13505

12905

12378

11914

11495

11132

10826

10491

36.8

14377

13657

13048

12512

12041

11615

11246

10936

10597

37.0

14540

13808

13189

12645

12166

11734

11360

11045

10702

37.2

14701

13958

13329

12777

12291

11853

11473

11154

10806

37.4

14863

14108

13470

12909

12416

11971

11586

11263

10911

37.6

15024

14258

13610

13041

12541

12090

11699

11372

11016

37.8

15187

14409

13751

13174

12667

12209

11813

11482

11121

08.01.128

07-14-08

1.00

1.50

2.00

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

38.0

15351

14561

13893

13308

12793

12329

11927

11592

11226

38.2

15516

14715

14037

13443

12921

12450

12043

11703

11332

38.4

15684

14870

14182

13579

13050

12572

12159

11815

11440

38.6

15854

15029

14330

13718

13181

12696

12278

11929

11548

38.8

16028

15190

14480

13859

13314

12822

12398

12044

11658

39.0

16205

15354

14633

14002

13449

12950

12519

12160

11769

39.2

16385

15520

14788

14148

13586

13080

12643

12278

11882

39.4

16567

15689

14945

14295

13725

13211

12767

12398

11996

39.6

16751

15860

15104

14444

13865

13343

12893

12518

12110

39.8

16938

16032

15264

14594

14006

13477

13020

12639

12226

40.0

17126

16206

15426

14745

14149

13612

13148

12762

12342

40.2

17315

16381

15589

14897

14292

13747

13277

12885

12459

40.4

17505

16557

15752

15051

14437

13883

13406

13008

12576

40.6

17696

16734

15916

15204

14581

14020

13536

13132

12694

40.8

17888

16911

16081

15358

14726

14157

13666

13257

12812

41.0

18080

17089

16246

15513

14872

14295

13797

13381

12931

41.2

18273

17267

16411

15668

15018

14432

13927

13506

13050

41.4

18466

17445

16577

15823

15164

14570

14058

13631

13169

41.6

18659

17624

16743

15978

15310

14708

14189

13757

13288

41.8

18852

17803

16909

16133

15456

14847

14321

13882

13407

42.0

19046

17982

17075

16288

15602

14985

14452

14008

13527

42.2

19240

18161

17241

16444

15749

15124

14584

14133

13646

Original

07-14-08

08.01.129

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

42.4

19433

18340

17407

16599

15895

15262

14715

14259

13765

42.6

19627

18519

17573

16755

16042

15400

14847

14384

13885

42.8

19821

18699

17739

16910

16188

15539

14978

14510

14004

43.0

20014

18878

17905

17066

16334

15677

15109

14635

14124

43.2

20208

19057

18071

17221

16481

15815

15241

14761

14243

43.4

20401

19235

18237

17376

16627

15953

15372

14886

14362

43.6

20593

19414

18402

17531

16773

16091

15503

15011

14481

43.8

20785

19592

18567

17685

16918

16229

15634

15136

14600

FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

114

111

108

106

104

102

100

99

98

3.2

127

124

122

120

118

116

115

114

112

3.4

141

138

136

134

132

131

130

128

127

3.6

156

153

151

149

147

146

145

144

142

3.8

172

169

167

165

163

162

160

159

158

4.0

190

186

184

182

180

178

177

176

174

4.2

208

204

202

200

197

195

194

192

191

08.01.130

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

4.4

229

224

221

219

216

214

212

210

208

4.6

251

246

243

239

236

233

231

229

226

4.8

275

269

265

261

257

254

251

248

245

5.0

301

294

290

285

280

275

272

268

265

5.2

329

321

315

309

303

298

293

289

285

5.4

357

348

341

334

327

321

316

311

306

5.6

386

376

368

360

352

344

338

332

326

5.8

416

404

395

385

376

368

361

354

347

6.0

445

432

421

411

401

392

383

376

369

6.2

474

459

447

436

425

415

406

398

389

6.4

502

486

473

460

448

437

428

419

410

6.6

529

512

497

484

471

459

449

440

430

6.8

554

536

520

506

492

480

470

460

450

7.0

579

559

542

527

513

501

490

480

470

7.2

603

582

564

548

534

521

510

500

490

7.4

627

605

585

569

555

542

531

521

510

7.6

652

628

608

591

576

563

552

542

531

7.8

678

653

632

614

599

586

574

564

553

8.0

706

680

657

639

624

610

598

588

576

8.2

737

709

685

666

650

636

624

613

601

8.4

770

741

716

696

680

665

652

641

628

8.6

807

776

751

730

712

697

683

671

658

Original

07-14-08

08.01.131

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

8.8

847

816

789

767

748

731

717

704

690

9.0

892

859

830

807

787

769

753

739

724

9.2

939

904

875

850

829

809

792

777

761

9.4

989

953

922

896

872

851

833

816

798

9.6

1041

1003

971

943

918

895

875

857

837

9.8

1094

1055

1021

991

964

940

918

898

877

10.0

1149

1108

1072

1041

1011

985

961

940

918

10.2

1203

1161

1124

1090

1059

1030

1005

982

958

10.4

1258

1214

1175

1139

1106

1075

1048

1024

998

10.6

1313

1266

1225

1188

1152

1120

1091

1065

1038

10.8

1366

1318

1275

1235

1198

1163

1132

1105

1076

11.0

1419

1368

1323

1281

1242

1206

1173

1144

1114

11.2

1471

1418

1371

1327

1285

1247

1213

1183

1151

11.4

1523

1467

1418

1372

1329

1289

1253

1221

1188

11.6

1574

1516

1465

1417

1371

1330

1293

1260

1225

11.8

1626

1566

1512

1461

1414

1371

1333

1298

1262

12.0

1678

1615

1559

1506

1458

1413

1373

1337

1300

12.2

1730

1665

1606

1552

1502

1455

1414

1376

1338

12.4

1782

1715

1654

1598

1546

1498

1455

1417

1377

12.6

1836

1766

1704

1646

1592

1543

1498

1459

1418

12.8

1890

1819

1754

1695

1639

1588

1543

1502

1459

13.0

1946

1872

1806

1745

1688

1636

1589

1547

1503

08.01.132

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

13.2

2203

1927

1859

1796

1738

1684

1636

1593

1548

13.4

2061

1983

1913

1849

1789

1734

1684

1640

1594

13.6

2121

2041

1969

1903

1842

1785

1734

1689

1641

13.8

2182

2100

2027

1959

1896

1838

1785

1739

1690

14.0

2244

2160

2085

2016

1951

1892

1838

1790

1740

14.2

2308

2223

2146

2075

2008

1947

1892

1842

1791

14.4

2374

2286

2208

2135

2067

2004

1947

1896

1843

14.6

2442

2352

2271

2197

2127

2062

2003

1951

1896

14.8

2512

2419

2337

2260

2188

2121

2061

2007

1950

15.0

2584

2488

2403

2324

2250

2182

2120

2063

2005

15.2

2657

2559

2471

2390

2314

2243

2179

2121

2061

15.4

2731

2630

2540

2456

2378

2305

2239

2179

2117

15.6

2805

2702

2609

2523

2442

2367

2299

2237

2173

15.8

2880

2774

2679

2590

2507

2430

2360

2296

2229

16.0

2955

2846

2748

2657

2572

2492

2420

2354

2286

16.2

3030

2918

2818

2724

2636

2554

2480

2412

2342

16.4

3105

2990

2887

2791

2700

2616

2539

2470

2397

16.6

3178

3061

2955

2856

2764

2677

2598

2526

2452

16.8

3251

3131

3022

2921

2826

2737

2656

2582

2505

17.0

3323

3200

3089

2985

2888

2796

2713

2637

2559

17.2

3394

3268

3155

3049

2949

2855

2770

2692

2612

17.4

3466

3337

3221

3113

3010

2914

2827

2747

2665

Original

07-14-08

08.01.133

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

17.6

3538

3406

3288

3177

3072

2974

2884

2803

2719

17.8

3610

3476

3355

3242

3135

3035

2943

2859

2773

18.0

3684

3547

3424

3308

3199

3096

3002

2917

2829

18.2

3759

3620

3494

3375

3264

3159

3063

2976

2887

18.4

3836

3694

3565

3445

3331

3224

3127

3038

2946

18.6

3916

3771

3639

3517

3401

3292

3192

3101

3008

18.8

3997

3850

3716

3591

3472

3361

3260

3167

3072

19.0

4081

3931

3795

3667

3547

3434

3330

3236

3139

19.2

4158

4014

3875

3745

3623

3508

3402

3307

3207

19.4

4256

4099

3957

3825

3700

3583

3476

3379

3278

19.6

4345

4185

4041

3906

3780

3660

3551

3452

3349

19.8

4435

4272

4126

3989

3860

3738

3628

3527

3422

20.0

4527

4360

4211

4072

3940

3817

3704

3602

3495

20.2

4618

4449

4297

4155

4021

3896

3781

3677

3568

20.4

4710

4538

4383

4238

4102

3975

3858

3752

3641

20.6

4802

4626

4469

4321

4183

4054

3935

3827

3714

20.8

4894

4715

4554

4404

4263

4131

4011

3901

3786

21.0

4985

4803

4639

4486

4343

4209

4086

3974

3858

21.2

5077

4890

4723

4568

4422

4286

4161

4047

3928

21.4

5168

4978

4808

4650

4501

4363

4236

4120

3999

21.6

5259

5065

4892

4731

4580

4439

4310

4192

4069

21.8

5350

5153

4977

4813

4659

4516

4384

4264

4139

08.01.134

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

22.0

5441

5241

5061

4894

4738

4592

4459

4337

4210

22.2

5532

5328

5146

4976

4817

4669

4533

4410

4280

22.4

5624

5417

5231

5058

4897

4746

4608

4483

4351

22.6

5716

5505

5316

5141

4977

4824

4684

4556

4423

22.8

5809

5594

5402

5224

5058

4902

4760

4631

4495

23.0

5902

5684

5489

5308

5139

4981

4837

4706

4568

23.2

5996

5774

5576

5393

5221

5061

4915

4781

4642

23.4

6091

5865

5664

5478

5304

5142

4993

4858

4717

23.6

6187

5958

5754

5565

5388

5223

5073

4936

4792

23.8

6285

6051

5844

5653

5473

5306

5153

5014

4868

24.0

6384

6146

5936

5741

5559

5389

5235

5094

4946

24.2

6485

6243

6029

5831

5646

5474

5317

5174

5024

24.4

6588

6341

6123

5923

5735

5560

5400

5256

5103

24.6

6693

6441

6220

6015

5825

5647

5485

5338

5184

24.8

6800

6543

6317

6110

5916

5735

5571

5422

5265

25.0

6909

6647

6417

6205

6008

5825

5658

5506

5347

25.2

7020

6752

6517

6302

6101

5915

5746

5592

5430

25.4

7131

6858

6618

6399

6195

6006

5834

5678

5514

25.6

7244

6965

6720

6497

6290

6097

5923

5764

5597

25.8

7357

7072

6822

6595

6385

6189

6012

5851

5682

26.0

7470

7179

6925

6693

6479

6281

6101

5937

5766

26.2

7583

7286

7026

6791

6574

6372

6189

6024

5850

Original

07-14-08

08.01.135

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

26.4

7695

7392

7128

6889

6668

6463

6278

6110

5933

26.6

7806

7498

7229

6985

6762

6554

6366

6196

6016

26.8

7915

7602

7328

7081

6854

6644

6453

6281

6099

27.0

8024

7705

7427

7177

6947

6733

6540

6365

6181

27.2

8132

7808

7526

7272

7039

6822

6626

6450

6263

27.4

8241

7911

7624

7367

7131

6911

6713

6534

6345

27.6

8349

8014

7723

7462

7223

7001

6800

6619

6427

27.8

8459

8119

7823

7558

7316

7091

6887

6704

6510

28.0

8571

8225

7924

7655

7410

7182

6976

6790

6593

28.2

8684

8332

8027

7754

7505

7274

7065

6877

6678

28.4

8801

8442

8132

7855

7602

7367

7156

6965

6763

28.6

8920

8555

8239

7957

7700

7462

7248

7055

6851

28.8

9043

8670

8349

8062

7801

7560

7342

7147

6940

29.0

9169

8789

8461

8169

7904

7658

7438

7240

7030

29.2

9298

8909

8575

8278

8008

7759

7535

7335

7122

29.4

9429

9032

8692

8389

8114

7861

7634

7431

7215

29.6

9563

9157

8810

8501

8221

7964

7733

7528

7308

29.8

9698

9284

8929

8614

8329

8068

7834

7625

7403

30.0

9835

9412

9049

8728

8438

8172

7935

7724

7498

30.2

9973

9540

9171

8843

8548

8277

8036

7822

7594

30.4

10111

9670

9292

8958

8657

8382

8138

7921

7689

30.6

10250

9799

9414

9074

8767

8488

8240

8020

7785

08.01.136

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

30.8

10389

9929

9536

9189

8877

8593

8341

8119

7881

31.0

10529

10059

9657

9304

8987

8698

8443

8217

7976

31.2

10668

10188

9779

9419

9096

8803

8544

8316

8072

31.4

10807

10318

9901

9534

9206

8908

8646

8414

8167

31.6

10946

10448

10022

9649

6315

9013

8747

8513

8262

31.8

11086

10578

10144

9764

9425

9118

8848

8611

8358

32.0

11225

10708

10266

9879

9534

9223

8950

8710

8453

32.2

11365

10838

10388

9994

9644

9328

9051

8808

8549

32.4

11504

10968

10510

10110

9754

9434

9153

8907

8644

32.6

11644

11098

10632

10225

9864

9539

9255

9006

8740

32.8

11784

11229

10755

10341

9975

9645

9357

9105

8836

33.0

11924

11359

10878

10458

10085

9751

9460

9205

8932

33.2

12066

11491

11002

10575

10197

9858

9563

9305

9029

33.4

12209

11624

11127

10693

10310

9966

9667

9406

9126

33.6

12352

11759

11253

10813

10423

10075

9772

9508

9224

33.8

12500

11895

11381

10934

10539

10185

9878

9610

9323

34.0

12650

12034

11512

11057

10655

10296

9985

9714

9423

34.2

12802

12175

11644

11182

10774

10410

10093

9819

9524

34.4

12958

12320

11780

11310

10895

10525

10204

9926

9627

34.6

13117

12468

11918

11440

11018

10642

10316

10034

9731

34.8

13281

12619

12059

11573

11144

10761

10430

10144

9836

35.0

13448

12774

12203

11708

11272

10883

10546

10256

9943

Original

07-14-08

08.01.137

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

35.2

13618

12931

12350

11846

11402

11005

10663

10368

10051

35.4

13791

13091

12498

11985

11533

11130

10782

10482

10160

35.6

13965

13252

12648

12125

11665

11255

10901

10597

10269

35.8

14141

13414

12799

12266

11798

11381

11021

10711

10379

36.0

14317

13577

12950

12408

11931

11507

11141

10826

10489

36.2

14493

13739

13101

12549

12065

11633

11261

10942

10599

36.4

14668

13901

13252

12690

12197

11758

11380

11056

10709

36.6

14842

14062

13401

12830

12329

11883

11499

11170

10818

36.8

15015

14222

13549

12969

12460

12007

11617

11284

10926

37.0

15186

14380

13696

13107

12590

12130

11734

11396

11034

37.2

15356

14537

13843

13244

12720

12253

11851

11509

11142

37.4

15526

14694

13989

13382

12849

12375

11968

11621

11249

37.6

15696

14851

14136

13519

12979

12498

12085

11734

11357

37.8

15867

15009

14283

13657

13109

12621

12203

11847

11465

38.0

16039

15169

14431

13796

13240

12754

12321

11960

11574

38.2

16213

15329

14580

13936

13372

12870

12440

12075

11683

38.4

16389

15492

14732

14077

13505

12997

12560

12190

11794

38.6

16568

15658

14885

14221

13641

13125

12682

12307

11905

38.8

16750

15826

15041

14367

13779

13255

12806

12426

12018

39.0

16935

15997

15200

14516

13918

13387

12932

12546

12133

39.2

17124

16170

15361

14666

14060

13521

13059

12667

12248

39.4

17314

16346

15524

14819

14203

13656

13187

12790

12365

08.01.138

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

39.6

17507

16524

15689

14972

14348

13792

13317

12914

12483

39.8

17701

16704

15855

15128

14493

13930

13447

13038

12601

40.0

17898

16885

16023

15284

14640

14069

13579

13164

12721

40.2

18095

17067

16191

15441

14788

14208

13711

13290

12841

40.4

18294

17250

16361

15599

14937

14348

13844

13417

12961

40.6

18493

17434

16531

15758

15086

14489

13977

13544

13082

40.8

18693

17618

16701

15917

15235

14630

14111

13672

13203

41.0

18893

17802

16872

16076

15384

14771

14245

13799

13324

41.2

19093

17987

17043

16236

15534

14912

14379

13927

13446

41.4

19294

18172

17214

16395

15684

15053

14513

14055

13567

41.6

19495

18357

17385

16555

15834

15195

14647

14183

13689

41.8

19697

18543

17557

16715

15984

15337

14782

14312

13811

42.0

19898

18729

17729

16875

16135

15478

14916

14440

13933

42.2

20100

18914

17900

17035

16285

15620

15051

14568

14055

42.4

20301

19100

18072

17195

16435

15762

15185

14697

14177

42.6

20503

19286

18244

17355

16585

15904

15320

14825

14299

42.8

20705

19472

18415

17515

16736

16046

15454

14953

14421

43.0

20906

19658

18587

17675

16886

16187

15589

15081

14542

43.2

21107

19844

18758

17834

17036

16329

15723

15209

14664

43.4

21308

20029

18930

17997

17186

16470

15857

15337

14786

43.6

21508

20214

19100

18153

17335

16612

15991

15465

14907

43.8

21707

20398

19271

18312

17485

16753

16125

15593

15029

Original

07-14-08

08.01.139

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE =-1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

126

123

120

118

115

114

111

110

108

3.2

141

137

135

133

130

129

127

125

124

3.4

156

153

150

148

146

145

143

141

140

3.6

172

169

166

165

162

161

159

158

156

3.8

189

186

183

182

179

178

176

174

173

4.0

208

204

201

199

197

195

193

192

190

4.2

228

223

221

218

215

213

211

209

208

4.4

249

244

241

239

235

233

230

228

226

4.6

273

267

264

260

256

253

250

248

245

4.8

299

292

288

283

279

275

271

268

265

5.0

326

319

313

308

302

297

293

289

285

5.2

355

346

340

333

326

321

315

311

306

5.4

385

375

367

359

351

345

338

333

327

5.6

416

404

395

386

377

369

361

355

348

5.8

447

434

423

413

402

393

385

378

370

6.0

477

463

451

439

428

418

408

400

392

6.2

508

492

479

466

453

442

432

423

414

6.4

537

520

505

491

478

466

455

445

435

6.6

566

547

531

516

501

489

477

467

456

6.8

592

572

555

539

524

511

499

488

477

7.0

618

596

578

562

546

533

520

509

498

08.01.140

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE =-1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

644

620

601

584

568

555

542

530

519

7.4

669

645

624

606

591

577

564

552

540

7.6

696

669

647

630

614

600

586

575

563

7.8

723

696

672

654

638

624

610

598

586

8.0

753

724

699

681

664

649

635

623

611

8.2

765

754

729

710

692

677

663

650

637

8.4

820

788

761

741

723

707

692

679

666

8.6

858

825

797

776

757

740

724

711

696

8.8

901

866

837

815

795

777

760

745

730

9.0

947

911

881

857

835

816

797

782

765

9.2

997

959

927

902

878

857

838

820

803

9.4

1049

1010

976

949

923

901

879

861

842

9.6

1103

1062

1027

998

970

946

923

903

882

9.8

1159

1116

1080

1048

1018

991

967

945

923

10.0

1216

1171

1133

1099

1067

1038

1011

988

964

10.2

1273

1227

1186

1150

1116

1085

1056

1031

1005

10.4

1330

1282

1239

1201

1164

1131

1101

1074

1046

10.6

1387

1337

1292

1251

1212

1177

1145

1116

1087

10.8

1443

1390

1343

1300

1259

1221

1187

1157

1126

11.0

1497

1442

1393

1347

1304

1265

1229

1197

1165

11.2

1552

1494

1443

1394

1349

1308

1270

1237

1203

11.4

1605

1546

1491

1441

1394

1351

1311

1276

1241

Original

07-14-08

08.01.141

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE =-1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.6

1659

1597

1540

1487

1438

1393

1352

1316

1279

11.8

1712

1648

1588

1534

1482

1436

1393

1355

1317

12.0

1766

1699

1637

1580

1527

1479

1435

1395

1355

12.2

1820

1750

1686

1628

1573

1523

1477

1436

1395

12.4

1875

1803

1736

1676

1619

1568

1520

1478

1435

12.6

1931

1856

1788

1725

1667

1614

1565

1521

1477

12.8

1988

1911

1840

1776

1716

1661

1611

1566

1521

13.0

2046

1966

1894

1828

1766

1710

1658

1612

1566

13.2

2105

2024

1949

1881

1818

1760

1707

1660

1612

13.4

2166

2082

2006

1936

1871

1812

1758

1709

1660

13.6

2228

2142

2064

1993

1926

1866

1809

1760

1709

13.8

2291

2203

2124

2051

1982

1920

1863

1812

1760

14.0

2357

2267

2185

2110

2040

1976

1917

1865

1811

14.2

2424

2331

2248

2171

2099

2034

1973

1919

1864

14.4

2492

2398

2312

2233

2160

2092

2030

1974

1918

14.6

2563

2466

2378

2297

2222

2152

2088

2031

1973

14.8

2636

2536

2446

2363

2285

2213

2148

2089

2028

15.0

2710

2607

2515

2429

2349

2276

2208

2147

2085

15.2

2786

2680

2585

2497

2415

2339

2269

2206

2142

15.4

2862

2754

2656

2566

2481

2403

330

2265

2199

15.6

2940

2828

2728

2634

2547

2467

2392

2325

2257

15.8

3017

2903

2799

2704

2614

2531

2454

2385

2315

08.01.142

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE =-1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.0

3095

2978

2871

2773

2680

2595

2516

2445

2372

16.2

3173

3052

2943

2842

2747

2659

2577

2504

2429

16.4

3250

3126

3014

2910

2812

2722

2638

2563

2486

16.6

3326

3199

3084

2977

2877

2784

2698

2621

2542

16.8

3401

3271

3153

3044

2941

2846

2758

2678

2597

17.0

3475

3343

3222

3110

3005

2907

2816

2735

2652

17.2

3549

3414

3290

3175

3068

2968

2875

2791

2706

17.4

3623

3484

3358

3241

3131

3028

2933

2848

2761

17.6

3697

3556

3427

3307

3194

3090

2992

2905

2816

17.8

3773

3628

3496

3374

3259

3152

3052

2963

2873

18.0

3849

3701

3567

3442

3325

3215

3114

3022

2930

18.2

3927

3776

3639

3512

3392

3280

3177

3083

2989

18.4

4007

3853

3713

3583

3461

3347

3241

3146

3050

18.6

4089

3932

3790

3657

3533

3417

3309

3212

3114

18.8

4174

4014

3869

3734

3607

3489

3379

3280

3180

19.0

4262

4099

3951

3813

3684

3563

3451

3350

3249

19.2

4351

4185

4034

3894

3762

3640

3526

3423

3319

19.4

4443

4273

4120

3977

3843

3718

3602

3497

3391

19.6

4536

4363

4206

4061

3925

3797

3679

3573

3465

19.8

4630

4454

4294

4146

4007

3878

3758

3649

3539

20.0

4725

4545

4383

4232

4091

3959

3837

3726

3614

20.2

4821

4637

4472

4318

4174

4040

3916

3804

3689

Original

07-14-08

08.01.143

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE =-1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

20.4

4916

4730

4561

4404

4258

4122

3995

3881

3764

20.6

5012

4822

4649

4490

4341

4203

4074

3958

3839

20.8

5107

4913

4738

4576

4424

4283

4152

4033

3912

21.0

5202

5004

4825

4660

4506

4362

4229

4109

3985

21.2

5296

5095

4913

4745

4588

4441

4306

4183

4058

21.4

5391

5186

5000

4829

4669

4520

4382

4257

4130

21.6

5485

5276

5087

4913

4750

4599

4459

4331

4202

21.8

5579

5367

5174

4997

4831

4677

4535

4405

4274

22.0

5674

5458

5261

5081

4912

4756

4611

4480

4345

22.2

5769

5548

5349

5165

4994

4835

4687

4554

4418

22.4

5864

5640

5436

5250

5076

4914

4764

4629

4490

22.6

5959

5731

5525

5335

5158

4994

4842

4704

4564

22.8

6056

5824

5614

5421

5241

5075

4920

4781

4638

23.0

6153

5917

5703

5508

5325

5156

4999

4858

4713

23.2

6250

6010

5794

5595

5410

5239

5079

4936

4789

23.4

6349

6105

5885

5684

5496

5322

5160

5015

4865

23.6

6450

6201

5978

5773

5583

5406

5242

5094

4943

23.8

6552

6299

6072

5864

5670

5491

5325

5175

5021

24.0

6655

6397

6167

5956

5759

5577

5409

5257

5101

24.2

6760

6498

6263

6049

5849

5664

5494

5339

5181

24.4

6868

6600

6361

6143

5941

5753

5580

5423

5263

24.6

6978

6704

6461

6239

6033

5843

5667

5508

5345

08.01.144

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE =-1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

24.8

7089

6811

6563

6337

6127

5934

5755

5594

5428

25.0

7203

6919

6665

6435

6222

6026

5844

5681

5513

25.2

7319

7028

6769

6535

6319

6119

5934

5768

5598

25.4

7436

7138

6874

6635

6415

6212

6025

5856

5683

25.6

7553

7249

6980

6736

6513

6306

6116

5945

5769

25.8

7671

7361

7085

6837

6610

6400

6207

6033

5855

26.0

7789

7472

7191

6939

6708

6494

6298

6122

5941

26.2

7907

7583

7296

7039

6805

6588

6389

6210

6026

26.4

8024

7693

7401

7140

6901

6682

6479

6298

6112

26.6

8139

7803

7505

7239

6997

6774

6569

6386

6196

26.8

8253

7910

7607

7338

7093

6866

6659

6472

6281

27.0

8366

8017

7709

7436

7187

6958

6747

6559

6364

27.2

8479

8124

7811

7533

7281

7049

6836

6644

6448

27.4

8592

8230

7913

7631

7376

7140

6924

6731

6531

27.6

8705

8338

8015

7729

7470

7231

7013

6817

6615

27.8

8820

8446

8118

7828

7566

7324

7102

6904

6699

28.0

8936

8556

8222

7928

7662

7417

7193

6992

6785

28.2

9055

8667

8329

8030

7760

7511

7284

7081

6871

28.4

9176

8782

8437

8133

7860

7607

7377

7171

6959

28.6

9301

8899

8549

8240

7962

7705

7472

7263

7048

28.8

9430

9020

8663

8348

8066

7806

7569

7357

7139

29.0

9562

9144

8780

8460

8172

7908

7667

7453

7232

Original

07-14-08

08.01.145

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE =-1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

29.2

9698

9271

8899

8573

8280

8012

7768

7551

7326

29.4

9837

9400

9021

8688

8390

8117

7869

7649

7422

29.6

9977

9531

9144

8805

8501

8224

7972

7749

7518

29.8

10120

9664

9269

8923

8614

8331

8076

7850

7615

30.0

10264

9799

9395

9042

8727

8439

8180

7951

7713

30.2

10410

9934

9522

9162

8840

8548

8284

8052

7811

30.4

10556

10070

9649

9282

8954

8657

8389

8154

7909

30.6

10702

10206

9776

9401

9068

8766

8494

8255

8008

30.8

10848

10341

9903

9521

9182

8874

8598

8357

8105

31.0

10995

10477

10029

9640

9295

8983

8702

8458

8203

31.2

11141

10613

10156

9759

9408

9091

8806

8558

8301

31.4

11287

10748

10282

9878

9521

9199

8910

8659

8398

31.6

11433

10884

10409

9997

9634

9307

9014

8760

8495

31.8

11579

11020

10535

10117

9747

9415

9118

8860

8592

32.0

11725

11155

10662

10236

9850

9523

9222

8961

8690

32.2

11872

11291

10789

10355

9974

9631

9326

9062

8787

32.4

12019

11427

10916

10475

10087

9740

9430

9163

8885

32.6

12166

11564

11043

10595

10201

9848

9535

9264

8983

32.8

12313

11700

11171

10715

10315

9958

9640

9366

9081

33.0

12461

11838

11300

10837

10430

10068

9746

9468

9180

33.2

12610

11976

11429

10959

10546

10178

9852

9571

9279

33.4

12761

12116

11560

11082

10663

10290

9959

9675

9379

08.01.146

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE =-1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

33.6

12914

12257

11693

11207

10781

10402

10067

9779

9479

33.8

13069

12401

11827

11333

10901

10516

10176

9885

9581

34.0

13227

12547

11963

11461

11022

10632

10287

9992

9684

34.2

13387

12696

12102

11592

11146

10749

10399

10100

9787

34.4

13552

12848

12244

11725

11271

10868

10513

10209

9893

34.6

13721

13003

12388

11860

11399

10989

10629

10321

9999

34.8

13893

13163

12536

11998

11529

11113

10746

10433

10107

35.0

14070

13325

12686

12139

11662

11238

10865

10548

10217

35.2

14249

13490

12839

12282

11796

11365

10986

10663

10327

35.4

14431

13658

12994

12426

11932

11493

11108

10781

10438

35.6

14615

13827

13150

12572

12069

11622

11230

10897

10550

35.8

14800

13997

13307

12718

12207

11752

11353

11015

10662

36.0

14985

14167

13464

12865

12344

11882

11476

11133

10775

36.2

15172

14338

13622

13011

12482

12012

11600

11250

10887

36.4

15357

14508

13779

13158

12619

12141

11722

11368

10999

36.6

15540

14677

13934

13303

12756

12270

11844

11485

11111

36.8

15722

14844

14089

13447

12891

12398

11966

11601

11221

37.0

15903

15010

14242

13590

13026

12524

12086

11716

11332

37.2

16082

15175

14394

13732

13160

12651

12206

11831

11442

37.4

16262

15339

14547

13874

13294

12777

12326

11946

11552

37.6

16441

15504

14699

14017

13428

12904

12447

12061

11662

37.8

16621

15670

14852

14160

13562

13031

12567

12177

11772

Original

07-14-08

1.50

2.00

08.01.147

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE =-1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

38.0

16803

15837

15007

14304

13698

13159

12689

12293

11883

38.2

16986

16006

15163

14449

13834

13288

12811

12410

11995

38.4

17172

16176

15320

14596

13973

13418

12935

12529

12108

38.6

17360

16350

15480

14745

14113

13550

13060

12649

12222

38.8

17552

16526

15643

14897

14255

13685

13188

12770

12338

39.0

17747

16706

15809

15051

14400

13821

13317

12893

12455

39.2

17945

16887

15976

15207

14546

13959

13447

13018

12574

39.4

18145

17072

16146

15365

14694

14098

13579

13144

12693

39.6

18347

17258

16318

15525

14844

14239

13713

13271

12814

39.8

18551

17446

16491

15686

14995

14381

13847

13398

12935

40.0

18757

17635

16665

15848

15146

14524

13982

13527

13057

40.2

18964

17825

16841

16011

15299

14667

14118

13656

13180

40.4

19172

18016

17017

16175

15452

14811

14254

13786

13303

40.6

19381

18208

17193

16339

15606

14956

14391

13916

13426

40.8

19590

18400

17370

16503

15760

15100

14527

14046

13549

41.0

19799

18592

17547

16667

15913

15245

14664

14176

13673

41.2

20009

18785

17724

16832

16067

15390

14801

14307

13797

41.4

20218

18978

17902

16997

16222

15535

14938

14437

13920

41.6

20428

19170

18079

17161

16376

15680

15075

14568

14044

41.8

20638

19363

18257

17326

16530

15825

15212

14698

14168

42.0

20849

19556

18434

17491

16684

15970

15350

14829

14292

42.2

21059

19750

18612

17656

16839

16115

15487

14959

14416

08.01.148

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE =-1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

42.4

21269

19943

18789

17821

16993

16260

15624

15090

14540

42.6

21479

20136

18967

17986

17147

16405

15761

15221

14663

42.8

21690

20329

19145

18150

17301

16550

15899

15351

14787

43.0

21900

20522

19322

18315

17456

16695

16036

15482

14911

43.2

22109

20715

19499

18480

17610

16840

16173

15612

15035

43.4

22318

20908

19676

18644

17764

16985

16310

15742

15159

43.6

22527

21100

19853

18808

17918

17130

16447

15873

15282

43.8

22734

21292

20030

18972

18071

17275

13584

16003

15406

FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

144

140

137

134

132

129

126

123

122

3.2

161

156

154

151

148

146

143

141

139

3.4

178

173

171

168

166

163

161

158

157

3.6

196

191

188

186

183

181

179

176

175

3.8

214

209

207

204

202

199

197

194

193

4.0

235

229

227

224

221

218

216

213

211

Original

07-14-08

08.01.149

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

4.2

256

250

247

244

241

238

235

232

230

4.4

280

273

269

266

262

258

255

252

250

4.6

305

297

293

288

284

280

276

272

270

4.8

332

323

318

312

307

302

298

294

290

5.0

361

351

344

338

331

325

320

315

311

5.2

391

380

372

364

356

349

343

337

332

5.4

422

410

400

391

382

374

367

360

354

5.6

454

440

429

418

408

399

390

383

376

5.8

486

470

458

446

434

424

415

406

398

6.0

518

501

487

473

461

449

439

429

420

6.2

549

531

515

501

487

474

463

453

443

6.4

580

560

543

527

512

499

487

476

465

6.6

609

588

570

553

537

523

510

498

487

6.8

637

615

595

578

562

547

533

521

509

7.0

664

641

620

602

585

570

556

544

532

7.2

691

666

645

626

609

594

579

566

554

7.4

718

692

670

651

634

618

603

590

577

7.6

746

718

696

676

659

643

628

614

601

7.8

775

746

723

703

685

669

653

639

626

8.0

806

776

752

732

713

696

681

666

653

8.2

839

809

784

763

744

726

710

695

681

8.4

876

844

818

796

776

758

741

726

711

08.01.150

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

8.6

917

884

857

833

812

793

775

759

744

8.8

962

927

898

874

851

831

812

795

778

9.0

1011

974

944

917

893

871

851

833

815

9.2

1063

1024

992

964

938

914

892

873

854

9.4

1118

1077

1043

1012

985

959

935

914

894

9.6

1175

1132

1095

1063

1033

1005

980

957

935

9.8

1234

1188

1149

1114

1082

1052

1025

1000

977

10.0

1294

1245

1204

1166

1132

1100

1071

1044

1019

10.2

1354

1303

1259

1219

1182

1147

1116

1088

1061

10.4

1413

1360

1314

1271

1231

1195

1162

1132

1103

10.6

1472

1417

1367

1322

1280

1241

1206

1174

1144

10.8

1530

1472

1420

1372

1328

1287

1250

1216

1184

11.0

1587

1526

1472

1421

1374

1332

1293

1257

1223

11.2

1643

1580

1522

1469

1421

1376

1335

1298

1262

11.4

1699

1632

1572

1517

1466

1419

1377

1338

1301

11.6

1754

1685

1623

1565

1512

1463

1419

1378

1339

11.8

1809

1738

1673

1613

1558

1507

1461

1419

1378

12.0

1865

1791

1723

1661

1604

1552

1504

1460

1418

12.2

1921

1844

1774

1710

1651

1597

1548

1503

1459

12.4

1978

1899

1826

1760

1699

1643

1593

1546

1501

12.6

2036

1954

1880

1811

1749

1691

1639

1591

1545

12.8

2095

2011

1935

1864

1800

1741

1687

1637

1590

Original

07-14-08

08.01.151

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

13.0

2156

2070

1991

1919

1853

1792

1737

1686

1637

13.2

2218

2130

2019

1975

1907

1845

1788

1736

1685

13.4

2282

2191

2108

2033

1963

1899

1841

1787

1735

13.6

2347

2254

2169

2092

2020

1955

1895

1840

1787

13.8

2414

2318

2232

2152

2079

2012

1950

1894

1839

14.0

2483

2385

2296

2215

2139

2070

2007

1949

1893

14.2

2553

2452

2362

2278

2201

2130

2065

2006

1948

14.4

2625

2522

2429

2343

2264

2191

2124

2063

2004

14.6

2699

2593

2497

2410

2328

2253

2184

2121

2060

14.8

2775

2666

2568

2477

2393

2316

2245

2181

2118

15.0

2852

2740

2639

2546

2460

2380

2307

2241

2175

15.2

2931

2816

2712

2616

2527

2445

2370

2301

2234

15.4

3010

2892

2785

2686

2595

2510

2433

2362

2292

15.6

3090

2969

2858

2757

2663

2576

2496

2423

2351

15.8

3170

3046

2932

2828

2731

2642

2559

2484

2410

16.0

3251

3123

3006

2899

2799

2707

2622

2545

2468

16.2

3330

3199

3080

2969

2867

2772

2685

2605

2527

16.4

3410

3275

3152

3039

2934

2837

2748

2666

2585

16.6

3488

3350

3224

3108

3001

2901

2809

2725

2642

16.8

3565

3424

3295

3177

3067

2965

2870

2784

2699

17.0

3641

3497

3366

3244

3132

3027

2931

2843

2756

17.2

3717

3570

3435

3312

3197

3090

2991

2901

2812

08.01.152

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

17.4

3793

3643

3505

3379

3262

3153

3052

2960

2869

17.6

3869

3716

3576

3447

3328

3216

3113

3019

2927

17.8

3946

3790

3647

3516

3394

3281

3176

3079

2985

18.0

4025

3866

3720

3586

3462

3346

3239

3141

3045

18.2

4106

3943

3785

3659

3532

3414

3304

3204

3106

18.4

4188

4023

3872

3733

3604

3483

3372

3269

3170

18.6

4274

4105

3951

3809

3678

3555

3441

3337

3235

18.8

4363

4190

4033

3889

3755

3629

3514

3407

3304

19.0

4455

4278

4118

3971

3834

3706

3588

3480

3374

19.2

4549

4369

4205

4055

3915

3785

3665

3554

3446

19.4

4645

4461

4294

4141

3999

3866

3743

3630

3520

19.6

4743

4555

4385

4228

4083

3948

3823

3708

3595

19.8

4841

4650

4476

4317

4169

4031

3903

3786

3671

20.0

4941

4746

4569

4406

4255

4114

3984

3865

3748

20.2

5041

4842

4661

4495

4341

4198

4066

3944

3824

20.4

5142

4938

4754

4584

4427

4282

4147

4023

3901

20.6

5241

5034

4846

4673

4513

4365

4228

4101

3977

20.8

5340

5129

4937

4761

4598

4447

4307

4179

4052

21.0

5439

5224

5028

4848

4683

4529

4386

4255

4126

21.2

5537

5318

5118

4935

4766

4610

4465

4332

4200

21.4

5634

5411

5208

5021

4850

4690

4543

4407

4274

21.6

5732

5505

5297

5108

4933

4771

4621

4483

4347

Original

07-14-08

08.01.153

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

21.8

5829

5598

5387

5194

5016

4851

4699

4559

4421

22.0

5927

5692

5477

5280

5100

4932

4778

4635

4494

22.2

6025

5785

5567

5367

5184

5013

4856

4711

4568

22.4

6124

5880

5657

5455

5268

5095

4935

4788

4643

22.6

6223

5975

5749

5543

5353

5177

5015

4866

4718

22.8

6323

6071

5841

5632

5439

5261

5096

4944

4795

23.0

6425

6168

5934

5721

5526

5345

5178

5024

4872

23.2

6527

6266

6028

5812

5614

5430

5260

5104

4950

23.4

6631

6365

6124

5904

5703

5516

5344

5185

5029

23.6

6737

6465

6220

5997

5793

5603

5429

5268

5109

23.8

6844

6567

6318

6092

5884

5691

5514

5351

5190

24.0

6953

6671

6417

6187

5976

5781

5601

5436

5272

24.2

7063

6776

6518

6284

6069

5871

5689

5521

5355

24.4

7176

6883

6620

6382

6164

5963

5777

5607

5439

24.6

7291

6992

6723

6481

6260

6055

5867

5695

5524

24.8

7409

7103

6829

6582

6357

6149

5958

5783

5610

25.0

7528

7215

6936

6684

6455

6244

6050

5872

5696

25.2

7649

7329

7044

6787

6554

6340

6143

5962

5783

25.4

7771

7444

7152

6891

6654

6436

6236

6052

5871

25.6

7894

7560

7251

6995

6754

6532

6329

6143

5958

25.8

8017

7675

7371

7099

6854

6629

6422

6233

6046

26.0

8140

7791

7480

7203

6954

6725

6516

6324

6134

08.01.154

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

26.2

8262

7906

7588

7307

7054

6821

6608

6414

6221

26.4

8383

8020

7696

7410

7153

6917

6701

6504

6308

26.6

8503

8133

7803

7512

7251

7011

6793

6593

6395

26.8

8622

8244

7908

7613

7348

7105

6883

6681

6480

27.0

8739

8354

8013

7713

7445

7198

6974

6769

6566

27.2

8855

8464

8117

7813

7541

7291

7064

6856

6650

27.4

8972

8574

8222

7913

7637

7384

7154

6944

6736

27.6

9089

8685

8327

8013

7734

7478

7244

7032

6821

27.8

9209

8797

8433

8115

7832

7572

7336

7120

6907

28.0

9330

8910

8541

8218

7931

7668

7428

7210

6994

28.2

9454

9027

8651

8323

8031

7765

7522

7301

7083

28.4

9581

9146

8764

8430

8134

7864

7618

7394

7172

28.6

9713

9269

8880

8541

8239

7965

7715

7489

7264

28.8

9849

9396

8999

8654

8348

8068

7815

7586

7358

29.0

9990

9527

9122

8770

8458

8175

7917

7685

7454

29.2

10134

9661

9248

8889

8571

8283

8021

7785

7551

29.4

10281

9798

9376

9009

8686

8392

8127

7887

7650

29.6

10431

9937

9506

9132

8802

8503

8234

7991

7749

29.8

10583

10078

9637

9256

8920

8615

8341

8095

7850

30.0

10737

10220

9770

9380

9038

8728

8450

8199

7951

30.2

10892

10363

9903

9505

9156

8841

8558

8304

8052

30.4

11047

10507

10036

9631

9275

8954

8667

8409

8153

Original

07-14-08

08.01.155

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

30.6

11201

10650

10169

9755

9393

9067

8775

8514

8254

30.8

11356

10792

10302

9880

9511

9179

8883

8618

8354

31.0

11509

10935

10434

10004

9628

9291

8990

8721

8454

31.2

11663

11076

10565

10127

9745

9402

9097

8825

8554

31.4

11816

11218

10697

10250

9861

9513

9203

8928

8654

31.6

11969

11359

10828

10373

9978

9624

9310

9030

8753

31.8

12122

11501

10959

10496

10094

9735

9416

9133

8852

32.0

12275

11642

11091

10619

10211

9846

9523

9236

8952

32.2

12429

11784

11222

10743

10328

9958

9630

9339

9051

32.4

12583

11927

11355

10867

10445

10070

9737

9443

9151

32.6

12738

12070

11488

10992

10563

10182

9845

9547

9252

32.8

12894

12214

11622

11117

10682

10295

9953

9652

9352

33.0

13052

12359

11757

11244

10802

10409

10063

9757

9454

33.2

13210

12505

11893

11372

10923

10524

10173

9863

9556

33.4

13371

12653

12030

11501

11045

10640

10284

9970

9659

33.6

13534

12803

12170

11632

11168

10758

10396

10078

9763

33.8

13699

12956

12311

11764

11293

10876

10510

10188

9868

34.0

13868

13110

12455

11899

11420

10997

10624

10298

9974

34.2

14039

13268

12601

12035

11549

11118

10741

10410

10081

34.4

14214

13429

12750

12174

11680

11242

10859

10523

10189

34.6

14393

13593

12901

12316

11813

11368

10978

10637

10299

34.8

14576

13761

13056

12460

11948

11496

11100

10754

10410

08.01.156

0.00

07-14-08

.50

1.00

1.50

2.00

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

35.0

14763

13932

13214

12606

12085

11625

11223

10871

10522

35.2

14953

14106

13373

12754

12225

11756

11347

10990

10635

35.4

15145

14282

13535

12904

12365

11889

11472

11109

10749

35.6

15339

14459

13697

13055

12506

12022

11598

11229

10864

35.8

15534

14637

13861

13207

12648

12155

11725

11350

10978

36.0

15730

14816

14024

13358

12790

12289

11851

11470

11093

36.2

15925

14994

14188

13510

12932

12422

11977

11591

11208

36.4

16120

15172

14351

13661

13074

12556

12103

11711

11322

36.6

16313

15349

14513

13811

13214

12688

12229

11830

11436

36.8

16505

15524

14673

13960

13354

12819

12353

11949

11549

37.0

16695

15698

14832

14108

13492

12950

12477

12067

11662

37.2

16884

15871

14991

14255

13630

13080

12600

12185

11774

37.4

17073

16044

15150

14402

13768

13210

12723

12302

11886

37.6

17263

16217

15308

14550

13907

13340

12847

12420

11999

37.8

17453

16390

15468

14698

14046

13471

12971

12539

12112

38.0

17644

16566

15629

14847

14186

13603

13096

12658

12225

38.2

17838

16743

15791

14998

14327

13736

13222

12778

12340

38.4

18034

16922

15956

15151

14470

13870

13349

12899

12455

38.6

18232

17104

16123

15306

14615

14007

13478

13022

12573

38.8

18435

17289

16293

15464

14763

14146

13610

13147

12691

39.0

18640

17478

16467

15624

14913

14287

13743

13274

12812

39.2

18849

17669

16642

15787

15065

14429

13878

13402

12933

Original

07-14-08

08.01.157

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

39.4

19059

17863

16820

15951

15218

14574

14014

13532

13056

39.6

19272

18058

16999

16117

15373

14719

14151

13662

13180

39.8

19487

18255

17180

16285

15530

14866

14290

13794

13304

40.0

19703

18454

17362

16454

15687

15014

14429

13926

13430

40.2

19921

18653

17546

16623

15845

15162

14569

14059

13555

40.4

20139

18853

17729

16793

16003

15310

14709

14192

13681

40.6

20358

19054

17913

16963

16162

15459

14850

14325

13808

40.8

20576

19254

18097

17133

16321

15608

14990

14458

13934

41.0

20795

19455

18281

17303

16479

15756

15130

14591

14060

41.2

21014

19655

18465

17473

16637

15905

15270

14724

14186

41.4

21232

19856

18649

17643

16796

16053

15410

14857

14312

41.6

21451

20056

18833

17813

16954

16202

15550

14990

14438

41.8

21670

20257

19017

17983

17112

16350

15690

15123

14564

42.0

21888

20457

19200

18153

17271

16499

15831

15256

14690

42.2

22107

20658

19384

18323

17429

16647

15971

15389

14815

42.4

22325

20858

19568

18492

17587

16795

16111

15522

14941

42.6

22543

21058

19752

18662

17746

16944

16251

15655

15067

42.8

22761

21259

19935

18832

17904

17092

16391

15787

15193

43.0

22979

21459

20119

19001

18062

17241

16531

15920

15319

43.2

23196

21659

20302

19171

18220

17389

16671

16053

15445

43.4

23413

21859

20485

19341

18379

17538

16811

16186

15571

43.6

23629

22058

20668

19510

18537

17686

16951

16319

15697

08.01.158

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

43.8

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

23844

22256

20851

19679

18695

17835

17091

16452

15823

FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

165

160

157

152

150

146

144

140

139

3.2

184

179

176

172

169

166

163

160

158

3.4

204

199

196

192

189

185

183

180

178

3.6

225

219

216

212

209

205

203

200

198

3.8

246

240

237

233

229

226

223

220

218

4.0

268

262

259

254

250

247

244

240

238

4.2

292

285

281

276

272

268

265

261

258

4.4

317

310

305

300

295

290

286

282

279

4.6

344

335

330

324

318

313

308

303

300

4.8

373

363

356

349

342

336

330

325

321

5.0

403

392

383

375

367

360

353

347

342

5.2

434

421

411

402

393

384

377

370

364

5.4

466

452

440

429

419

409

401

393

386

Original

07-14-08

08.01.159

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

5.6

499

483

469

457

445

435

425

416

408

5.8

532

514

499

485

472

460

449

439

430

6.0

565

545

529

513

499

486

474

463

453

6.2

597

576

558

541

525

511

498

487

476

6.4

629

606

587

569

552

537

523

511

499

6.6

659

636

615

596

578

562

548

535

522

6.8

689

664

642

623

604

588

572

559

546

7.0

717

692

669

649

630

613

597

583

570

7.2

746

719

697

676

656

639

623

608

594

7.4

774

747

724

703

683

665

649

633

619

7.6

804

776

753

731

711

692

676

660

646

7.8

835

807

783

760

740

721

704

688

673

8.0

869

839

815

792

771

751

734

717

702

8.2

905

874

849

825

804

783

765

748

733

8.4

944

912

887

862

839

818

799

781

765

8.6

988

954

927

901

877

855

835

816

799

8.8

1036

1000

971

943

918

895

873

854

835

9.0

1087

1049

1019

989

962

937

914

893

874

9.2

1142

1102

1069

1037

1008

981

957

934

913

9.4

1200

1157

1121

1087

1056

1027

1001

977

954

9.6

1259

1214

1175

1139

1105

1074

1046

1021

996

9.8

1321

1272

1230

1191

1155

1122

1092

1065

1039

08.01.160

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

10.0

1383

1331

1286

1244

1206

1171

1138

1109

1081

10.2

1445

1390

1342

1297

1256

1219

1185

1154

1124

10.4

1507

1449

1398

1350

1307

1267

1230

1197

1166

10.6

1568

1507

1452

1402

1356

1314

1275

1240

1207

10.8

1627

1563

1506

1453

1404

1360

1319

1282

1247

11.0

1685

1619

1558

1502

1452

1405

1362

1324

1287

11.2

1743

1673

1609

1551

1498

1449

1405

1364

1326

11.4

1800

1727

1661

1600

1544

1493

1447

1405

1365

11.6

1856

1781

1712

1648

1591

1538

1490

1445

1404

11.8

1913

1835

1763

1697

1638

1582

1533

1486

1444

12.0

1970

1889

1815

1746

1685

1628

1576

1528

1484

12.2

2028

1944

1868

1797

1734

1674

1621

1572

1526

12.4

2087

2001

1922

1849

1784

1723

1668

1616

1570

12.6

2147

2059

1977

1902

1835

1772

1716

1663

1615

12.8

2210

2119

2035

1958

1889

1824

1766

1712

1662

13.0

2274

2180

2095

2016

1945

1878

1819

1763

1712

13.2

2340

2244

2156

2075

2002

1934

1873

1816

1763

13.4

2407

2309

2219

2136

2061

1992

1929

1870

1816

13.6

2477

2376

2284

2199

2122

2051

1986

1926

1871

13.8

2548

2444

2350

2263

2184

2111

2045

1984

1926

14.0

2620

2514

2418

2329

2248

2173

2105

2042

1983

14.2

2695

2586

2487

2396

2313

2236

2166

2102

2041

Original

07-14-08

08.01.161

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

14.4

2771

2659

2557

2462

2379

2300

2228

2162

2099

14.6

2848

2734

2629

2533

2446

2365

2291

2223

2158

14.8

2927

2809

2702

2604

2514

2430

2354

2284

2217

15.0

3008

2887

2776

2675

2582

2496

2417

2345

2276

15.2

3089

2965

2851

2746

2651

2563

2481

2407

2335

15.4

3171

3043

2926

2819

2720

2629

2545

2469

2395

15.6

3254

3122

3002

2891

2790

2696

2610

2531

2454

15.8

3336

3201

3077

2964

2859

2763

2674

2593

2514

16.0

3419

3280

3153

3036

2929

2830

2738

2655

2573

16.2

3501

3359

3228

3108

2998

2896

2802

2716

2633

16.4

3582

3437

3302

3180

3067

2962

2866

2778

2692

16.6

3662

3514

3376

3250

3135

3028

2929

2839

2751

16.8

3742

3589

3449

3321

3203

3093

2992

2900

2810

17.0

3820

3665

3521

3390

3270

3158

3055

2960

2869

17.2

3898

3739

3593

3460

3337

3223

3118

3021

2928

17.4

3976

3815

3666

3530

3405

3289

3181

3083

2987

17.6

4055

3890

3739

3600

3473

3355

3246

3145

3048

17.8

4135

3967

3813

3672

3543

3422

3311

3208

3109

18.0

4217

4045

3888

3745

3613

3491

3377

3272

3172

18.2

4301

4126

3966

3820

3686

3561

3445

3339

3236

18.4

4387

4209

4046

3897

3761

3633

3515

3407

3302

18.6

4477

4295

4128

3977

3838

3708

3588

3477

3370

08.01.162

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

18.8

4570

4384

4214

4060

3917

3785

3663

3549

3441

19.0

4666

4476

4303

4145

4000

3865

3740

3624

3513

19.2

4764

4570

4393

4232

4084

3946

3818

3701

3587

19.4

4865

4667

4486

4321

4170

4029

3899

3779

3663

19.6

4968

4765

4580

4412

4257

4113

3980

3858

3739

19.8

5072

4865

4675

4503

4345

4199

4063

3938

3817

20.0

5176

4955

4771

4595

4434

4284

4146

4018

3895

20.2

5281

5065

4867

4687

4523

4370

4228

4098

3972

20.4

5385

5165

4963

4779

4611

4455

4311

4178

4050

20.6

5489

5264

5058

4870

4699

4540

4393

4258

4127

20.8

5592

5362

5152

4961

4786

4624

4474

4337

4203

21.0

5693

5460

5245

5050

4873

4708

4555

4415

4279

21.2

5794

5556

5337

5139

4958

4790

4635

4492

4354

21.4

5895

5653

5430

5227

5044

4873

4715

4569

4428

21.6

5995

5749

5522

5316

5129

4955

4794

4646

4503

21.8

6096

5845

5614

5404

5214

5037

4874

4723

4578

22.0

6197

5941

5706

5493

5300

5120

4954

4801

4653

22.2

6299

6038

5799

5582

5386

5203

5035

4879

4729

22.4

6401

6136

5893

5672

5473

5287

5116

4958

4806

22.6

6505

6235

5987

5764

5561

5372

5199

5038

4884

22.8

6610

6335

6083

5856

5650

5459

5282

5119

4963

23.0

6717

6436

6180

5950

5741

5546

5367

5202

5043

Original

07-14-08

08.01.163

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

23.2

6825

6539

6279

6044

5832

5635

5453

5285

5124

23.4

6935

6644

6379

6140

5925

5725

5540

5370

5206

23.6

7046

6749

6480

6238

6019

5815

5628

5456

5289

23.8

7159

6857

6583

6336

6114

5907

5717

5543

5373

24.0

7275

6966

6687

6436

6210

6000

5808

5630

5459

24.2

7392

7077

6792

6537

6307

6095

5899

5719

5545

24.4

7511

7189

6899

6640

6406

6190

5991

5808

5631

24.6

7632

7303

7008

6743

6505

6286

6084

5899

5719

24.8

7756

7420

7117

6848

6606

6383

6178

5990

5807

25.0

7881

7537

7228

6954

6708

6481

6272

6081

5896

25.2

8008

7656

7340

7060

6810

6579

6367

6174

5985

25.4

8135

7776

7452

7167

6912

6678

6463

6266

6075

25.6

8263

7896

7565

7274

7015

6777

6558

6359

6164

25.8

8391

8015

7678

7381

7118

6876

6654

6451

6254

26.0

8519

8135

7790

7488

7220

6974

6749

6544

6343

26.2

8646

8254

7902

7595

7323

7073

6844

6636

6433

26.4

8772

8372

8013

7700

7424

7170

6938

6727

6521

26.6

8897

8489

8123

7805

7525

7267

7032

6818

6609

26.8

9020

8604

8232

7909

7624

7363

7125

6908

6697

27.0

9141

8718

8340

8012

7723

7459

7217

6998

6784

27.2

9262

8831

8447

8114

7822

7554

7310

7088

6871

27.4

9384

8945

8555

8217

7921

7650

7402

7177

6958

08.01.164

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

27.6

9506

9060

8663

8321

8020

7746

7495

7268

7046

27.8

9630

9176

8773

8426

8121

7843

7589

7359

7135

28.0

9757

9295

8885

8532

8223

7941

7684

7451

7224

28.2

9888

9416

9000

8641

8328

8041

7781

7545

7315

28.4

10022

9541

9117

8753

8434

8144

7879

7641

7408

28.6

10161

9671

9239

8868

8544

8249

7980

7739

7503

28.8

10306

9805

9364

8986

8656

8357

8084

7839

7599

29.0

10456

9944

9494

9108

8772

8467

8190

7941

7698

29.2

10610

10086

9626

9232

8890

8579

8298

8045

7799

29.4

10767

10231

9761

9359

9010

8694

8407

8151

7901

29.6

10928

10379

9898

9487

9131

8809

8518

8258

8004

29.8

11090

10529

10037

9617

9254

8926

8630

8365

8107

30.0

11254

10680

10176

9747

9377

9043

8742

8474

8211

30.2

11419

10832

10316

9878

9501

9161

8855

8582

8316

30.4

11584

10983

10456

10009

9624

9278

8967

8690

8420

30.6

11748

11134

10596

10139

9747

9394

9078

8797

8523

30.8

11910

11284

10734

10268

9869

9510

9189

8904

8626

31.0

12072

11433

10871

10396

9990

9625

9299

9010

8729

31.2

12233

11581

11007

10523

10110

9739

9409

9115

8830

31.4

12393

11728

11143

10650

10230

9853

9518

9221

8932

31.6

12554

11876

11279

10777

10350

9967

9627

9326

9033

31.8

12714

12023

11415

10904

10470

10081

9736

9431

9135

Original

07-14-08

08.01.165

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

32.0

12875

12171

11551

11031

10590

10195

9845

9536

9236

32.2

13037

12320

11689

11159

10711

10310

9955

9642

9338

32.4

13200

12469

11827

11288

10833

10426

10065

9748

9441

32.6

13364

12620

11966

11418

10955

10542

10177

9856

9544

32.8

13530

12772

12106

11550

11079

10660

10289

9964

9648

33.0

13698

12926

12249

11683

11205

10779

10403

10073

9753

33.2

13868

13082

12393

11817

11331

10899

10517

10183

9859

33.4

14040

13240

12539

11953

11460

11021

10633

10295

9966

33.6

14215

13400

12687

12091

11590

11144

10750

10407

10074

33.8

14393

13563

12837

12231

11721

11268

10869

10521

10183

34.0

14574

13728

12989

12373

11854

11394

10989

10636

10293

34.2

14758

13896

13143

12517

11990

11522

11110

10752

10404

34.4

14945

14067

13301

12663

12127

11651

11233

10869

10516

34.6

15136

14241

13460

12811

12266

11782

11357

10988

10630

34.8

15331

14419

13623

12961

12407

11915

11482

11108

10744

35.0

15529

14599

13787

13114

12549

12049

11609

11229

10859

35.2

15729

14782

13954

13268

12693

12184

11737

11351

10976

35.4

15932

14966

14122

13423

12838

12321

11866

11473

11092

35.6

16137

15152

14291

13580

12984

12457

11995

11597

11209

35.8

16342

15339

14461

13736

13131

12595

12125

11720

11327

36.0

16548

15526

14631

13893

13277

12732

12255

11843

11444

36.2

16753

15713

14801

14050

13423

12869

12384

11966

11561

08.01.166

07-14-08

1.00

1.50

2.00

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

36.4

16958

15898

14969

14206

13569

13006

12513

12089

11678

36.6

17162

16083

15137

14361

13714

13142

12641

12211

11794

36.8

17363

16266

15304

14514

13858

13277

12769

12332

11910

37.0

17564

16448

15469

14667

14000

13411

12895

12453

12025

37.2

17764

16630

15634

14819

14143

13545

13022

12574

12139

37.4

17963

16811

15799

14972

14285

13678

13148

12694

12254

37.6

18163

16992

15964

15124

14428

13813

13275

12815

12369

37.8

18364

17175

16130

15278

14572

13948

13403

12936

12485

38.0

18566

17359

16298

15433

14717

14083

13531

13059

12602

38.2

18770

17544

16467

15590

14863

14221

13661

13182

12719

38.4

18977

17733

16639

15748

15011

14360

13792

13307

12838

38.6

19187

17925

16814

15910

15162

14501

13926

13434

12958

38.8

19401

18120

16992

16074

15315

14645

14061

13562

13081

39.0

19518

18318

17174

16242

15471

14791

14199

13693

13204

39.2

19838

18519

17357

16411

15629

14939

14338

13825

13330

39.4

20060

18723

17544

16583

15789

15088

14479

13958

13456

39.6

20284

18928

17732

16757

15950

15239

14621

14093

13583

39.8

20511

19136

17921

16931

16113

15391

14764

14229

13712

40.0

20738

19344

18112

17107

16276

15544

14908

14365

13840

40.2

20967

19553

18303

17284

16440

15697

15052

14501

13969

40.4

21196

19763

18495

17460

16604

15851

15196

14638

14099

40.6

21425

19973

18687

17637

16768

16004

15340

14774

14228

Original

07-14-08

08.01.167

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

40.8

21654

20183

18878

17813

16932

16157

15484

14911

14357

41.0

21882

20392

19069

17990

17095

16310

15628

15047

14486

41.2

22110

20600

19260

18165

17259

16462

15772

15183

14614

41.4

22339

20809

19451

18341

17421

16615

15915

15319

14743

41.6

22566

21017

19641

18516

17584

16767

16058

15454

14871

41.8

22794

21225

19831

18691

17747

16919

16201

15590

14999

42.0

23021

21433

20021

18866

17909

17071

16344

15725

15127

42.2

23248

21641

20211

19041

18072

17223

16487

15860

15255

42.4

23474

21848

20400

19216

18234

17374

16630

15996

15383

42.6

23701

22056

20590

19391

18397

17526

16773

16131

15512

42.8

23926

22263

20780

19565

18559

17678

16916

16266

15640

43.0

24152

22471

20969

19740

18722

17831

17059

16402

15768

43.2

24377

22677

21158

19915

18885

17983

17202

16538

15897

43.4

24601

22884

21348

20090

19048

18135

17345

16673

16025

43.6

24824

23090

21537

20265

19210

18288

17489

16809

16154

43.8

25046

23295

21725

20439

19373

18440

17632

16945

16282

08.01.168

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

188

182

176

171

167

164

162

161

162

3.2

211

205

199

195

190

187

185

183

183

3.4

235

228

223

218

213

210

207

205

205

3.6

259

252

246

241

237

233

230

228

227

3.8

284

276

271

265

260

256

253

250

248

4.0

309

301

295

289

284

280

276

272

270

4.2

336

327

320

314

308

303

299

294

291

4.4

363

353

346

339

333

327

322

317

313

4.6

392

381

373

365

358

351

345

339

334

4.8

422

410

400

391

383

375

368

362

356

5.0

453

439

428

418

408

400

392

384

377

5.2

485

470

457

445

434

425

415

407

399

5.4

517

501

486

473

461

450

439

430

421

5.6

551

532

516

501

487

475

463

453

443

5.8

584

563

545

529

514

501

488

476

465

6.0

617

595

575

558

541

526

513

500

488

6.2

650

627

605

586

569

553

538

524

511

6.4

683

658

635

615

596

579

563

549

535

6.6

716

689

665

643

624

606

589

574

559

6.8

747

719

694

672

652

633

615

599

585

7.0

778

750

724

701

680

660

642

626

611

Original

07-14-08

08.01.169

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

810

780

754

730

708

688

670

653

638

7.4

842

811

785

760

738

718

699

681

665

7.6

875

844

816

792

769

748

729

711

695

7.8

910

878

850

824

801

780

760

742

725

8.0

947

914

885

859

835

813

793

774

757

8.2

987

952

923

896

871

848

827

808

790

8.4

1030

994

963

935

909

885

864

843

825

8.6

1077

1039

1007

977

950

925

902

881

862

8.8

1127

1087

1053

1022

993

967

943

920

900

9.0

1182

1139

1103

1070

1039

1011

985

962

940

9.2

1239

1194

1155

1120

1087

1057

1030

1004

981

9.4

1298

1251

1209

1171

1136

1104

1075

1048

1023

9.6

1360

1309

1264

1224

1186

1152

1121

1092

1065

9.8

1422

1369

1321

1277

1237

1201

1168

1137

1108

10.0

1485

1429

1377

1331

1289

1250

1214

1182

1151

10.2

1549

1489

1434

1385

1340

1298

1261

1226

1193

10.4

1612

1548

1490

1438

1390

1346

1306

1270

1235

10.6

1673

1606

1545

1490

1439

1393

1351

1312

1276

10.8

1733

1663

1599

1540

1487

1439

1394

1354

1315

11.0

1792

1719

1651

1590

1534

1483

1437

1394

1354

11.2

1850

1774

1703

1638

1580

1527

1478

1434

1392

11.4

1908

1828

1754

1687

1627

1571

1520

1473

1430

08.01.170

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.6

1965

1883

1805

1736

1673

1615

1562

1514

1469

11.8

2023

1937

1857

1785

1720

1660

1605

1554

1508

12.0

2081

1993

1910

1835

1768

1706

1649

1597

1549

12.2

5141

2050

1964

1887

1818

1754

1695

1641

1591

12.4

2203

2109

2021

1941

1869

1803

1743

1687

1636

12.6

2266

2170

2179

1997

1923

1856

1793

1735

1683

12.8

2332

2233

2140

2056

1980

1910

1846

1787

1733

13.0

2400

2298

2203

2117

2039

1968

1902

1841

1786

13.2

2471

2366

2268

2180

2101

2027

1960

1898

1841

13.4

2543

2436

2336

2246

2164

2089

2020

1956

1898

13.6

2617

2508

2405

2313

2229

2153

2082

2017

1957

13.8

2693

2581

2476

2382

2296

2218

2145

2078

2017

14.0

2771

2656

2549

2452

2364

2284

2210

2141

2077

14.2

2850

2732

2622

2523

2433

2351

2275

2205

2139

14.4

2931

2809

2697

2595

2503

2418

2340

2268

2201

14.6

3012

2888

2772

2668

2573

2486

2406

2332

2262

14.8

3095

2967

2845

2741

2644

2554

2471

2396

2323

15.0

3173

3047

2925

2814

2714

2622

2537

2459

2384

15.2

3262

3127

3001

2888

2785

2690

2602

2522

2445

15.4

3346

3208

3078

2962

2856

2758

2667

2585

2505

15.6

3431

3289

3156

3035

2926

2825

2733

2647

2565

15.8

3516

3369

3233

2109

2997

2893

2798

2710

2625

Original

07-14-08

08.01.171

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.0

3600

3450

3310

3183

3068

2961

2863

2772

2685

16.2

3685

3531

3386

3256

3138

3029

2928

2835

2745

16.4

3768

3611

3463

3329

3208

3096

2993

2897

2805

16.6

3851

3690

3539

3402

3279

3164

3058

2960

2865

16.8

3933

3769

3614

3475

3348

3231

3123

3023

2927

17.0

4015

3847

3690

3547

3418

3299

2188

3086

2988

17.2

4097

3925

3765

3620

3489

3367

3254

3149

3050

17.4

4179

4004

3841

3693

3559

3435

3320

3214

3112

17.6

4262

4084

3918

3768

3631

3505

3387

3279

3176

17.8

4346

4164

3996

3843

3704

3575

3456

3346

3240

18.0

4433

4247

4075

3920

3778

3647

3526

3414

3306

18.2

4521

4332

4157

3998

3855

3721

3597

3483

3374

18.4

4612

4419

4240

4079

3933

3797

3671

3554

3443

18.6

4706

4509

4327

4163

4013

3875

3746

3627

3514

18.8

4803

4602

4416

4248

4096

3955

3824

3703

3587

19.0

4904

4698

4508

4337

4181

4037

3903

3780

3662

19.2

5007

4796

4602

4427

4268

4121

3985

3858

3738

19.4

5112

4897

4698

4519

4357

4206

4067

3938

3815

19.6

5219

7999

4795

4612

4446

4293

4151

4019

3893

19.8

5326

5101

4893

4706

4537

4380

4235

4100

3972

20.0

5435

5205

4992

4800

4627

4467

4319

4182

4051

20.2

5543

5308

5090

4895

4718

4555

4403

4263

4129

08.01.172

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

20.4

5651

5411

5188

4988

4808

4642

4487

4344

4208

20.6

5758

5513

5285

5082

4898

4728

4570

4425

4285

20.8

5863

5614

5381

5174

4986

4813

4652

4504

4362

21.0

5968

5713

5476

5265

5074

4897

4734

4583

4438

21.2

6072

5812

5571

5355

5161

4981

4815

5661

4514

21.4

6175

5911

5665

5445

5248

5064

4895

4739

4589

21.6

6278

6010

5759

5536

5335

5149

4976

4817

4664

21.8

6382

6108

5853

5626

5422

5232

5057

4895

4740

22.0

6485

6208

5948

5717

5509

5317

5139

4974

4817

22.2

6592

6308

6044

5809

5598

5403

5221

5054

4894

22.4

6699

6410

6141

5902

5688

5489

5305

5135

4973

22.6

6808

6513

6240

5997

5779

5577

5390

5218

5053

22.8

6919

6619

6340

6093

5872

5667

5477

5302

5135

23.0

7032

6726

6442

6191

5966

5758

5566

5388

5218

23.2

7147

6835

6546

6291

6062

5851

5656

5475

5303

23.4

7264

6945

6652

6392

6160

5945

5747

5564

5389

23.6

7383

7058

6759

6494

6258

6041

5839

5654

5476

23.8

7504

7172

6867

6598

6358

6137

5933

5745

5565

24.0

7627

7287

6977

6703

6459

6235

6027

5836

5654

24.2

7751

7405

7088

6809

6561

6333

6123

5929

5744

24.4

7878

7524

7200

6916

6664

6432

6219

6022

5834

24.6

8006

7644

7313

7024

6767

6532

6315

6116

5924

Original

07-14-08

08.01.173

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

24.8

8136

7766

7428

7132

6872

6632

6412

6210

6015

25.0

8268

7889

7543

7242

6976

6733

6509

6304

6106

25.2

8400

8012

7659

7351

7081

6834

6607

6398

6198

25.4

8533

8137

7775

7461

7187

6935

6704

6492

6289

25.6

8667

8261

7891

7571

7292

7036

6802

6587

6380

25.8

8800

8386

8008

7682

7397

7137

6899

6681

6471

26.0

8933

8510

8124

7791

7502

7238

6997

6775

6562

26.2

9065

8633

8239

7901

7607

7339

7094

6869

6653

26.4

9196

8755

8354

8010

7711

7439

7190

6963

6744

26.6

9326

8876

8468

8118

7815

7539

7287

7056

6834

26.8

9454

8996

8581

8225

7918

7638

7383

7149

6924

27.0

9582

9115

8693

8332

8021

7737

7478

7242

7014

27.2

9709

9234

8805

8439

8123

7836

7574

7334

7104

27.4

9836

9353

8917

8546

8226

7935

7670

7428

7195

27.6

9965

9473

9031

8654

8330

8036

7767

7522

7286

27.8

10097

9596

9126

8764

8436

8137

7865

7617

7378

28.0

10231

9721

9264

8876

8543

8240

7964

7713

7471

28.2

10370

9849

9384

8990

8652

8344

8065

7810

7566

28.4

10513

9982

9508

9107

8763

8451

8168

7910

7662

28.6

10661

10119

9636

9227

8878

8561

8273

8011

7760

28.8

10816

10261

9768

9351

8995

8673

8380

8115

7860

29.0

10976

10409

9904

9479

9116

8787

8490

8221

7962

08.01.174

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

29.2

11141

10560

10043

9608

9238

8904

8602

8328

8065

29.4

11309

10714

10185

9741

9363

9022

8715

8437

8170

29.6

11481

10871

10329

9875

9489

9142

8829

8546

8275

29.8

11655

11030

10475

10010

9616

9262

8944

8657

8381

30.0

11829

11190

10621

10145

9744

9383

9059

8767

8487

30.2

12005

11350

10767

10281

9872

9504

9174

8878

8594

30.4

12180

11510

10913

10416

9999

9625

9289

8988

8700

30.6

12353

11669

11058

10551

10125

9744

9403

9098

8805

30.8

12525

11826

11202

10684

10250

9863

9516

8206

8910

31.0

12695

11981

11344

40815

10374

9980

9628

9314

9013

31.2

12864

12135

11485

10947

10498

10097

9740

9422

9117

31.4

13033

12289

11626

11077

10621

10214

9851

9529

9220

31.6

13201

12443

11767

11208

10744

10331

9963

9636

9323

31.8

13369

12597

11908

11339

10867

10448

10074

9743

9426

32.0

13539

12752

12049

11471

10991

10565

10187

9851

9530

32.2

13710

12908

12192

11603

11116

10684

10300

9959

9635

32.4

13882

13065

12337

11738

11243

10803

10414

10069

9740

32.6

14057

13225

12483

11874

11370

10924

10529

10180

9846

32.8

14235

13387

12632

12012

11500

11047

10646

10292

9954

33.0

14416

13552

12783

12152

11632

11172

10765

10406

10063

33.2

14599

13719

12936

12294

11766

11298

10885

10521

10174

33.4

14786

13889

13091

12439

11901

11426

11007

10637

10285

Original

0.00

07-14-08

.50

1.00

1.50

2.00

08.01.175

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

33.6

14975

14061

13249

12585

12039

11556

11130

10755

10398

33.8

15168

14236

13409

12733

12178

11687

11254

10874

10511

34.0

15363

14414

13572

12883

12318

11820

11380

10994

10626

34.2

15562

14594

13736

13036

12461

11954

11507

11115

10741

34.4

15763

14777

13903

13190

12605

12089

11635

11237

10858

34.6

15968

14963

14072

13345

12750

12226

11765

11360

10975

34.8

16175

15151

14243

13503

12897

12363

11895

11484

11093

35.0

16385

15342

14416

13662

13045

12502

12026

11609

11211

35.2

16597

15534

14590

13822

12195

12642

12158

11734

11330

35.4

16811

15728

14766

13983

13344

12783

12290

11860

11449

35.6

17027

15923

14942

14145

13495

12923

12423

11985

11569

35.8

17242

16118

15119

14307

13646

13064

12555

12111

11688

36.0

17458

16314

15295

14469

13796

13205

12688

12237

11808

36.2

17674

16509

15472

14631

13946

13346

12820

12363

11927

36.4

17889

16703

15647

14792

14096

13486

12953

12488

12046

36.6

18103

16897

15822

14952

14245

13625

13084

12613

12165

36.8

18136

17089

15995

15111

14393

13764

13215

12737

12283

37.0

18527

17279

16168

15269

14541

13902

13345

12861

12400

37.2

18738

17470

16340

15427

14688

14040

13475

12984

12518

37.4

18948

17660

16512

15585

14835

14178

13605

13108

12636

37.6

19160

17851

16685

15744

14983

14317

13736

13232

12754

37.8

19372

18043

16859

15904

15132

14456

13868

18357

12873

08.01.176

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

38.0

19586

18237

17034

16065

15282

14597

14000

13483

12992

38.2

19802

18433

17212

16228

15434

14739

14134

13610

13113

38.4

20020

18631

17392

16394

15588

14883

14270

13739

13235

38.6

20242

18833

17576

16563

15744

15030

14408

13870

13359

38.8

20468

19039

17763

16734

15904

15179

14548

14002

13485

39.0

20696

19248

17953

16909

16066

15330

14690

14137

13612

39.2

20928

19459

18146

17086

16230

15483

14834

14273

13741

39.4

21162

19674

18341

17266

16396

15638

14979

14410

13870

39.6

21398

19890

18538

17447

16564

15794

15126

14549

14001

39.8

21636

20107

18737

17629

16733

15952

15274

14688

14133

40.0

21875

20326

18936

17812

16902

16109

15422

14828

14264

40.2

22115

20546

19136

17996

17072

16268

15570

14968

14397

40.4

22355

20766

19337

18180

17242

16426

15719

15108

14529

40.6

22595

20985

19537

18363

17412

16584

15867

15248

14661

40.8

22834

21204

19736

18546

17581

16742

16015

15388

14793

41.0

23073

21422

19935

18729

17750

16899

16162

15527

14924

41.2

23312

21640

20133

18910

17918

17056

16309

15665

15055

41.4

23550

21857

20331

19092

18086

17212

16456

15804

15185

41.6

23787

22073

20528

19273

18254

17368

16602

15942

15316

41.8

24023

22289

20725

19453

18421

17524

16748

16080

15446

42.0

24259

22505

20922

19634

18588

17679

16894

16218

15577

42.2

24495

22721

21118

19814

18755

17835

17040

16356

15707

Original

07-14-08

08.01.177

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

42.4

24730

22936

21315

19995

18922

17991

17186

16494

15837

42.6

24964

23150

21511

20175

19089

18147

17333

16632

15968

42.8

25197

23365

21707

20355

19256

18303

17479

16770

16099

43.0

25430

23579

21903

20536

19424

18459

17626

16909

16229

43.2

25662

23793

22099

20717

19592

18615

17773

17047

16360

43.4

25893

24006

22295

20897

19759

18772

17920

17186

16492

43.6

26123

24219

22490

21078

19927

18929

18067

17325

16623

43.8

26352

24432

22686

21259

20095

19086

18214

17464

16754

FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

220

213

206

201

195

193

191

192

193

3.2

247

240

233

227

221

219

216

216

216

3.4

274

267

259

253

247

244

241

239

239

3.6

302

294

286

280

273

269

265

263

262

3.8

330

321

313

306

299

295

290

287

284

4.0

359

349

340

333

325

320

314

310

307

4.2

388

377

368

359

351

345

339

333

329

4.4

417

406

395

386

377

370

363

356

351

08.01.178

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

4.6

447

435

423

412

403

394

386

379

372

4.8

478

464

451

439

428

419

410

401

394

5.0

510

494

479

466

454

443

433

423

415

5.2

542

524

508

493

480

467

456

445

436

5.4

574

555

536

520

506

492

480

468

457

5.6

607

586

566

548

532

517

503

490

479

5.8

640

617

595

576

559

542

528

513

501

6.0

674

649

626

604

586

568

552

537

524

6.2

708

682

656

634

614

595

578

562

547

6.4

742

714

687

663

642

622

604

587

572

6.6

777

747

719

694

671

650

632

614

598

6.8

811

780

751

725

701

680

660

642

626

7.0

846

814

784

757

733

710

690

671

654

7.2

882

849

817

790

765

742

721

702

684

7.4

919

885

853

824

798

775

753

734

716

7.6

957

922

889

860

833

809

787

767

748

7.8

997

961

927

897

870

845

822

801

782

8.0

1039

1002

967

936

908

882

859

837

818

8.2

1084

1045

1009

977

948

921

897

874

854

8.4

1131

1091

1053

1020

989

962

936

913

892

8.6

1182

1140

1100

1065

1033

1004

978

953

931

8.8

1236

1191

1149

1113

1079

1048

1020

995

971

Original

07-14-08

08.01.179

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

9.0

1292

1245

1201

1162

1126

1094

1064

1037

1012

9.2

1351

1302

1255

1213

1175

1141

1110

1081

1054

9.4

1412

1360

1310

1265

1225

1189

1155

1125

1097

9.6

1475

1419

1366

1319

1276

1237

1202

1169

1139

9.8

1538

1479

1422

1372

1327

1286

1248

1214

1182

10.0

1602

1539

1479

1426

1378

1335

1295

1258

1224

10.2

1665

1599

1536

1480

1429

1383

1341

1302

1266

10.4

1728

1659

1592

1533

1480

1431

1386

1345

1307

10.6

1790

1717

1647

1584

1529

1477

1431

1388

1348

10.8

1850

1774

1700

1635

1577

1523

1474

1429

1387

11.0

1910

1830

1753

1685

1624

1568

1516

1469

1426

11.2

1968

1885

1805

1734

1670

1612

1558

1510

1464

11.4

2026

1941

1857

1783

1717

1657

1601

1550

1503

11.6

2085

1996

1909

1833

1764

1702

1644

1591

1542

11.8

2144

2052

1962

1884

1813

1748

1688

1633

1582

12.0

2205

2110

2017

1936

1862

1796

1733

1677

1624

12.2

2267

2169

2073

1990

1914

1845

1781

1722

1668

12.4

2331

2231

2132

2046

1968

1897

1831

1771

1715

12.6

2399

2295

2193

2105

2025

1952

1884

1822

1765

12.8

2469

2362

2258

2167

2085

2010

1940

1876

1818

13.0

2542

2432

2326

2232

2148

2071

1999

1934

1873

13.2

2617

2505

2396

2300

2213

2135

2061

1994

1932

08.01.180

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

13.4

2695

2580

2468

2370

2281

2200

2125

2056

1992

13.6

2775

2657

2542

2442

2350

2268

2190

2120

2054

13.8

2857

2736

2618

2515

2421

2336

2257

2185

2118

14.0

2940

2816

2695

2589

2493

2406

2325

2251

2182

14.2

3024

2897

2773

2664

2566

2476

2393

2317

2246

14.4

3109

2978

2851

2739

2639

2547

2461

2383

2310

14.6

3195

3060

2930

2815

2712

2617

2529

2449

2374

14.8

3280

3142

3008

2890

2784

2686

2596

2514

2436

15.0

3366

3224

3087

2965

2856

2755

2663

2578

2498

15.2

3453

3306

3165

3040

2928

2824

2729

2641

2559

15.4

3539

3389

3243

3115

2999

2893

2795

2704

2619

15.6

3625

3471

3321

3189

3071

2961

2860

2767

2679

15.8

3712

3553

3400

3264

3142

3029

2925

2830

2740

16.0

3798

3636

3478

3338

3214

3098

2991

2892

2800

16.2

3885

3718

3556

3413

3285

3166

3057

2956

2861

16.4

3971

3800

3635

3488

3357

3235

3123

3019

2922

16.6

4057

3883

3713

3564

3430

3305

3190

3084

2984

16.8

4143

3965

3792

3639

3503

3375

3258

3149

3047

17.0

4230

4048

3872

3716

3576

3446

3326

3215

3111

17.2

4317

4131

3952

3793

3650

3518

3396

3283

3177

17.4

4404

4215

4033

3871

3726

3591

3466

3351

3243

17.6

4493

4301

4115

3950

3802

3665

3538

3421

3311

Original

07-14-08

08.01.181

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

17.8

4583

4387

4198

4030

3880

3740

3611

3492

3380

18.0

4676

4476

4283

4112

3959

3816

3685

3564

3450

18.2

4770

4566

4369

4195

4039

3894

3761

3637

3521

18.4

4867

4659

4458

4281

4122

3974

3838

3712

3594

18.6

4966

4754

4549

4368

4206

4056

3917

3789

3668

18.8

5069

4851

4642

4458

4292

4139

3997

3867

3744

19.0

5174

4952

4738

4549

4380

4224

4079

3946

3821

19.2

5281

5054

4835

4642

4470

4310

4162

4026

3899

19.4

5390

5157

4933

4736

4560

4397

4247

4108

3977

19.6

5501

5262

5033

4831

4652

4485

4331

4190

4056

19.8

5612

5368

5133

4927

4744

4573

4417

4272

4136

20.0

5723

5474

5233

5023

4836

4662

4502

4354

4215

20.2

5835

5579

5333

5119

4928

4750

4587

4436

4294

20.4

5945

5684

5433

5214

5019

4838

4672

4518

4373

20.6

6055

5789

5532

5308

5110

4926

4756

4599

4451

20.8

6163

5892

5630

5402

5200

5012

4839

4679

4529

21.0

6270

5993

5727

5495

5289

5098

4921

4759

4605

21.2

6376

6095

5823

5587

5377

5183

5003

4838

4682

21.4

6483

6196

5919

5679

5466

5268

5086

4917

4758

21.6

6589

6297

6016

5771

5555

5354

5168

4997

4835

21.8

6697

6400

6113

5864

5644

5440

5251

5077

4913

22.0

6805

6503

6211

5958

5735

5527

5335

5158

4991

08.01.182

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

22.2

6915

6608

6310

6053

5826

5615

5420

5240

5071

22.4

7028

6714

6412

6150

5919

5705

5506

5324

5152

22.6

7143

6823

6515

6249

6014

5796

5595

5409

5235

22.8

7261

6935

6621

6350

6111

5890

5685

5497

5320

23.0

7382

7049

6729

6453

6210

5985

5778

5586

5406

23.2

7506

7166

6839

6558

6311

6083

5872

5678

5495

23.4

7632

7284

6951

6664

6413

6181

5967

5770

5585

23.6

7761

7405

7064

6772

6517

6281

6064

5864

5676

23.8

7891

7527

7179

6881

6622

6382

6162

5959

5768

24.0

8023

7651

7295

6992

6728

6484

6260

6054

5861

24.2

8157

7776

7412

7103

6834

6586

6359

6150

5954

24.4

8292

7902

7530

7214

6941

6689

6459

6247

6047

24.6

8428

8028

7648

7326

7048

6792

6558

6343

6141

24.8

8565

8156

7767

7438

7156

6895

6657

6439

6234

25.0

8702

8284

7886

7551

7263

6998

6757

6535

6327

25.2

8841

8412

8005

7663

7371

7101

6856

6631

6419

25.4

8979

8541

8125

7776

7478

7204

6955

6726

6512

25.6

9118

8669

8244

7888

7586

7307

7054

6822

6604

25.8

9256

8798

8364

8001

7693

7410

7153

6918

6697

26.0

9395

8926

8483

8113

7801

7513

7252

7013

6789

26.2

9533

9055

8602

8226

7908

7616

7351

7109

6882

26.4

9671

9183

8721

8338

8015

7719

7450

7205

6974

Original

07-14-08

08.01.183

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

26.6

9807

9310

8840

8450

8123

7822

7550

7301

7067

26.8

9943

9437

8959

8563

8230

7925

7649

7397

7160

27.0

10079

9563

9077

8675

8338

8029

7749

7494

7254

27.2

10216

9691

9196

8788

8446

8133

7850

7591

7348

27.4

10353

9819

9317

8902

8555

8238

7951

7689

7443

27.6

10493

9949

9438

9017

8666

8344

8053

7788

7539

27.8

10635

10081

9562

9134

8777

8451

8156

7887

7635

28.0

10781

10217

9688

9253

8890

8559

8260

7988

7733

28.2

10931

10355

9817

9374

9006

8669

8366

8090

7832

28.4

11086

10498

9949

9498

9123

8781

8474

8194

7932

28.6

11247

10646

10084

9624

9243

8896

8583

8300

8034

28.8

11413

10798

10224

9754

9366

9012

8695

8407

8137

29.0

11585

10955

10367

9887

9491

9131

8808

8515

8242

29.2

11762

11116

10513

10022

9618

9251

8923

8625

8348

29.4

11942

11279

10661

10159

9747

9373

9038

8736

8454

29.6

12125

11445

10811

10298

9877

9495

9155

8848

8562

29.8

12310

11612

10962

10437

10008

9618

9272

8960

8669

30.0

12496

11781

11114

10576

10138

9742

9389

9072

8777

30.2

12682

11949

11266

10716

10269

9865

9506

9185

8885

30.4

12867

12116

11416

10855

10400

9988

9623

9296

8992

30.6

13050

12282

11566

10993

10529

10109

9739

9407

9099

30.8

13230

12445

11714

11129

10657

10230

9853

9518

9205

08.01.184

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

31.0

13409

12607

11860

11264

10784

10350

9968

9627

9310

31.2

13587

12768

12006

11399

10910

10470

10081

9736

9415

31.4

13764

12929

12152

11533

11037

10589

10195

9846

9520

31.6

13941

13090

12297

11668

11163

10709

10309

9955

9625

31.8

14119

13251

12444

11803

11290

10829

10423

10065

9731

32.0

14298

13414

12591

11940

11419

10951

10539

10175

9837

32.2

14480

13579

12741

12078

11549

11073

10655

10287

9945

32.4

14664

13747

12893

12218

11680

11197

10774

10400

10053

32.6

14852

13917

13048

12361

11814

11324

10894

10515

10163

32.8

15045

14092

13206

12507

11951

11453

11016

10632

10275

33.0

15241

14270

13368

12656

12090

11583

11140

10750

10389

33.2

15442

14452

13532

12808

12232

11716

11266

10870

10503

33.4

15646

14637

13699

12961

12375

11851

11394

10992

10620

33.6

15853

14824

13869

13117

12521

11988

11523

11115

10737

33.8

16063

15015

14041

13275

12668

12126

11653

11239

10855

34.0

16277

15208

14215

13435

12817

12265

11785

11364

10974

34.2

16492

15403

14391

13597

12967

12406

11917

11490

11094

34.4

16710

15600

14569

13759

13119

12547

12050

11616

11214

34.6

16931

15799

14748

13923

13271

12689

12184

11743

11335

34.8

17153

15999

14928

14088

13424

12832

12319

11870

11456

35.0

17376

16201

15109

14253

13577

12975

12453

11998

11577

35.2

17601

16403

15291

14419

13731

13118

12588

12126

11699

Original

07-14-08

1.00

1.50

2.00

08.01.185

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

35.4

17827

16607

15473

14586

13885

13262

12723

12254

11820

35.6

18053

16811

15656

14752

14040

13406

12858

12381

11941

35.8

18280

17015

15839

14919

14195

13550

12994

12509

12063

36.0

18507

17219

16022

15086

14349

13694

13129

12637

12184

36.2

18734

17423

16205

15253

14504

13838

13264

12765

12305

36.4

18960

17627

16388

15419

14658

13981

13399

12893

12427

36.6

19185

17830

16569

15585

14811

14125

13534

13021

12548

36.8

19410

18032

16750

15750

14965

14268

13668

13148

12669

37.0

19634

18234

16931

15915

15118

14411

13802

13275

12790

37.2

19858

18435

17112

16080

15271

14554

13937

13403

12911

37.4

20082

18637

17293

16246

15425

14697

14072

13530

13032

37.6

20307

18840

17475

16413

15579

14841

14207

13659

13154

37.8

20532

19044

17658

16581

15735

14987

14344

13788

13277

38.0

20760

19250

17844

16750

15892

15133

14482

13918

13400

38.2

20990

19457

18031

16921

16050

15281

14621

14050

13525

38.4

21222

19668

18221

17095

16211

15431

14761

14183

13651

38.6

21457

19881

18414

17272

16375

15583

14904

14318

13779

38.8

21695

20098

18610

17451

16541

15738

15049

14454

13908

39.0

21936

20318

18809

17634

16709

15894

15195

14592

14038

39.2

22180

20540

19011

17818

16880

16053

15343

14732

14170

39.4

22426

20765

19215

18005

17052

16212

15493

14873

14303

39.6

22674

20991

19420

18193

17226

16373

15643

15015

14437

08.01.186

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

39.8

22923

21219

19627

18382

17400

16535

15795

15157

14571

40.0

23173

21448

19835

18572

17576

16698

15946

15300

14705

40.2

23424

21677

20044

18763

17751

16860

16098

15443

14840

40.4

23676

21907

20252

18953

17927

17023

16250

15585

14975

40.6

23927

22136

20460

19143

18102

17185

16402

15728

15109

40.8

24177

22364

20667

19332

18276

17347

16553

15870

15243

41.0

24427

22592

20873

19520

18450

17507

16703

16012

15377

41.2

24677

22819

21079

19708

18623

17668

16853

16153

15510

41.4

24925

23046

21284

19895

18795

17828

17003

16294

15643

41.6

25173

23271

21489

20082

18968

17988

17152

16434

15775

41.8

25420

23496

21693

20269

19140

18147

17301

16575

15908

42.0

25666

23721

21897

20455

19312

18307

17451

16716

16041

42.2

25911

23944

22100

20642

19484

18467

17600

16856

16173

42.4

26154

24167

22303

20828

19656

18627

17750

16997

16306

42.6

26397

24390

22506

21014

19829

18787

17900

17138

16440

42.8

26638

24612

22709

21201

20001

18948

18050

17280

16573

43.0

26878

24833

22911

21388

20174

19109

18200

17422

16707

43.2

27116

25053

23114

21575

20348

19270

18351

17564

16841

43.4

27353

25273

23316

21762

20521

19432

18503

17706

16975

43.6

27589

25492

23519

21949

20695

19593

18654

17849

17110

43.8

27324

25711

23721

22136

20869

19756

18806

17992

17244

Original

07-14-08

08.01.187

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

266

259

253

248

243

240

238

236

236

3.2

297

289

282

276

270

266

263

260

259

3.4

328

319

311

303

297

292

288

284

282

3.6

359

349

339

331

324

318

313

308

305

3.8

390

379

368

358

350

343

337

332

327

4.0

421

408

396

386

377

369

361

355

349

4.2

451

438

424

413

402

394

385

378

371

4.4

482

467

452

439

428

418

408

400

392

4.6

513

496

480

466

453

442

431

421

413

4.8

544

525

507

491

478

465

453

443

433

5.0

574

555

535

517

502

488

475

464

453

5.2

606

584

562

543

526

511

497

484

473

5.4

637

613

590

569

551

534

519

506

494

5.6

669

644

618

596

576

558

542

527

515

5.8

702

675

647

623

602

583

565

550

536

6.0

736

706

677

652

629

608

590

574

559

6.2

770

739

708

681

657

635

616

599

584

6.4

806

773

741

712

687

664

643

625

610

6.6

843

809

775

745

719

695

673

654

638

6.8

881

846

810

779

752

727

705

685

668

7.0

921

884

848

816

788

762

739

718

700

7.2

963

925

887

854

825

798

774

753

735

08.01.188

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.4

1006

967

928

894

864

836

812

790

770

7.6

1051

1011

970

935

904

876

851

828

808

7.8

1098

1056

1015

978

946

917

891

867

846

8.0

1147

1103

1060

1023

990

960

932

908

885

8.2

1198

1152

1108

1069

1034

1003

975

949

926

8.4

1251

1203

1157

1116

1080

1048

1018

991

966

8.6

1306

1256

1207

1165

1127

1093

1062

1033

1007

8.8

1363

1311

1260

1215

1175

1139

1106

1076

1048

9.0

1422

1367

1313

1265

1224

1186

1151

1119

1090

9.2

1483

1425

1367

1317

1273

1233

1196

1162

1131

9.4

1545

1483

1423

1369

1323

1280

1241

1205

1172

9.6

1608

1543

1478

1422

1373

1328

1287

1249

1214

9.8

1671

1602

1535

1475

1423

1376

1332

1292

1255

10.0

1734

1662

1591

1528

1473

1423

1378

1336

1297

10.2

1797

1722

1647

1581

1524

1471

1423

1379

1338

10.4

1860

1781

1702

1634

1573

1519

1468

1422

1380

10.6

1921

1839

1757

1686

1623

1566

1513

1465

1421

10.8

1982

1896

1812

1737

1672

1613

1558

1508

1462

11.0

2042

1953

1865

1788

1721

1659

1603

1551

1504

11.2

2101

2010

1919

1840

1770

1706

1648

1595

1546

11.4

2161

2066

1973

1891

1819

1754

1694

1639

1589

11.6

2221

2124

2028

1944

1870

1803

1741

1684

1633

Original

07-14-08

08.01.189

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.8

2283

2183

2084

1998

1922

1853

1789

1731

1678

12.0

2346

2244

2142

2053

1975

1904

1839

1779

1725

12.2

2412

2306

2202

2111

2031

1958

1890

1829

1773

12.4

2481

2372

2265

2171

2089

2014

1944

1881

1824

12.6

2552

2441

2331

2234

2149

2072

2001

1936

1877

12.8

2628

2513

2400

2301

2213

2134

2060

1993

1933

13.0

2707

2588

2472

2370

2280

2198

2122

2053

1991

13.2

2788

2666

2546

2441

2349

2264

2186

2115

2051

13.4

2872

2747

2623

2515

2419

2332

2252

2179

2112

13.6

2958

2829

2702

2590

2492

2402

2319

2244

2175

13.8

3046

2913

2781

2666

2565

2473

2387

2309

2238

14.0

3135

2997

2862

2743

2639

2544

2456

2375

2301

14.2

3224

3083

2943

2821

2713

2615

2525

2442

2365

14.4

3314

3168

3024

2898

2788

2686

2593

2507

2428

14.6

3403

3253

3105

2975

2861

2757

2661

2573

2491

14.8

3491

3337

3185

3051

2934

2827

2728

2637

2552

15.0

3579

3421

3264

3127

3006

2895

2793

2700

2613

15.2

3667

3504

3343

3202

3078

2964

2859

2762

2672

15.4

3754

3587

3422

3277

3149

3032

2924

2825

2732

15.6

3842

3670

3500

3351

3220

3100

2989

2887

2792

15.8

3930

3754

3579

3426

3292

3169

3055

2950

2852

16.0

4018

3837

3659

3502

3364

3238

3121

3013

2913

08.01.190

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.2

4106

3921

3739

3578

3437

3307

3188

3077

2975

16.4

4195

4006

3819

3655

3511

3378

3256

3143

3038

16.6

4286

4092

3901

3734

3586

3451

3325

3210

3102

16.8

4377

4180

3984

3813

3663

3524

3397

3279

3169

17.0

4469

4268

4069

3895

3741

3600

3469

3349

3237

17.2

4563

4358

4155

3977

3820

3677

3544

3421

3307

17.4

4659

4449

4242

4061

3901

3755

3620

3495

3379

17.6

4755

4542

4331

4146

3984

3835

3697

3570

3452

17.8

4854

4636

4421

4233

4067

3916

3775

3646

3526

18.0

4954

4732

4512

4321

4152

3998

3855

3724

3601

18.2

5056

4829

4605

4410

4238

4081

3936

3802

3677

18.4

5161

4928

4700

4501

4326

4166

4017

3881

3754

18.6

5267

5030

4796

4593

4414

4251

4100

3961

3832

18.8

5376

5133

4894

4686

4504

4337

4183

4042

3910

19.0

5486

5237

4993

4780

4595

4425

4268

4123

3988

19.2

5598

5343

5093

4876

4686

4513

4352

4205

4067

19.4

5711

5450

5194

4972

4778

4601

4437

4287

4146

19.6

5825

5558

5295

5068

4871

4690

4523

4369

4226

19.8

5939

5666

5397

5165

4964

4779

4608

4451

4305

20.0

6053

5774

5499

5262

5056

4868

4694

4534

4384

20.2

6167

5881

5601

5359

5149

4957

4779

4616

4464

20.4

6280

5988

5702

5456

5242

5046

4865

4698

4543

Original

07-14-08

08.01.191

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

20.6

6392

6095

5802

5551

5334

5134

4950

4780

4622

20.8

6503

6200

5902

5647

5425

5222

5035

4862

4701

21.0

6612

6304

6001

5742

5516

5310

5119

4943

4780

21.2

6721

6408

6100

5836

5607

5398

5204

5025

4859

21.4

6831

6512

6200

5931

5699

5486

5288

5107

4938

21.6

6941

6618

6300

6027

5791

5574

5374

5190

5018

21.8

7053

6724

6401

6124

5883

5664

5460

5273

5099

22.0

7167

6832

6503

6221

5977

5754

5548

5358

5181

22.2

7284

6942

6607

6321

6073

5846

5636

5444

5264

22.4

7404

7055

6714

6422

6170

5940

5727

5531

5349

22.6

7527

7172

6823

6526

6270

6036

5819

5620

5436

22.8

7655

7291

6935

6632

6371

6133

5914

5712

5524

23.0

7787

7414

7050

6741

6475

6233

6010

5805

5614

23.2

7923

7540

7167

6851

6581

6335

6107

5899

5706

23.4

8061

7669

7286

6963

6688

6437

6207

5995

5798

23.6

8202

7799

7407

7077

6796

6541

6307

6092

5892

23.8

8344

7931

7528

7191

6905

6646

6408

6189

5986

24.0

8488

8064

7651

7306

7015

6751

6509

6287

6081

24.2

8633

8197

7774

7422

7125

6857

6611

6385

6176

24.4

8778

8331

7897

7538

7235

6963

6712

6484

6271

24.6

8923

8465

8020

7653

7345

7068

6814

6581

6365

24.8

9067

8598

8143

7768

7455

7173

6914

6679

6459

08.01.192

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

25.0

9210

8730

8265

7883

7564

7277

7015

6776

6552

25.2

9354

8863

8387

7997

7673

7381

7115

6872

6646

25.4

9497

8995

8509

8111

7781

7485

7215

6969

6739

25.6

9640

9127

8630

8225

7890

7590

7315

7065

6832

25.8

9784

9260

8753

8340

7999

7694

7415

7162

6925

26.0

9928

9393

8875

8455

8109

7799

7516

7259

7019

26.2

10073

9527

8999

8571

8219

7904

7617

7357

7113

26.4

10219

9661

9123

8687

8330

8010

7719

7455

7208

26.6

10366

9797

9248

8805

8442

8117

7822

7554

7304

26.8

10514

9934

9374

8923

8554

8225

7926

7654

7401

27.0

10665

10072

9502

9043

8668

8335

8031

7755

7499

27.2

10817

10213

9631

9164

8784

8445

8137

7858

7598

27.4

10972

10355

9762

9287

8900

8556

8244

7961

7698

27.6

11129

10500

9895

9411

9018

8669

8352

8065

7798

27.8

11290

10647

10030

9537

9138

8783

8461

8171

7900

28.0

11455

10798

10168

9665

9259

8898

8572

8277

8003

28.2

11623

10951

10308

9795

9381

9015

8683

8384

8106

28.4

11795

11108

10450

9927

9506

9133

8796

8493

8211

28.6

11973

11269

10595

10061

9632

9253

8910

8602

8316

28.8

12155

11433

10744

10198

9760

9374

9026

8713

8423

29.0

12341

11601

10895

10336

9890

9496

9142

8824

8530

29.2

12530

11772

11047

10476

10020

9619

9259

8936

8637

Original

07-14-08

08.01.193

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

29.4

12722

11945

11202

10617

10152

9744

9377

9049

8746

29.6

12917

12119

11357

10759

10285

9868

9495

9162

8854

29.8

13113

12294

11513

10902

10418

9993

9614

9275

8963

30.0

13307

12476

11670

11044

10551

10118

9732

9389

9071

30.2

13502

12644

11825

11187

10683

10243

9851

9502

9180

30.4

13695

12818

11981

11328

10815

10368

9969

9615

9288

30.6

13887

12990

12134

11469

10947

10492

10086

9728

9396

30.8

14076

13160

12286

11608

11077

10615

10203

9840

9504

31.0

14263

13329

12437

11747

11207

10737

10320

9952

9612

31.2

14449

13496

12588

11885

11337

10860

10437

10063

9719

31.4

14635

13664

12738

12023

11466

10983

10553

10175

9827

31.6

14821

13832

12890

12163

11597

11106

10671

10288

9935

31.8

15010

14003

13043

12303

11729

11230

10789

10401

10044

32.0

15201

14175

13198

12446

11862

11356

10908

10515

10153

32.2

15396

14351

13356

12590

11997

11484

11029

10631

10264

32.4

15596

14531

13517

12738

12135

11613

11152

10748

10377

32.6

15801

14716

13683

12890

12276

11746

11277

10867

10491

32.8

16012

14906

13853

13045

12420

11881

11405

10989

10606

33.0

16229

15101

14027

13204

12567

12018

11535

11112

10724

33.2

16451

15301

14206

13366

12717

12158

11666

11237

10843

33.4

16677

15504

14387

13531

12870

12300

11800

11363

10963

33.6

16908

15711

14572

13698

13024

12444

11935

11491

11084

08.01.194

07-14-08

1.00

1.50

2.00

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

33.8

17141

15920

14758

13867

13179

12589

12071

11619

11206

34.0

17377

16132

14946

14037

13336

12735

12207

11749

11329

34.2

17614

16345

15136

14208

13494

12881

12345

11879

11452

34.4

17853

16559

15326

14380

13652

13028

12482

12008

11575

34.6

18091

16773

15516

14552

13810

13175

12620

12138

11698

34.8

18330

16986

15706

14724

13968

13322

12757

12268

11821

35.0

18568

17200

15895

14895

14126

13468

12894

12398

11943

35.2

18806

17413

16085

15066

14283

13614

13031

12527

12066

35.4

19044

17626

16274

15237

14441

13761

13168

12657

12189

35.6

19282

17839

16464

15409

14598

13907

13305

12786

12311

35.8

19520

18052

16653

15580

14756

14053

13442

12916

12434

36.0

19758

18266

16843

15751

14914

14200

13580

13045

12557

36.2

19996

18479

17032

15923

15072

14347

13717

13175

12680

36.4

20234

18693

17222

16095

15230

14494

13855

13306

12803

36.6

20473

18906

17413

16268

15389

14642

13993

13436

12927

36.8

20711

19121

17604

16441

15549

14790

14132

13568

13051

37.0

20950

19336

17796

16615

15709

14939

14272

13699

13176

37.2

21190

19551

17988

16789

15870

15089

14412

13832

13302

37.4

21431

19768

18182

16965

16032

15239

14553

13965

13428

37.6

21672

19985

18377

17142

16195

15391

14695

14099

13554

37.8

21915

20205

18573

17321

16360

15544

14838

14233

13682

38.0

22159

20425

18771

17501

16526

15698

14982

14369

13810

Original

07-14-08

08.01.195

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

38.2

22405

20648

18971

17683

16693

15853

15128

14506

13940

38.4

22653

20872

19173

17867

16862

16010

15274

14644

14070

38.6

22902

21099

19378

18053

17034

16169

15422

14783

14202

38.8

23154

21328

19584

18241

17207

16329

15572

14924

14334

39.0

23408

21559

19793

18431

17381

16491

15723

15066

14468

39.2

23664

21792

20004

18623

17558

16654

15875

15208

14602

39.4

23921

22026

20216

18816

17735

16818

16027

15352

14737

39.6

24179

22262

20429

19010

17914

16983

16181

15496

14872

39.8

24439

22499

20644

19206

18093

17149

16335

15640

15008

40.0

24700

22737

20859

19401

18272

17314

16489

15785

15144

40.2

24961

22975

21074

19597

18452

17480

16643

15930

15280

40.4

25223

23213

21289

19793

18632

17646

16798

16074

15416

40.6

25485

23452

21504

19988

18811

17811

16951

16219

15552

40.8

25747

23690

21719

20183

18989

17976

17105

16363

15687

41.0

26009

23928

21933

20377

19167

18140

17258

16506

15822

41.2

26271

24165

22146

20571

19345

18304

17410

16649

15957

41.4

26532

24402

22359

20764

19522

18468

17563

16793

16092

41.6

26792

24637

22572

20957

19699

18632

17715

16936

16227

41.8

27050

24872

22784

21150

19876

18795

17868

17079

16361

42.0

27307

25106

22995

21342

20053

18959

18020

17222

16496

42.2

27562

25339

23207

21535

20230

19123

18173

17366

16631

42.4

27815

25571

23418

21728

20408

19288

18327

17510

16767

08.01.196

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

42.6

28065

25801

23628

21921

20586

19453

18481

17655

16903

42.8

28312

26036

23839

22115

20765

19619

18635

17800

17040

43.0

28558

26258

24049

22309

20944

19785

18791

17946

17177

43.2

28800

26484

24259

22503

21124

19952

18947

18092

17314

43.4

29041

26710

24468

22698

21304

20120

19103

18239

17452

43.6

29280

26934

24678

22892

21485

20288

19260

18386

17591

43.8

29518

27158

24887

23087

21666

20456

19417

18533

17729

FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

318

312

308

303

299

295

292

288

285

3.2

352

345

338

331

326

321

317

311

307

3.4

386

376

368

360

353

347

341

335

330

3.6

419

408

398

388

380

372

365

358

352

3.8

452

439

427

416

406

397

389

381

374

4.0

485

470

456

443

432

422

413

403

395

4.2

517

500

484

470

457

446

435

425

416

4.4

548

530

512

496

482

469

457

446

436

Original

07-14-08

08.01.197

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

4.6

579

559

538

521

506

492

479

466

456

4.8

609

587

565

546

529

513

499

486

475

5.0

639

615

591

570

551

535

519

505

493

5.2

669

643

616

594

574

556

539

525

512

5.4

699

671

643

619

597

578

560

545

531

5.6

730

700

670

644

621

600

581

565

552

5.8

762

730

698

671

646

624

604

587

573

6.0

795

762

728

699

673

649

628

611

596

6.2

830

795

759

729

702

677

654

637

621

6.4

868

831

793

761

733

707

684

665

649

6.6

908

869

830

797

767

740

716

696

679

6.8

950

910

870

835

805

776

751

731

713

7.0

996

954

912

877

845

816

789

768

749

7.2

1043

1001

957

920

888

858

830

808

788

7.4

1094

1049

1005

966

933

902

873

850

829

7.6

1146

1100

1054

1014

980

947

918

893

871

7.8

1200

1152

1105

1064

1028

994

964

938

914

8.0

1256

1206

1157

1114

1077

1043

1011

983

958

8.2

1313

1262

1210

1166

1127

1091

1058

1029

1002

8.4

1372

1318

1264

1218

1177

1140

1106

1074

1046

8.6

1431

1375

1319

1270

1227

1188

1152

1119

1089

8.8

1492

1433

1373

1322

1277

1236

1198

1163

1131

08.01.198

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

9.0

1552

1491

1428

1374

1327

1283

1243

1206

1172

9.2

1615

1549

1483

1426

1376

1330

1288

1249

1213

9.4

1678

1608

1538

1478

1425

1377

1332

1291

1253

9.6

1740

1667

1593

1530

1474

1423

1376

1333

1293

9.8

1803

1726

1648

1582

1523

1470

1420

1375

1333

10.0

1866

1785

1704

1634

1572

1516

1464

1417

1373

10.2

1928

1844

1759

1686

1622

1563

1509

1460

1414

10.4

1990

1903

1814

1739

1672

1611

1555

1503

1456

10.6

2052

1961

1869

1791

1722

1659

1601

1548

1499

10.8

2113

2019

1925

1844

1773

1708

1648

1593

1543

11.0

2173

2077

1980

1897

1824

1757

1696

1640

1589

11.2

2234

2135

2036

1952

1877

1808

1745

1688

1636

11.4

2296

2195

2094

2007

1930

1860

1796

1737

1684

11.6

2359

2256

2152

2063

1985

1914

1848

1788

1734

11.8

2424

2318

2212

2122

2042

1969

1902

1840

1785

12.0

2491

2382

2275

2182

2100

2025

1957

1894

1837

12.2

2561

2449

2339

2244

2161

2084

2014

1950

1891

12.4

2633

2520

2407

2309

2223

2145

2073

2007

1947

12.6

2710

2593

2477

2377

2289

2208

2134

2066

2004

12.8

2791

2670

2550

2447

2356

2273

2197

2126

2063

13.0

2875

2751

2627

2520

2426

2340

2261

2189

2123

13.2

2963

2834

2706

2595

2498

2409

2328

2252

2184

Original

07-14-08

08.01.199

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

13.4

3053

2919

2786

2672

2572

2479

2395

2316

2245

13.6

3144

3006

2869

2750

2646

2550

2462

2381

2308

13.8

3237

3094

2952

2829

2721

2622

2531

2447

2370

14.0

3331

3183

3035

2908

2796

2694

2599

2512

2433

14.2

3425

3272

3119

2988

2872

2765

2667

2577

2495

14.4

3518

3360

3202

3066

2946

2836

2735

2642

2556

14.6

3611

3447

3284

3144

3020

2907

2802

2705

2617

14.8

3701

3533

3365

3221

3093

2976

2867

2768

2676

15.0

3791

3618

3444

3296

3164

3044

2932

2830

2735

15.2

3880

3702

3523

3371

3236

3111

2996

2891

2794

15.4

3968

3785

3602

3446

3306

3179

3061

2953

2852

15.6

4056

3869

3681

3520

3378

3247

3126

3015

2912

15.8

4145

3953

3760

3596

3450

3315

3191

3077

2972

16.0

4234

4038

3841

3672

3523

3385

3258

3141

3033

16.2

4325

4124

3922

3750

3597

3456

3326

3207

3096

16.4

4417

4212

4006

3830

3673

3530

3396

3275

3161

16.6

4511

4301

4091

3911

3752

3605

3469

3345

3229

16.8

4608

4394

4179

3996

3833

3683

3544

3418

3300

17.0

4707

4488

4269

4082

3916

3764

3622

3493

3373

17.2

4808

4585

4361

4171

4001

3846

3702

3571

3449

17.4

4911

4683

4455

4261

4089

3931

3784

3650

3526

17.6

5016

4784

4551

4353

4178

4017

3868

3731

3605

08.01.200

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

17.8

5123

4886

4649

4447

4268

4104

3952

3814

3685

18.0

5232

4990

4747

4542

4360

4193

4038

3897

3766

18.2

5343

5095

4847

4637

4452

4282

4124

3980

3847

18.4

5455

5201

4948

4734

4545

4371

4211

4064

3928

18.6

5568

5309

5050

4831

4638

4461

4298

4148

4009

18.8

5683

5417

5152

4928

4731

4551

4384

4232

4090

19.0

5798

5526

5254

5026

4825

4641

4471

4315

4170

19.2

5914

5636

5357

5124

4919

4730

4557

4398

4250

19.4

6031

5746

5461

5222

5012

4820

4643

4480

4330

19.6

6148

5856

5564

5320

5106

4910

4729

4563

4409

19.8

6265

5966

5667

5418

5200

4999

4814

4645

4488

20.0

6382

6076

5771

5516

5293

5089

4900

4728

4568

20.2

6498

6185

5874

5614

5387

5179

4986

4811

4647

20.4

6613

6294

5976

5712

5480

5269

5073

4894

4727

20.6

6727

6402

6079

5810

5574

5358

5159

4977

4808

20.8

6840

6510

6181

5907

5668

5448

5246

5061

4888

21.0

6952

6617

6282

6005

5761

5539

5333

5145

4970

21.2

7065

6724

6385

6102

5855

5629

5420

5230

5052

21.4

7178

6832

6487

6201

5950

5721

5509

5315

5135

21.6

7292

6941

6591

6300

6046

5813

5598

5402

5219

21.8

7409

7052

6697

6401

6143

5907

5689

5490

5305

22.0

7528

7165

6804

6504

6242

6002

5781

5579

5391

Original

07-14-08

08.01.201

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

22.2

7652

7281

6914

6608

6342

6099

5874

5669

5479

22.4

7779

7401

7026

6715

6445

6197

5969

5761

5568

22.6

7912

7525

7141

6825

6549

6298

6066

5854

5658

22.8

8050

7654

7260

6937

6656

6401

6165

5950

5750

23.0

8193

7786

7382

7052

6766

6505

6255

6047

5844

23.2

8340

7922

7507

7169

6877

6611

6367

6145

5939

23.4

8490

8060

7633

7287

6989

6719

6470

6244

6034

23.6

8643

8200

7761

7407

7103

6827

6574

6344

6130

23.8

8798

8342

7890

7527

7217

6936

6678

6444

6227

24.0

8953

8484

8020

7648

7331

7045

6782

6544

6324

24.2

9109

8626

8149

7769

7446

7154

6887

6645

6420

24.4

9263

8767

8277

7889

7559

7263

6991

6745

6517

24.6

9416

8908

8405

8008

7672

7370

7094

6844

6612

24.8

9567

9046

8531

8126

7784

7477

7196

6942

6707

25.0

9716

9183

8656

8243

7895

7583

7298

7040

6801

25.2

9864

9318

8780

8359

8006

7689

7399

7138

6895

25.4

10012

9454

8904

8475

8116

7794

7500

7235

6989

25.6

10159

9589

9028

8592

8226

7900

7601

7332

7083

25.8

10307

9726

9153

8709

8338

8006

7703

7430

7177

26.0

10457

9863

9279

8827

8450

8113

7805

7529

7273

26.2

10609

10003

9406

8946

8563

8221

7909

7629

7369

26.4

10763

10144

9536

9068

8678

8331

8015

7731

7467

08.01.202

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

26.6

10921

10289

9668

9191

8795

8443

8122

7834

7566

26.8

11083

10437

9804

9318

8915

8557

8231

7939

7667

27.0

11248

10589

9942

9446

9037

8673

8341

8045

7770

27.2

11418

10743

10082

9578

9161

8790

8454

8154

7875

27.4

11591

10901

10226

9711

9287

8910

8568

8263

7981

27.6

11767

11062

10372

9846

9414

9031

8684

8374

8088

27.8

11948

11226

10520

9984

9543

9154

8801

8486

8196

28.0

12132

11393

10670

10123

9674

9277

8918

8599

8304

28.2

12319

11563

10822

10263

9806

9402

9037

8713

8414

28.4

12510

11735

10977

10405

9939

9528

9156

8827

8524

28.6

12704

11910

11133

10549

10073

9654

9276

8942

8634

28.8

12901

12087

11290

10693

10207

9780

9396

9057

8744

29.0

13101

12266

11449

10838

10343

9908

9516

9172

8854

29.2

13303

12446

11609

10984

10478

10035

9637

9287

8964

29.4

13507

12628

11769

11131

10614

10163

9757

9402

9074

29.6

13711

12810

11930

11277

10750

10290

9878

9517

9184

29.8

13915

12992

12091

11424

10887

10418

9999

9632

9294

30.0

14119

13174

12251

11570

11022

10546

10119

9747

9405

30.2

14322

13355

12411

11716

11158

10673

10240

9862

9515

30.4

14524

13535

12570

11861

11293

10800

10360

9977

9625

30.6

14723

13713

12728

12005

11428

10927

10480

10092

9735

30.8

14919

13889

12884

12149

11562

11053

10600

10206

9845

Original

-1.00

-.50

0.00

07-14-08

.50

1.00

1.50

2.00

08.01.203

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

31.0

15114

14064

13040

12292

11696

11179

10720

10321

9955

31.2

15308

14238

13195

12435

11830

11306

10840

10436

10066

31.4

15503

14413

13351

12578

11964

11433

10960

10552

10177

31.6

15699

14590

13509

12723

12100

11561

11082

10668

10289

31.8

15898

14769

13669

12871

12238

11691

11205

10786

10401

32.0

16102

14951

13832

13020

12378

11822

11330

10905

10516

32.2

16310

15139

13999

13173

12520

11956

11456

11026

10631

32.4

16524

15331

14171

13330

12666

12093

11585

11148

10748

32.6

16746

15531

14348

13492

12815

12232

11717

11273

10867

32.8

16976

15737

14531

13658

12969

12375

11851

11400

10988

33.0

17214

15950

14720

13829

13126

12521

11988

11530

11110

33.2

17458

16168

14913

14003

13286

12670

12126

11660

11235

33.4

17707

16390

15109

14181

13449

12821

12267

11793

11360

33.6

17960

16617

15309

14361

13613

12973

12409

11926

11486

33.8

18216

16845

15511

14542

13779

13126

12551

12061

11613

34.0

18474

17076

15714

14725

13946

13280

12695

12195

11740

34.2

18733

17306

15917

14908

14113

13434

12838

12330

11867

34.4

18992

17537

16120

15090

14279

13588

12981

12464

11994

34.6

19249

17766

16322

15272

14445

13741

13123

12598

12120

34.8

19503

17993

16521

15452

14609

13892

13264

12731

12246

35.0

19756

18218

16720

15630

14772

14043

13405

12863

12370

35.2

20007

18442

16917

15808

14934

14193

13544

12995

12495

08.01.204

07-14-08

2.00

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

35.4

20256

18664

17113

15984

15096

14343

13684

13127

12619

35.6

20505

18886

17308

16161

15258

14492

13823

13258

12744

35.8

20753

19108

17504

16338

15419

14642

13963

13390

12868

36.0

21001

19330

17700

16515

15582

14792

14103

13522

12993

36.2

21250

19552

17897

16693

15745

14943

14244

13655

13119

36.4

21500

19776

18095

16872

15909

15095

14386

13789

13245

36.6

21751

20001

18295

17052

16075

15249

14529

13924

13373

36.8

22004

20227

18497

17235

16242

15404

14674

14060

13502

37.0

22258

20456

18700

17420

16412

15561

14820

14198

13632

37.2

22514

20686

18906

17606

16583

15719

14968

14337

13763

37.4

22771

20918

19113

17794

16756

15879

15117

14477

13895

37.6

23030

21152

19322

17984

16930

16040

15267

14618

14028

37.8

23290

21387

19533

18175

17106

16203

15418

14760

14162

38.0

23551

21623

19745

18368

17283

16366

15571

14903

14297

38.2

23814

21861

19958

18562

17461

16531

15724

15046

14432

38.4

24077

22100

20173

18757

17640

16697

15878

15191

14568

38.6

24341

22340

20389

18954

17820

16863

16032

15336

14704

38.8

24606

22580

20606

19152

18002

17031

16188

15482

14841

39.0

24872

22822

20824

19350

18184

17199

16344

15628

14978

39.2

25138

23065

21044

19550

18367

17367

16500

15774

15116

39.4

25406

23309

21263

19750

18550

17536

16657

15921

15254

39.6

25674

23553

21484

19951

18734

17706

16814

16068

15391

Original

07-14-08

08.01.205

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER TWO (WSTA 262.0) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

39.8

25943

23798

21705

20152

18918

17875

16971

16215

15529

40.0

26212

24044

21926

20353

19102

18045

17128

16362

15667

40.2

26483

24290

22148

20554

19286

18214

17285

16509

15805

40.4

26755

24536

22370

20756

19470

18384

17442

16656

15943

40.6

27027

24783

22592

20957

19654

18553

17599

16802

16080

40.8

27300

25031

22813

21158

19837

18722

17755

16949

16218

41.0

27574

25278

23035

21358

20020

18890

17911

17095

16355

41.2

27847

25525

23256

21559

20203

19059

18067

17241

16492

41.4

28120

25772

23477

21759

20386

19227

18223

17387

16630

41.6

28391

26018

23697

21959

20569

19396

18380

17534

16767

41.8

28661

26263

23918

22159

20752

19564

18536

17680

16905

42.0

28929

26506

24137

22359

20936

19733

18693

17827

17043

42.2

29193

26748

24357

22559

21119

19903

18851

17975

17181

42.4

29455

26988

24576

22760

21303

20073

19009

18123

17320

42.6

29713

27226

24794

22960

21488

20244

19168

18272

17460

42.8

29967

27462

25012

23161

21674

20416

19328

18422

17600

43.0

30217

27696

25229

23362

21860

20589

19488

18572

17742

43.2

30463

27928

25446

23564

22046

20762

19650

18723

17883

43.4

30707

28158

25663

23765

22233

20936

19812

18875

18026

43.6

30949

28387

25879

23967

22421

21110

19974

19027

18168

43.8

31189

28616

26095

24169

22608

21285

20137

19179

18311

08.01.206

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

12264

12852

13439

14004

14563

15118

15640

16094

16535

3.2

12424

13001

13579

14148

14711

15259

15773

16221

16657

3.4

12583

13150

13720

14293

14860

15400

15906

16348

16778

3.6

12743

13301

13862

14438

15008

15542

16038

16474

16899

3.8

12904

13452

14006

14584

15156

15683

16170

16600

17019

4.0

13064

13605

14152

14732

15304

15824

16302

16725

17138

4.2

13226

13759

14300

14880

15452

15965

16434

16850

17256

4.4

13387

13915

14451

15031

15601

16106

16566

16974

17374

4.6

13550

14072

14604

15182

15749

16247

16697

17097

17490

4.8

13713

14232

14761

15336

15898

16387

16828

17219

17605

5.0

13877

14394

14921

15491

16047

16527

16958

17341

17718

5.2

14042

14558

15083

15647

16196

16667

17089

17462

17831

5.4

14207

14723

15247

15804

16344

16808

17219

17583

17942

5.6

14373

14889

15413

15963

16493

16948

17350

17703

18052

5.8

14540

15057

15581

16122

16641

17088

17481

17822

18161

6.0

14707

15225

15749

16281

16789

17228

17612

17942

18269

6.2

14878

15395

15918

16440

16937

17368

17744

18061

18376

6.4

15042

15564

16088

16600

17084

17508

17877

18181

18482

6.6

15211

15734

16257

16758

17231

17649

18010

18300

18587

6.8

15380

15904

16426

16917

17378

17790

18144

18420

18691

7.0

15549

16074

16595

17075

17524

17931

18279

18540

18794

7.2

15720

16245

16763

17232

17670

18071

18414

18659

18897

Original

07-14-08

08.01.207

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.4

15891

16416

16932

17389

17815

18211

18548

18778

18999

7.6

16065

16587

17099

17546

17960

18351

18681

18897

19101

7.8

16240

16760

17267

17703

18106

18490

18814

19014

19202

8.0

16417

16933

17434

17860

18251

18629

18945

19131

19304

8.2

16596

17107

17602

18016

18396

18766

19073

19247

19405

8.4

16778

17282

17769

18173

18542

18902

19199

19361

19507

8.6

16962

17459

17936

18330

18688

19037

19323

19473

19609

8.8

17150

17636

18104

18487

18834

19170

19443

19584

19711

9.0

17340

17815

18271

18645

18980

19301

19560

19694

19813

9.2

17533

17995

18438

18802

19127

19431

19675

19801

19916

9.4

17727

18176

18605

18960

19273

19561

19787

19908

20019

9.6

17923

18357

18772

19117

19419

19689

19898

20014

20121

9.8

18121

18539

18938

19274

19565

19816

20008

20119

20224

10.0

18319

18721

19104

19430

19711

19943

20117

20223

20326

10.2

18518

18903

19270

19586

19855

20069

20226

20327

20427

10.4

18717

19085

19435

19741

20000

20195

20335

20431

20528

10.6

18916

19266

19599

19895

20143

20321

20444

20534

20629

10.8

19115

19447

19763

20048

20285

20446

20554

20638

20728

11.0

19313

19628

19927

20200

20426

20572

20665

20742

20827

11.2

19510

19808

20090

20352

20566

20697

20777

20846

20925

11.4

19707

19987

20253

20502

20705

20822

20889

20950

21023

11.6

19903

20167

20415

20652

20843

20946

21001

21054

21120

08.01.208

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.8

20098

20346

20578

20801

20979

21070

21114

21158

21217

12.0

20292

20525

20742

20950

21114

21193

21227

21263

21314

12.2

20486

20704

20906

21098

21248

21315

21340

21367

21411

12.4

20679

20883

21070

21246

21380

21436

21453

21472

21508

12.6

20870

21062

21235

21394

21510

21557

21565

21576

21604

12.8

21061

21241

21402

21541

21639

21676

21678

21681

21701

13.0

21251

21420

21568

21687

21767

21794

21789

21785

21799

13.2

21440

21598

21735

21834

21893

21911

21901

21890

21896

13.4

21628

21777

21902

21979

22018

22027

22012

21994

21994

13.6

21816

21954

22067

22124

22143

22143

22122

22099

22091

13.8

22004

22131

22232

22268

22267

22259

22233

22203

22189

14.0

22191

22307

22395

22411

22391

22374

22343

22307

22287

14.2

22377

22481

22557

22553

22515

22489

22453

22412

22385

14.4

22564

22654

22716

22694

22639

22604

22562

22516

22482

14.6

22751

22826

22872

22833

22763

22719

22672

22619

22580

14.8

22937

22996

23025

22971

22888

22835

22781

22723

22678

15.0

23124

23164

23175

23107

23014

22951

22890

22827

22775

15.2

23311

23330

23323

23243

23140

23068

22999

22930

22873

15.4

23497

23496

23468

23377

23266

23184

23107

23033

22970

15.6

23684

23660

23612

23510

23392

23301

23216

23136

23067

15.8

23870

23824

23755

23643

23518

23417

23325

23240

23165

16.0

24056

23987

23896

23775

23643

23534

23434

23343

23262

Original

07-14-08

08.01.209

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.2

24242

24149

24037

23906

23768

23650

23543

23446

23359

16.4

24427

24311

24178

24037

23893

23767

23652

23549

23455

16.6

24613

24473

24319

24167

24017

23883

23762

23653

23552

16.8

24797

24635

24460

24297

24139

23999

23872

23756

23649

17.0

24981

24796

24601

24427

24262

24114

23982

23860

23745

17.2

25164

24957

24743

24557

24383

24230

24092

23964

23842

17.4

25346

25118

24885

24686

24504

24345

24202

24068

23938

17.6

25526

25278

25027

24816

24624

24459

24312

24171

24035

17.8

25704

25437

25169

24945

24744

24573

24421

24275

24132

18.0

25880

25595

25311

25074

24864

24687

24530

24378

24228

18.2

26053

25751

25453

25204

24984

24801

24638

24481

24326

18.4

26224

25906

25595

25333

25104

24914

24746

24584

24423

18.6

26392

26059

25736

25462

25224

25027

24852

24686

24521

18.8

26556

26211

25876

25592

25345

25139

24958

24788

24619

19.0

26717

26361

26016

25721

25465

25251

25062

24889

24717

19.2

26877

26509

26155

25851

25586

25362

25166

24990

24815

19.4

27034

26656

26294

25980

25707

25473

25269

25091

24913

19.6

27190

26802

26431

26108

25828

25584

25372

25191

25011

19.8

27345

26947

26568

26237

25948

25695

25475

25291

25108

20.0

27500

27091

26704

26364

26069

25806

25577

25391

25205

20.2

27655

27235

26839

26491

26189

25916

25679

25490

25301

20.4

27811

27378

26973

26618

26308

26027

25782

25588

25396

08.01.210

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

20.6

27968

27522

27105

26743

26427

26137

25884

25686

25489

20.8

28127

27665

27236

26867

26546

26248

25987

25784

25582

21.0

28287

27808

27366

26991

26664

26358

26091

25882

25673

21.2

28447

27952

27495

27113

26781

26468

26194

25979

25763

FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

11882

12452

13022

13594

14165

14728

15258

15737

16202

3.2

12033

12601

13171

13741

14309

14868

15393

15867

16324

3.4

12183

12751

13321

13889

14454

15009

15529

15996

16447

3.6

12335

12901

13471

14037

14599

15150

15664

16125

16570

3.8

12488

13052

13621

14185

14744

15291

15800

16254

16692

4.0

12642

13204

13772

14335

14890

15433

15935

16382

16814

4.2

12797

13358

13924

14485

15038

15575

16070

16511

16935

4.4

12954

13512

14077

14636

15186

15717

16206

16639

17057

4.6

13113

13669

14232

14788

15335

15860

16341

16766

17177

4.8

13274

13826

14387

14942

15485

16003

16476

16894

17297

Original

07-14-08

08.01.211

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

5.0

13437

13986

14543

15096

15636

16147

16611

17021

17417

5.2

13601

14147

14701

15252

15788

16292

16747

17148

17536

5.4

13768

14310

14860

15409

15940

16436

16882

17274

17655

5.6

13936

14474

15020

15566

16094

16581

17017

17400

17772

5.8

14105

14640

15182

15724

16247

16726

17152

17526

17890

6.0

14277

14807

15344

15883

16401

16872

17288

17652

18006

6.2

14449

14975

15508

16043

16554

17017

17423

17777

18122

6.4

14623

15145

15673

16202

16708

17162

17559

17902

18237

6.6

14798

15317

15839

16363

16861

17307

17695

18028

18351

6.8

14975

15489

16007

16523

17014

17452

17831

18153

18464

7.0

15152

15663

16176

16684

17166

17596

17967

18278

18577

7.2

15330

15838

16345

16845

17318

17741

18103

18402

18689

7.4

15509

16014

16516

17007

17469

17885

18238

18526

18800

7.6

15690

16191

16687

17168

17620

18028

18374

18650

18910

7.8

15871

16368

16859

17330

17771

18171

18509

18772

19019

8.0

16052

16546

17031

17492

17922

18314

18643

18894

19128

8.2

16235

16724

17204

17654

18073

18456

18776

19015

19236

8.4

16418

16903

17376

17816

18224

18598

18908

19136

19343

8.6

16602

17082

17549

17978

18375

18739

19039

19254

19449

8.8

16787

17261

17722

18141

18525

18879

19169

19372

19555

9.0

16972

17440

17895

18304

18676

19019

19298

19489

19660

9.2

17158

17620

18068

18466

18827

19158

19425

19604

19764

08.01.212

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

9.4

17345

17800

18240

18629

18978

19297

19552

19718

19868

9.6

17534

17981

18413

18791

19128

19434

19677

19832

19971

9.8

17724

18162

18585

18953

19278

19571

19801

19944

20074

10.0

17916

18344

18758

19115

19428

19707

19924

20056

20177

10.2

18109

18527

18930

19277

19577

19843

20045

20167

20280

10.4

18305

18711

19102

19438

19726

19977

20166

20278

20382

10.6

18503

18895

19275

19598

19875

20111

20286

20388

20484

10.8

18704

19082

19447

19759

20022

20244

20405

20497

20587

11.0

18906

19269

19619

19918

20170

20376

20523

20607

20689

11.2

19110

19457

19791

20078

20316

20507

20640

20715

20792

11.4

19316

19645

19963

20236

20462

20637

20756

20824

20894

11.6

19522

19834

20134

20395

20607

20767

20872

20932

20996

11.8

19730

20024

20306

20552

20752

20896

20988

21040

21098

12.0

19937

20213

20477

20710

20896

21025

21103

21148

21200

12.2

20144

20402

20649

20866

21039

21152

21218

21255

21302

12.4

20350

20591

20820

21023

21181

21280

21332

21362

21403

12.6

20555

20780

20991

21179

21323

21407

21447

21470

21504

12.8

20759

20967

21162

21334

21463

21533

21561

21577

21605

13.0

20962

21154

21333

21489

21603

21659

21676

21684

21706

13.2

21164

21341

21503

21644

21742

21784

21790

21790

21806

13.4

21365

21526

21673

21797

21881

21909

21904

21897

21906

13.6

21564

21711

21842

21950

22018

22033

22018

22004

22006

Original

07-14-08

08.01.213

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

13.8

21763

21896

22011

22102

22154

22156

22132

22111

22106

14.0

21961

22079

22179

22253

22289

22279

22246

22217

22206

14.2

22159

22262

22346

22403

22423

22402

22360

22324

22305

14.4

22356

22444

22512

22552

22556

22523

22474

22431

22405

14.6

22553

22625

22678

22700

22688

22644

22587

22537

22505

14.8

22750

22805

22842

22845

22819

22764

22700

22644

22604

15.0

22946

22985

23004

22991

22948

22884

22813

22751

22704

15.2

23142

23164

23166

23135

23077

23003

22926

22857

22804

15.4

23337

23342

23327

23278

23205

23122

23038

22964

22904

15.6

23532

23519

23486

23419

23332

23240

23151

23071

23004

15.8

23727

23695

23644

23560

23459

23358

23263

23177

23104

16.0

23921

23870

23801

23700

23585

23476

23375

23284

23204

16.2

24114

24044

23957

23840

23711

23594

23487

23390

23304

16.4

24306

24217

24112

23978

23837

23712

23600

23496

23403

16.6

24498

24389

24265

24116

23963

23830

23712

23603

23503

16.8

24689

24560

24418

24254

24089

23948

23824

23709

23602

17.0

24879

24729

24569

24391

24216

24067

23936

23815

23702

17.2

25068

24898

24720

24528

24342

24185

24048

23921

23801

17.4

25256

25066

24869

24664

24469

24304

24160

24027

23900

17.6

25444

25233

25017

24799

24595

24423

24272

24133

24000

17.8

25630

25399

25165

24934

24722

24541

24384

24239

24099

18.0

25816

25564

25312

25069

24848

24660

24495

24345

24198

08.01.214

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

18.2

26002

25729

25459

25204

24974

24778

24607

24450

24297

18.4

26186

25893

25605

25338

25099

24896

24718

24556

24397

18.6

26370

26056

25750

25471

25225

25013

24829

24661

24496

18.8

26553

26219

25895

25604

25349

25130

24939

24766

24595

19.0

26735

26382

26040

25737

25474

25247

25050

24871

24695

19.2

26916

26544

26184

25869

25598

25364

25160

24976

24794

19.4

27096

26705

26328

26001

25721

25480

25269

25080

24893

19.6

27274

26864

26471

26133

25845

25595

25378

25184

24992

19.8

27451

27023

26614

26264

25968

25710

25487

25288

25091

20.0

27626

27181

25756

26396

26090

25825

25596

25392

25190

20.2

27798

27337

26898

26526

26212

25940

25704

25495

25288

20.4

27968

27491

27039

26657

26334

26054

25811

25598

25386

20.6

28136

27644

27179

26787

26456

26168

25919

25701

25484

20.8

28301

27794

27319

26917

26578

26282

26026

25803

25581

21.0

28464

27944

27458

27047

26699

26395

26132

25905

25678

21.2

28624

28091

27596

27176

26820

26508

26238

26006

25774

Original

07-14-08

08.01.215

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

11488

12041

12597

13179

13757

14325

14867

15373

15865

3.2

11632

12191

12755

13327

13897

14465

15006

15505

15989

3.4

11777

12342

12912

13476

14037

14605

15145

15638

16114

3.6

11923

12493

13068

13625

14178

14746

15284

15770

16239

3.8

12070

12645

13225

13774

14321

14887

15423

15902

16364

4.0

12219

12798

13381

13924

14464

15029

15562

16035

16489

4.2

12370

12951

13537

14075

14610

15172

15701

16167

16614

4.4

12524

13106

13692

14226

14756

15315

15840

16299

16739

4.6

12680

13261

13847

14379

14905

15460

15979

16432

16864

4.8

12839

13418

14001

14532

15056

15605

16118

16564

16990

5.0

13001

13576

14155

14686

15209

15752

16257

16696

17116

5.2

13165

13735

14308

14841

15363

15899

16396

16828

17241

5.4

13332

13895

14463

14996

15519

16047

16535

16960

17367

5.6

13501

14057

14617

15153

15676

16195

16674

17092

17492

5.8

13673

14221

14773

15311

15833

16343

16813

17224

17617

6.0

13846

14387

14930

15469

15991

16492

16951

17355

17742

6.2

14022

14554

15088

15628

16150

16641

17089

17486

17866

6.4

14200

14723

15248

15788

16308

16790

17227

17617

17990

6.6

14379

14894

15411

15949

16467

16938

17365

17748

18113

6.8

14560

15067

15575

16111

16624

17086

17502

17878

18235

7.0

14742

15241

15742

16274

16782

17234

17640

18007

18357

7.2

14925

15417

15911

16437

16938

17381

17777

18136

18477

08.01.216

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.4

15110

15595

16082

16601

17095

17529

17914

18265

18597

7.6

15294

15774

16254

16765

17251

17676

18051

18393

18715

7.8

15480

15953

16428

16931

17407

17823

18188

18521

18832

8.0

15665

16134

16603

17096

17562

17970

18326

18648

18948

8.2

15849

16314

16779

17262

17718

18117

18464

18775

19063

8.4

16034

16495

16956

17428

17873

18264

18603

18901

19176

8.6

16217

16676

17134

17595

18028

18412

18742

19027

19288

8.8

16400

16857

17312

17762

18183

18559

18882

19152

19398

9.0

16582

17038

17491

17929

18337

18707

19022

19276

19507

9.2

16764

17219

17670

18096

18492

18855

19163

19400

19614

9.4

16947

17401

17849

18264

18647

19002

19303

19523

19721

9.6

17131

17583

18028

18431

18801

19149

19443

19646

19826

9.8

17316

17766

18208

18599

18955

19296

19581

19767

19932

10.0

17504

17950

18388

18767

19110

19441

19719

19888

20037

10.2

17694

18136

18568

18934

19264

19586

19854

20008

20141

10.4

17887

18323

18748

19102

19418

19730

19988

20127

20247

10.6

18084

18511

18928

19269

19573

19873

20119

20244

20352

10.8

18286

18702

19108

19437

19727

20014

20248

20361

20458

11.0

18491

18894

19288

19604

19881

20154

20374

20477

20564

11.2

18699

19088

19468

19771

20035

20292

20498

20591

20671

11.4

18910

19282

19647

19938

20189

20430

20620

20705

20778

11.6

19123

19478

19826

20105

20343

20567

20741

20818

20885

Original

07-14-08

08.01.217

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.8

19338

19674

20005

20271

20497

20703

20860

20931

20992

12.0

19554

19871

20183

20437

20651

20839

20978

21043

21099

12.2

19771

20068

20360

20602

20805

20974

21096

21154

21205

12.4

19988

20264

20537

20767

20958

21109

21213

21264

21311

12.6

20204

20460

20713

20932

21112

21244

21330

21375

21416

12.8

20420

20655

20888

21096

21265

21378

21447

21485

21521

13.0

20635

20850

21063

21260

21419

21512

21565

21594

21624

13.2

20849

21044

21237

21423

21571

21646

21682

21703

21727

13.4

21062

21238

21411

21585

21723

21780

21800

21813

21830

13.6

21275

21431

21584

21747

21873

21913

21917

21922

21932

13.8

21486

21623

21758

21907

22022

22045

22035

22031

22034

14.0

21697

21816

21931

22067

22169

22176

22152

22139

22136

14.2

21907

22008

22105

22227

22314

22306

22270

22248

22238

14.4

22116

22200

22280

22385

22458

22436

22387

22357

22339

14.6

22324

22392

22455

22542

22598

22563

22505

22466

22441

14.8

22532

22584

22631

22698

22736

22690

22622

22575

22542

15.0

22739

22776

22808

22854

22872

22815

22740

22684

22644

15.2

22945

22967

22984

23008

23005

22939

22857

22794

22746

15.4

23150

23158

23161

23161

23137

23062

22974

22903

22847

15.6

23354

23348

23337

23314

23268

23184

23090

23012

22949

15.8

23558

23537

23512

23465

23398

23306

23207

23122

23051

16.0

23761

23725

23686

23616

23527

23427

23323

23231

23153

08.01.218

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.2

23962

23912

23858

23765

23657

23548

23439

23340

23255

16.4

24163

24098

24029

23914

23786

23669

23554

23449

23357

16.6

24363

24281

24197

24062

23916

23790

23669

23558

23459

16.8

24562

24464

24363

24209

24047

23911

23784

23666

23561

17.0

24760

24644

24527

24355

24178

24033

23898

23774

23662

17.2

24958

24823

24688

24500

24310

24154

24012

23882

23764

17.4

25156

25001

24847

24644

24443

24276

24126

23990

23866

17.6

25353

25178

25005

24788

24575

24398

24240

24098

23967

17.8

25550

25354

25160

24930

24708

24520

24353

24206

24068

18.0

25748

25530

25315

25072

24840

24642

24467

24313

24169

18.2

25947

25705

25468

25212

24972

24764

24581

24421

24270

18.4

26146

25880

25620

25352

25103

24885

24695

24529

24370

18.6

26346

26054

25770

25490

25234

25007

24809

24636

24471

18.8

26547

26229

25921

25628

25363

25128

24924

24744

24571

19.0

26749

26404

26070

25765

25491

25249

25039

24851

24671

19.2

26951

26578

26219

25901

25619

25370

25154

24959

24770

19.4

27151

26752

26368

26036

25745

25490

25269

25066

24870

19.6

27351

26925

26516

26171

25872

25610

25383

25174

24970

19.8

27548

27096

26664

26306

25997

25730

25498

25281

25069

20.0

27742

27266

26812

26441

26123

25849

25612

25388

25169

20.2

27932

27434

26960

26575

26248

25968

25725

25494

25269

20.4

28118

27600

27109

26710

26373

26086

25837

25601

25369

Original

07-14-08

08.01.219

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

20.6

28299

27764

27257

26846

26497

26204

25949

25707

25470

20.8

28475

27925

27406

26981

26622

26321

26059

25813

25571

21.0

28645

28084

27555

27117

26747

26437

26168

25918

25672

21.2

28812

28240

27704

27253

26872

26553

26277

26023

25773

FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

11053

11621

12196

12781

13361

13922

14465

14994

15508

3.2

11208

11772

12343

12925

13503

14065

14606

15129

15635

3.4

11364

11924

12490

13070

13647

14207

14746

15263

15763

3.6

11520

12075

12638

13215

13790

14350

14887

15398

15891

3.8

11676

12228

12788

13361

13934

14494

15028

15533

16019

4.0

11833

12382

12938

13508

14079

14637

15169

15668

16146

4.2

11990

12536

13089

13657

14225

14781

15310

15803

16275

4.4

12148

12692

13243

13806

14371

14925

15451

15938

16403

4.6

12306

12849

13398

13958

14519

15070

15592

16073

16531

4.8

12466

13007

13554

14111

14667

15216

15734

16209

16660

5.0

12626

13166

13713

14265

14817

15362

15876

16345

16788

5.2

12787

13327

13873

14421

14968

15508

16018

16481

16917

08.01.220

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

5.4

12950

13490

14035

14579

15119

15656

16160

16617

17046

5.6

13113

13653

14198

14737

15272

15803

16303

16752

17175

5.8

13279

13818

14362

14897

15426

15951

16445

16888

17303

6.0

13446

13985

14527

15058

15581

16100

16587

17024

17432

6.2

13616

14152

14693

15219

15737

16249

16729

17159

17560

6.4

13787

14321

14860

15382

15894

16399

16871

17295

17688

6.6

13961

14491

15027

15545

16051

16549

17013

17430

17816

6.8

14137

14663

15194

15709

16210

16699

17155

17564

17943

7.0

14315

14836

15362

15873

16370

16850

17297

17699

18070

7.2

14496

15010

15530

16038

16530

17002

17438

17833

18196

7.4

14678

15185

15699

16203

16691

17153

17580

17967

18322

7.6

14862

15362

15868

16369

16852

17305

17721

18100

18447

7.8

15018

15540

16039

13536

17014

17457

17863

18233

18572

8.0

15235

15719

16211

16703

17175

17610

18005

18366

18695

8.2

15424

15899

16383

16870

17337

17762

18147

18498

18818

8.4

15613

16081

16557

17038

17499

17915

18289

18631

18940

8.6

15804

16264

16732

17207

17660

18068

18432

18762

19061

8.8

15995

16448

16909

17376

17821

18220

18575

18894

19181

9.0

16187

16633

17087

17546

17982

18373

18718

19025

19300

9.2

16380

16819

17266

17716

18142

18525

18862

19156

19418

9.4

16574

17007

17447

17886

18303

18677

19005

19286

19535

9.6

16768

17195

17628

18057

18463

18830

19148

19416

19651

Original

07-14-08

08.01.221

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

9.8

16964

17385

17811

18229

18623

18981

19291

19545

19766

10.0

17160

17575

17994

18400

18783

19133

19433

19673

19880

10.2

17358

17766

18178

18572

18942

19284

19575

19801

19993

10.4

17556

17958

18362

18745

19102

19434

19715

19927

20106

10.6

17756

18150

18547

18918

19262

19584

19855

20053

20217

10.8

17957

18343

18733

19091

19422

19733

19993

20177

20328

11.0

18159

18537

18918

19264

19582

19882

20130

20301

20438

11.2

18363

18732

19104

19438

19742

20030

20267

20423

20548

11.4

18568

18928

19290

19611

19902

20178

20401

20544

20656

11.6

18774

19124

19476

19785

20063

20324

20535

20665

20765

11.8

18983

19321

19662

19958

20222

20471

20668

20785

20873

12.0

19193

19518

19848

20132

20382

20616

20799

20903

20980

12.2

19405

19717

20034

20305

20542

20761

20929

21021

21088

12.4

19618

19917

20220

20478

20702

20905

21058

21139

21195

12.6

19834

20117

20405

20650

20861

21048

21186

21255

21302

12.8

20052

20318

20590

20822

21020

21191

21313

21371

21409

13.0

20272

20520

20774

20994

21179

21332

21439

21486

21516

13.2

20493

20723

20959

21165

21337

21474

21564

21601

21623

13.4

20716

20926

21143

21336

21495

21614

21688

21715

21730

13.6

20939

21129

21326

21506

21652

21754

21811

21829

21837

13.8

21163

21332

21510

21675

21808

21892

21933

21942

21944

14.0

21387

21536

21693

21844

21964

22031

22055

22055

22050

08.01.222

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

14.2

21610

21739

21876

22013

22119

22168

22177

22167

22156

14.4

21834

21942

22059

22181

22273

22305

22298

22280

22262

14.6

22056

22144

22242

22349

22426

22441

22419

22392

22367

14.8

22277

22346

22425

22515

22578

22576

22540

22503

22473

15.0

22498

22547

22608

22682

22728

22710

22660

22615

22577

15.2

22717

22748

22790

22847

22877

22844

22780

22726

22682

15.4

22935

22948

22972

23012

23026

22977

22901

22838

22786

15.6

23152

23147

23154

23176

23172

23109

23021

22949

22890

15.8

23368

23346

23335

23339

23318

23240

23140

23060

22994

16.0

23583

23544

23516

23500

23462

23370

23260

23172

23098

16.2

23797

23741

23696

23661

23605

23500

23379

23283

23202

16.4

24011

23937

23875

23820

23747

23628

23499

23394

23306

16.6

24223

24132

24053

23979

23886

23756

23617

23505

23410

16.8

24435

24327

24230

24135

24025

23882

23736

23616

23514

17.0

24647

24521

24406

24291

24162

24008

23854

23727

23618

17.2

24857

24714

24581

24445

24298

24133

23973

23839

23722

17.4

25067

24906

24754

24598

24433

24258

24091

23950

23825

17.6

25277

25097

24927

24750

24568

24382

24208

24061

23929

17.8

25486

25287

25098

24901

24701

24506

24326

24172

24033

18.0

25694

25477

25268

25051

24834

24630

24444

24283

24137

18.2

25902

25665

25436

25199

24967

24753

24561

24394

24240

18.4

26110

25852

25603

25347

25100

24877

24678

24504

24344

Original

07-14-08

08.01.223

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

18.6

26318

26039

25769

25494

25233

25000

24795

24615

24447

18.8

26525

26224

25932

25641

25366

25124

24912

24725

24550

19.0

26733

26409

26095

25786

25499

25249

25029

24835

24653

19.2

26939

26592

26256

25931

25632

25373

25146

24945

24756

19.4

27145

26774

26415

26075

25765

25497

25263

25055

24858

19.6

27350

26955

26574

26218

25898

25621

25380

25165

24961

19.8

27555

27135

26731

26360

26031

25745

25496

25274

25063

20.0

27758

27314

26888

26503

26164

25869

25612

25384

25165

20.2

27959

27492

27043

26644

26296

25993

25728

25493

25268

20.4

28160

27669

27198

26785

26427

26116

25844

25602

25370

20.6

28358

27845

27353

26926

26559

26239

25959

25711

25472

20.8

28555

28019

27507

27066

26689

26361

26075

25820

25575

21.0

28750

28192

23660

27205

26819

26483

26189

25928

25677

21.2

28943

28364

27813

27345

26948

26604

26304

26037

25779

FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE =0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

10624

11213

11806

12391

12968

13522

14065

14609

15139

3.2

10788

11361

11941

12532

13115

13667

14206

14745

15270

08.01.224

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE =0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.4

10951

11511

12077

12673

13261

13812

14347

14880

15400

3.6

11115

11661

12216

12815

13408

13957

14488

15016

15530

3.8

11278

11812

12357

12959

13554

14101

14629

15152

15660

4.0

11440

11965

12500

13104

13701

14246

14771

15289

15790

4.2

11603

12119

12647

13250

13847

14391

14914

15425

15920

4.4

11764

12275

12798

13398

13993

14537

15056

15562

16050

4.6

11926

12432

12952

13548

14139

14682

15199

15699

16181

4.8

12086

12592

13111

13700

14285

14827

15343

15837

16311

5.0

12246

12754

13274

13854

14431

14973

15487

15974

16441

5.2

12407

12918

13441

14010

14578

15119

15632

16113

16572

5.4

12567

13083

13610

14168

14725

15265

15777

16251

16702

5.6

12729

13250

13781

14328

14873

15412

15922

16390

16833

5.8

12891

13417

13953

14488

15022

15559

16067

16528

16963

6.0

13054

13586

14127

14650

15173

15707

16213

16667

17094

6.2

13219

13756

14300

14813

15325

15856

16358

16806

17225

6.4

13386

13927

14474

14977

15480

16006

16504

16945

17356

6.6

13556

14098

14646

15142

15636

16157

16650

17084

17487

6.8

13727

14269

14816

15307

15795

16310

16795

17222

17618

7.0

13902

14441

14985

15473

15956

16463

16940

17361

17749

7.2

14078

14613

15154

15639

16119

16617

17086

17500

17880

7.4

14258

14787

15321

15806

16283

16771

17231

17638

18011

7.6

14440

14962

15489

15974

16448

16927

17376

17776

18142

Original

07-14-08

08.01.225

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE =0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.8

14625

15138

15657

16142

16615

17083

17521

17914

18272

8.0

14813

15316

15826

16311

16782

17239

17666

18052

18403

8.2

15004

15496

15995

16480

16949

17395

17811

18190

18533

8.4

15197

15677

16166

16650

17116

17551

17956

18327

18664

8.6

15393

15862

16339

16820

17283

17707

18101

18464

18793

8.8

15592

16048

16514

16991

17449

17863

18245

18601

18923

9.0

15794

16237

16691

17162

17615

18019

18390

18738

19052

9.2

15997

16428

16870

17334

17780

18174

18534

18874

19180

9.4

16202

16621

17051

17507

17945

18330

18679

19011

19307

9.6

16408

16815

17233

17680

18109

18485

18824

19146

19434

9.8

16614

17010

17417

17854

18273

18640

18969

19281

19559

10.0

16821

17205

17602

18029

18437

18796

19115

19416

19682

10.2

17027

17402

17789

18204

18601

18951

19261

19550

19805

10.4

17232

17598

17977

18379

18765

19107

19407

19683

19925

10.6

17436

17795

18166

18556

18930

19263

19554

19816

20044

10.8

17638

17991

18356

18733

19094

19419

19702

19948

20160

11.0

17839

18187

18546

18911

19258

19575

19850

20080

20275

11.2

18039

18383

18737

19089

19423

19732

19998

20210

20388

11.4

18240

18579

18929

19267

19587

19888

20145

20340

20500

11.6

18441

18776

19121

19446

19752

20044

20292

20469

20611

11.8

18643

18974

19314

19625

19917

20199

20439

20597

20722

12.0

18848

19173

19507

19805

20081

20354

20583

20725

20832

08.01.226

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE =0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

12.2

19054

19373

19701

19984

20246

20508

20727

20851

20942

12.4

19264

19575

19894

20163

20410

20661

20869

20977

21052

12.6

19478

19779

20088

20342

20575

20813

21008

21102

21162

12.8

19697

19984

20281

20521

20739

20964

21146

21225

21274

13.0

19919

20192

20474

20700

20903

21114

21281

21348

21385

13.2

20144

20401

20668

20879

21067

21262

21414

21470

21498

13.4

20372

20611

20860

21057

21231

21410

21546

21592

21610

13.6

20603

20822

22105

21235

21395

21557

21676

21712

21722

13.8

20835

21033

21245

21413

21560

21703

21804

21832

21835

14.0

21068

21245

21436

21591

21724

21849

21932

21950

21947

14.2

21303

21457

21627

21768

21889

21994

22058

22068

22059

14.4

21537

21669

21817

21945

22054

22139

22184

22186

22171

14.6

21771

21879

22006

22122

22219

22284

22309

22303

22281

14.8

22004

22090

22194

22299

22385

22428

22434

22419

22391

15.0

22236

22299

22381

22476

22551

22573

22559

22534

22501

15.2

22468

22507

22568

22651

22717

22717

22683

22649

22609

15.4

22698

22715

22754

22827

22881

22860

22807

22764

22718

15.6

22928

22923

22940

23001

23045

23003

22931

22878

22825

15.8

23157

23130

23127

23175

23207

23145

23055

22992

22933

16.0

23385

23337

23313

23348

23367

23285

23179

23106

23040

16.2

23613

23544

23499

23519

23524

23425

23303

23220

23146

16.4

23840

23750

23686

23689

23679

23563

23426

23334

23253

Original

07-14-08

08.01.227

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE =0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.6

24066

23957

23874

23858

23830

23699

23550

23448

23359

16.8

24292

24164

24062

24026

23978

23834

23674

23563

23466

17.0

24517

24371

24251

24192

24123

23967

23798

23677

23572

17.2

24741

24578

24440

24357

24265

24098

23922

23792

23679

17.4

24965

24784

24629

24520

24405

24228

24046

23907

23786

17.6

25187

24990

24818

24682

24543

24358

24170

24022

23892

17.8

25408

25195

25005

24844

24680

24486

24293

24136

23999

18.0

25628

25398

25192

25004

24817

24614

24416

24251

24105

18.2

25846

25600

25377

25163

24953

24742

24538

24366

24212

18.4

26063

25801

25561

25322

25089

24869

24660

24480

24318

18.6

26278

25999

25742

25479

25226

24996

24781

24594

24425

18.8

26492

26196

25921

25636

25364

25124

24902

24707

24531

19.0

26704

26390

26098

25793

25503

25251

25021

24821

24638

19.2

26915

26584

26272

25948

25643

25379

25140

24934

24744

19.4

27125

26775

26444

26103

25783

25507

25259

25046

24850

19.6

27335

26966

26615

26256

25923

25635

25378

25159

24956

19.8

27546

27155

26783

26409

26064

25763

25496

25271

25062

20.0

27757

27344

26949

26560

26204

25891

25614

25383

25167

20.2

27970

27532

27114

26710

26344

26019

25733

25495

25273

20.4

28183

27720

27276

26858

26483

26147

25851

25607

25377

20.6

28399

27908

27438

27006

26621

26274

25971

25719

25482

20.8

28617

28096

27597

27151

26758

26402

26090

25831

25586

08.01.228

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE =0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

21.0

28837

28284

27755

27296

26894

26529

26210

25943

25689

21.2

29056

28471

27912

27439

27029

26656

26330

26055

25793

FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

10242

10831

11424

11996

12559

13125

13684

14229

14759

3.2

10388

10974

11565

12141

12706

13268

13821

14364

14892

3.4

10536

11118

11708

12286

12853

13411

13960

14499

15024

3.6

10685

11263

11851

12432

13001

13555

14098

14635

15157

3.8

10835

11410

11996

12578

13148

13699

14237

14770

15290

4.0

10988

11559

12141

12725

13296

13843

14377

14907

15422

4.2

11143

11709

12289

12872

13444

13988

14518

15043

15555

4.4

11301

11862

12437

13020

13592

14134

14659

15180

15687

4.6

11462

12018

12588

13169

13740

14280

14802

15318

15820

4.8

11625

12177

12741

13320

13889

14427

14945

15456

15952

5.0

11793

12338

12896

13471

14039

14575

15090

15595

16085

5.2

11963

12501

13052

13623

14189

14724

15236

15735

16217

5.4

12135

12667

13211

13777

14339

14873

15382

15875

16350

Original

07-14-08

08.01.229

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

5.6

12310

12835

13372

13932

14491

15023

15529

16015

16482

5.8

12485

13004

13534

14088

14643

15173

15677

16156

16615

6.0

12662

13175

13699

14246

14796

15324

15825

16298

16748

6.2

12839

13347

13865

14406

14950

15476

15974

16439

16881

6.4

13017

13520

14033

14567

15105

15628

16122

16581

17015

6.6

13194

13694

14203

14730

15261

15780

16271

16723

17148

6.8

13371

13869

14374

14895

15418

15933

16419

16865

17282

7.0

13548

14044

14547

15061

15577

16086

16568

17007

17416

7.2

13725

14219

14722

15229

15737

16240

16716

17149

17550

7.4

13903

14396

14897

15398

15898

16394

16865

17291

17685

7.6

14082

14574

15074

15568

16060

16549

17013

17433

17819

7.8

14263

14753

15252

15740

16223

16704

17162

17575

17954

8.0

14445

14933

15430

15912

16386

16860

17310

17717

18088

8.2

14630

15115

15609

16085

16551

17016

17458

17859

18223

8.4

14818

15298

15789

16259

16717

17173

17607

18001

18357

8.6

15009

15483

15969

16433

16884

17330

17755

18142

18492

8.8

15203

15670

16149

16607

17051

17488

17903

18284

18626

9.0

15401

15859

16329

16781

17220

17647

18052

18425

18760

9.2

15602

16050

16510

16956

17389

17806

18201

18566

18894

9.4

15805

16242

16691

17132

17558

17966

18349

18707

19027

9.6

16011

16436

16873

17307

17728

18125

18498

18847

19160

9.8

16218

16631

17056

17484

17898

18286

14647

18987

19292

08.01.230

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

10.0

16428

16827

17240

17661

18069

18446

18797

19127

19423

10.2

16638

17025

17425

17838

18239

18607

18947

19267

19553

10.4

16849

17223

17612

18016

18410

18768

19097

19406

19682

10.6

17061

17423

17799

18195

18580

18929

19247

19545

19810

10.8

17272

17623

17989

18375

18751

19090

19398

19684

19936

11.0

17485

17824

18180

18555

18921

19251

19549

19822

20062

11.2

17697

18027

18372

18736

19091

19413

19701

19960

20186

11.4

17910

18230

18565

18917

19261

19574

19852

20098

20308

11.6

18124

18434

18760

19100

19431

19735

20003

20235

20430

11.8

18339

18638

18956

19282

19601

18896

20154

20371

20551

12.0

18554

18844

19152

19465

19771

20056

20305

20506

20671

12.2

18771

19051

19349

19649

19941

20217

20455

20641

20790

12.4

18989

19259

19547

19833

20111

20376

20604

20776

20909

12.6

19208

19467

19746

20017

20281

20536

20753

20909

21026

12.8

19429

19677

19945

20202

20451

20695

20901

21041

21143

13.0

19651

19888

20144

20387

20622

20853

21047

21173

21260

13.2

19875

20100

20343

20571

20792

21011

21193

21304

21376

13.4

20100

20312

20543

20757

20962

21169

21337

21433

21492

13.6

20327

20525

20743

20942

21133

21326

21480

21562

21607

13.8

20556

20739

20943

21127

21304

21482

21622

21690

21722

14.0

20786

20954

21143

21312

21474

21637

21763

21817

21837

14.2

21017

21169

21342

21497

21645

21792

21903

21944

21951

Original

07-14-08

08.01.231

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

14.4

21250

21385

21541

21682

21816

21947

22041

22069

22065

14.6

21485

21601

21740

21867

21987

22100

22177

22193

22179

14.8

21722

21818

21939

22052

22158

22253

22313

22316

22293

15.0

21959

22035

22137

22237

22330

22406

22446

22438

22407

15.2

22198

22253

22334

22421

22500

22557

22579

22560

22521

15.4

22438

22471

22532

22605

22671

22708

22711

22681

22634

15.6

22678

22689

22729

22788

22841

22858

22842

22801

22748

15.8

22919

22907

22926

22971

23010

23007

22972

22920

22860

16.0

23160

23125

23122

23153

23178

23155

23101

23039

22973

16.2

23401

23343

23319

23335

23346

23302

23230

23158

23085

16.4

23642

23561

23515

23515

23511

23449

23358

23276

23197

16.6

23883

23778

23711

23695

23676

23594

23487

23394

23308

16.8

24123

23996

23907

23875

23839

23739

23615

23512

23418

17.0

24362

24213

24104

24053

24000

23883

23743

23629

23528

17.2

24600

24430

24300

24230

24160

24025

23872

23747

23638

17.4

24837

24646

24495

24406

24318

24167

24000

23864

23747

17.6

25073

24862

24691

24581

24474

24308

24127

23981

23856

17.8

25308

25077

24885

24755

24629

24448

24255

24099

23965

18.0

25542

25291

25080

24928

24783

24586

24382

24216

24074

18.2

25775

25505

25274

25100

24934

24724

24509

24333

24182

18.4

26006

25717

25467

25271

25085

24860

24635

24450

24291

18.6

26235

25928

25659

25440

25233

24995

24761

24567

24400

08.01.232

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

18.8

26463

26138

25851

25609

25381

25130

24887

24685

24508

19.0

26689

26348

26041

25776

25526

25263

25012

24802

24617

19.2

26914

26555

26230

25941

25671

25395

25137

24919

24726

19.4

27139

26762

26418

26106

25815

25527

25261

25036

24835

19.6

27362

26968

26605

26269

25957

25658

25385

25154

24944

19.8

27586

27173

26790

26431

26099

25788

25509

25270

25053

20.0

27809

27377

26973

26592

26241

25919

25633

25387

25162

20.2

28032

27580

27155

26751

26382

26049

25756

25504

25270

20.4

28256

27781

27334

26909

26523

26179

25879

25620

25379

20.6

28480

27982

27511

27066

26664

26310

26002

25736

25487

20.8

28705

28182

27686

27221

26805

26440

26125

25851

25594

21.0

28930

28381

27859

27375

26946

26571

26247

25966

25701

21.2

29155

28579

28030

27528

27087

26702

26370

26081

25808

FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE =1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

3.0

Original

9876

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

10458

11044

11598

12151

12734

13309

13851

14378

07-14-08

08.01.233

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE =1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.2

10006

10599

11195

11747

12297

12873

13443

13986

14513

3.4

10138

10740

11345

11897

12444

13014

13577

14121

14647

3.6

10273

10882

11495

12046

12591

13154

13713

14256

14782

3.8

10412

11026

11644

12196

12739

13296

13849

14392

14917

4.0

10554

11172

11793

12345

12887

13439

13986

14528

15051

4.2

10701

11320

11942

12494

13037

13583

14124

14664

15186

4.4

10854

11470

12090

12644

13187

13729

14264

14802

15320

4.6

11014

11623

12237

12793

13339

13876

14405

14939

15455

4.8

11179

11779

12383

12943

13491

14024

14549

15078

15589

5.0

11351

11938

12529

13092

13645

14174

14693

15217

15723

5.2

11528

12099

12676

13243

13800

14326

14839

15357

15857

5.4

11709

12263

12824

13393

13955

14478

14987

15498

15992

5.6

11893

12429

12973

13545

14111

14632

15135

15639

16126

5.8

12080

12598

13124

13699

14268

14786

15285

15781

16261

6.0

12267

12768

13279

13853

14424

14940

15435

15923

16395

6.2

12455

12941

13437

14010

14581

15095

15585

16066

16530

6.4

12643

13115

13599

14169

14738

15249

15736

16209

16665

6.6

12828

13291

13765

14330

14894

15404

15888

16353

16801

6.8

13012

13468

13937

14493

15050

15557

16039

16497

16937

7.0

13193

13646

14113

14659

15206

15711

16190

16642

17073

7.2

13373

13826

14293

14826

15361

15864

16341

16787

17209

7.4

13552

14007

14476

14996

15518

16018

16493

16932

17346

08.01.234

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE =1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.6

13731

14189

14662

15168

15675

16172

16644

17077

17483

7.8

13911

14373

14849

15341

15833

16326

16795

17222

17620

8.0

14091

14557

15037

15515

15993

16481

16947

17368

17757

8.2

14273

14742

15226

15690

16154

16637

17098

17513

17894

8.4

14456

14928

15414

15866

16317

16794

17250

17659

18032

8.6

14643

15115

15601

16043

16483

16952

17401

17804

18170

8.8

14833

15303

15786

16220

16651

17111

17553

17949

18307

9.0

15026

15492

15970

16397

16822

17272

17705

18094

18445

9.2

15222

15682

16153

16575

16994

17434

17857

18239

18583

9.4

15421

15873

16335

16754

17168

17597

18008

18383

18720

9.6

15624

16065

16517

16933

17343

17760

18161

18528

18858

9.8

15830

16259

16699

17112

17519

17925

18313

18672

18995

10.0

16038

16455

16882

17292

17696

18089

18465

18816

19132

10.2

16250

16653

17065

17472

17873

18254

18617

18960

19269

10.4

16465

16853

17250

17653

18050

18419

18770

19105

19406

10.6

16684

17055

17437

17835

18226

18584

18923

19249

19542

10.8

16905

17259

17626

18017

18402

18749

19076

19393

19678

11.0

17128

17466

17817

18199

18577

18913

19229

19537

19813

11.2

17354

17674

18010

18382

18751

19078

19382

19681

19947

11.4

17581

17885

18205

18566

18926

19242

19536

19824

20081

11.6

17810

18096

18402

18751

19100

19406

19690

19968

20213

11.8

18039

18309

18600

18936

19273

19571

19844

20111

20345

Original

07-14-08

08.01.235

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE =1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

12.0

18269

18523

18799

19122

19447

19735

19999

20254

20475

12.2

18498

18737

19000

19308

19621

19900

20154

20396

20604

12.4

18726

18951

19202

19495

19795

20065

20310

20537

20731

12.6

18953

19166

19405

19683

19969

20231

20466

20679

20856

12.8

19179

19380

19609

19872

20143

20397

20623

20819

20980

13.0

19403

19595

19813

20061

20318

20563

20780

20959

21101

13.2

19627

19809

20019

20251

20494

20729

20937

21098

21222

13.4

19851

20025

20224

20441

20669

20895

21094

21236

21341

13.6

20075

20240

20431

20632

20845

21061

21250

21373

21460

13.8

20300

20457

20638

20823

21021

21226

21405

21510

21578

14.0

20527

20674

20845

21015

21196

21391

21559

21646

21696

14.2

20756

20892

21052

21206

21372

21555

21711

21781

21814

14.4

20988

21112

21260

21398

21548

21718

21862

21915

21931

14.6

21223

21333

21467

21589

21724

21880

22010

22047

22050

14.8

21461

21556

21675

21781

21900

22040

22156

22179

22169

15.0

21703

21781

21882

21972

22075

22200

22300

22310

22289

15.2

21948

22006

22089

22163

22251

22358

22441

22440

22409

15.4

22195

22233

22296

22354

22427

22516

22581

22569

22529

15.6

22444

22460

22503

22545

22603

22673

22719

22697

22649

15.8

22695

22688

22709

22736

22779

22829

22856

22824

22769

16.0

22947

22916

22914

22926

22955

22984

22992

22951

22889

16.2

23200

23144

23119

23117

23131

23140

23127

23076

23008

08.01.236

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE =1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.4

23452

23371

23323

23307

23308

23295

23260

23200

23126

16.6

23705

23599

23527

23497

23486

23450

23394

23324

23244

16.8

23957

23825

23729

23687

23664

23604

23527

23447

23360

17.0

24208

24051

23931

23876

23842

23759

23660

23569

23475

17.2

24459

24276

24132

24065

24019

23913

23793

23690

23590

17.4

24709

24500

24333

24254

24196

24067

23925

23811

23704

17.6

24958

24724

24534

24441

24371

24220

24057

23932

23817

17.8

25206

24948

24735

24628

24544

24371

24190

24052

23929

18.0

25454

25172

24936

24813

24716

24522

24322

24172

24041

18.2

25701

25396

25138

24997

24884

24670

24454

24293

24153

18.4

25946

25620

25340

25180

25049

24817

24586

24413

24265

18.6

26191

25843

25543

25361

25210

24963

24718

24534

24376

18.8

26435

26068

25747

25541

25367

25105

24850

24656

24488

19.0

26678

26292

25951

25718

25521

25247

24983

24777

24599

19.2

26920

26515

26256

25895

25672

25386

25115

24899

24711

19.4

27161

26739

26360

26069

25820

25524

25247

25021

24822

19.6

27401

26961

26564

26243

25966

25661

25378

25143

24934

19.8

27639

27183

26766

26415

26110

25796

25509

25265

25046

20.0

27875

27403

26967

26586

26255

25931

25640

25387

25157

20.2

28112

27621

27167

26756

26398

26066

25769

25508

25269

20.4

28346

27838

27364

26925

26543

26201

25898

25629

25380

20.6

28579

28053

27559

27093

26688

26335

26026

25749

25492

Original

07-14-08

08.01.237

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE =1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

20.8

28810

28265

27751

27261

26834

26470

26153

25868

25603

21.0

29039

28476

27940

27427

26982

26605

26279

25987

25715

21.2

29268

28684

28127

27593

27130

26740

26404

26105

25826

FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

9519

10076

10636

11201

11774

12354

12925

13471

14002

3.2

9658

10221

10787

11348

11913

12491

13062

13608

14137

3.4

9797

10368

10938

11494

12052

12629

13200

13745

14271

3.6

9938

10515

11090

11642

12193

12767

13339

13883

14406

3.8

10081

10662

11241

11789

12335

12907

13477

14020

14540

4.0

10227

10811

11393

11938

12479

13047

13616

14157

14675

4.2

10375

10961

11544

12087

12624

13189

13756

14295

14810

4.4

10525

11112

11696

12238

12772

13333

13896

14433

14945

4.6

10680

11265

11848

12389

12922

13479

14037

14571

15081

4.8

10838

11419

12000

12542

13074

13626

14178

14709

15217

5.0

10999

11575

12152

12695

13229

13775

14321

14848

15353

5.2

11164

11733

12305

12850

13385

13926

14464

14987

15490

08.01.238

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

5.4

11332

11893

12459

13006

13543

14078

14608

15126

15626

5.6

11503

12055

12614

13163

13703

14232

14753

15266

15763

5.8

11677

12219

12770

13321

13863

14386

14899

15407

15901

6.0

11854

12386

12928

13480

14024

14542

15045

15548

16038

6.2

12033

12554

13088

13640

14185

14697

15193

15690

16175

6.4

12215

12725

13250

13801

14346

14854

15342

15833

16313

6.6

12399

12899

13415

13963

14507

15010

15493

15977

16450

6.8

12585

13075

13582

14126

14667

15167

15644

16122

16588

7.0

12772

13253

13752

14290

14827

15323

15797

16268

16726

7.2

12962

13434

13924

14455

14986

15480

15950

16414

16863

7.4

13153

13616

14099

14621

15146

15637

16104

16562

17001

7.6

13345

13801

14276

14788

15305

15794

16259

16709

17139

7.8

13538

13987

14455

14957

15466

15952

16414

16858

17277

8.0

13732

14175

14636

15128

15627

16110

16570

17006

17416

8.2

13926

14363

14818

15299

15790

16269

16726

17155

17555

8.4

14121

14553

15002

15473

15953

16428

16881

17304

17694

8.6

14316

14744

15187

15649

16119

16588

17037

17452

17833

8.8

14512

14936

15374

15826

16286

16749

17193

17601

17973

9.0

14708

15128

15562

16005

16455

16910

17348

17749

18114

9.2

14905

15321

15751

16185

16626

17073

17503

17897

18254

9.4

15103

15516

15941

16367

16798

17236

17659

18045

18395

9.6

15303

15712

16132

16550

16972

17400

17814

18193

18536

Original

07-14-08

08.01.239

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

9.8

15505

15909

16324

16734

17146

17564

17969

18341

18677

10.0

15710

16108

16516

16919

17322

17729

18124

18489

18819

10.2

15918

16309

16709

17104

17498

17894

18279

18637

18960

10.4

16130

16511

16903

17290

17675

18061

18435

18785

19101

10.6

16346

16716

17097

17476

17853

18227

18591

18934

19242

10.8

16566

16922

17291

17662

18031

18394

18747

19082

19384

11.0

16790

17131

17485

17848

18209

18562

18903

19230

19524

11.2

17018

17342

17681

18034

18388

18730

19060

19378

19665

11.4

17249

17554

17876

18220

18567

18898

19217

19527

19805

11.6

17482

17768

18073

18407

18746

19067

19375

19675

19944

11.8

17717

17983

18271

18594

18925

19236

19532

19823

20082

12.0

17953

18200

18470

18782

19105

19406

19691

19971

20220

12.2

18190

18417

18670

18971

19285

19575

19849

20118

20356

12.4

18427

18636

18872

19161

19465

19745

20008

20265

20491

12.6

18665

18856

19075

19351

19644

19915

20167

20412

20625

12.8

18901

19076

19280

19543

19825

20085

20327

20559

20757

13.0

19137

19297

19487

19735

20005

20256

20487

20704

20888

13.2

19374

19519

19695

19928

20185

20426

20647

20850

21018

13.4

19610

19742

19904

20122

20365

20596

20807

20995

21146

13.6

19846

19966

20115

20317

20545

20767

20967

21139

21274

13.8

20083

20190

20326

20513

20726

20937

21127

21283

21401

14.0

20322

20416

20539

20709

20906

21107

21286

21427

21527

08.01.240

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

14.2

20561

20642

20752

20905

21087

21276

21445

21569

21653

14.4

20802

20870

20965

21102

21267

21446

21603

21712

21778

14.6

21044

21099

21179

21299

21448

21615

21760

21853

21904

14.8

21289

21328

21394

21496

21629

21783

21917

21994

22029

15.0

21536

21559

21608

21693

21810

21951

22072

22135

22154

15.2

21784

21791

21823

21890

21991

22119

22227

22275

22280

15.4

22034

22023

22038

22088

22173

22286

22380

22413

22405

15.6

22285

22256

22253

22286

22355

22453

22532

22551

22530

15.8

22538

22490

22467

22483

22536

22619

22683

22688

22654

16.0

22792

22724

22682

22681

22719

22784

22832

22824

22779

16.2

23047

22958

22896

22879

22901

22949

22980

22959

22903

16.4

23303

23192

23110

23077

23084

23114

23126

23093

23027

16.6

23560

23427

23323

23276

23268

23277

23271

23225

23151

16.8

23818

23661

23536

23474

23451

23441

23414

23356

23274

17.0

24077

23895

23749

23672

23635

23603

23556

23486

23397

17.2

24336

24129

23961

23870

23819

23765

23697

23615

23520

17.4

24595

24363

24173

24068

24002

23926

23836

23743

23642

17.6

24855

24598

24384

24264

24185

24086

23975

23870

23763

17.8

25115

24832

24595

24461

24366

24245

24113

23997

23884

18.0

25375

25066

24807

24656

24546

24403

24250

24123

24004

18.2

25636

25301

25018

24850

24724

24559

24387

24249

24123

18.4

25896

25536

25228

25043

24901

24715

24524

24374

24241

Original

07-14-08

08.01.241

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

18.6

26156

25771

25439

25235

25075

24870

24661

24500

24358

18.8

26415

26006

25650

25425

25246

25023

24799

24625

24474

19.0

26674

26241

25861

25614

25415

25175

24937

24751

24590

19.2

26933

26476

26072

25801

25582

25326

25074

24877

24704

19.4

27190

26711

26283

25988

25747

25476

25212

25002

24818

19.6

27447

26946

26493

26173

25910

25624

25350

25128

24931

19.8

27702

27179

26703

26357

26071

25772

25487

25253

25044

20.0

27956

27412

26913

26540

26232

25918

25623

25378

25157

20.2

28208

27644

27122

26722

26390

26063

25759

25503

25270

20.4

28458

27875

27330

26903

26548

26208

25895

25628

25383

20.6

28706

28104

27538

27084

26706

26351

26029

25752

25496

20.8

28951

28332

27745

27265

26862

26494

26163

25876

25609

21.0

29195

28558

27951

27444

27018

26636

26296

25999

25722

21.2

29437

28783

28155

27623

27173

26777

26427

26122

25836

FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

3.0 08.01.242

9160

-1.50 9692

-1.00

-.50

0.00

.50

1.00

1.50

2.00

10231

10811

11401

11977

12541

13090

13626

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.2

9311

9846

10384

10953

11532

12113

12684

13229

13759

3.4

9463

10000

10537

11096

11665

12249

12827

13369

13893

3.6

9615

10153

10690

11240

11799

12386

12969

13508

14027

3.8

9766

10307

10844

11386

11935

12524

13111

13647

14161

4.0

9917

10460

10999

11532

12073

12663

13253

13786

14296

4.2

10068

10614

11154

11681

12214

12804

13394

13924

14431

4.4

10218

10767

11310

11832

12358

12946

13534

14063

14567

4.6

10368

10920

11467

11985

12506

13090

13674

14201

14703

4.8

10517

11074

11624

12141

12658

13235

13813

14339

14841

5.0

10667

11227

11783

12299

12814

13382

13952

14477

14979

5.2

10813

11382

11942

12459

12972

13532

14091

14615

15117

5.4

10971

11537

12102

12621

13133

13682

14231

14753

15256

5.6

11127

11694

12262

12783

13296

13834

14371

14891

15396

5.8

11286

11853

12423

12947

13460

13988

14512

15031

15535

6.0

11449

12014

12585

13112

13626

14143

14654

15171

15675

6.2

11617

12178

12747

13276

13792

14299

14799

15312

15815

6.4

11791

12345

12909

13441

13958

14456

14945

15454

15954

6.6

11972

12516

13072

13605

14124

14614

15094

15598

16094

6.8

12159

12690

13235

13768

14289

14774

15245

15744

16233

7.0

12352

12868

13399

13931

14454

14934

15399

15890

16372

7.2

12551

13049

13564

14094

14618

15095

15555

16039

16510

7.4

12754

13233

13730

14257

14781

15256

15713

16188

16649

Original

07-14-08

08.01.243

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.6

12960

13420

13899

14421

14945

15418

15872

16338

16788

7.8

13168

13609

14070

14587

15108

15580

16032

16489

16927

8.0

13377

13800

14244

14754

15272

15743

16192

16640

17067

8.2

13586

13993

14420

14923

15436

15905

16353

16791

17207

8.4

13794

14188

14601

15094

15601

16068

16514

16943

17347

8.6

14000

14384

14786

15269

15766

16231

16674

17095

17488

8.8

14203

14580

14975

15446

15932

16393

16833

17246

17630

9.0

14404

14778

15167

15626

16100

16556

16992

17397

17772

9.2

14603

14976

15363

15809

16268

16718

17150

17548

17915

9.4

14802

15176

15562

15994

16438

16881

17308

17699

18058

9.6

15001

15376

15762

16181

16609

17044

17466

17850

18202

9.8

15201

15578

15964

16369

16782

17208

17623

18001

18347

10.0

15403

15780

16166

16558

16955

17373

17780

18152

18491

10.2

15607

15984

16369

16748

17131

17539

17938

18303

18636

10.4

15816

16190

16571

16938

17308

17705

18096

18455

18781

10.6

16028

16396

16771

17128

17487

17873

18254

18606

18926

10.8

16246

16604

16970

17318

17667

18043

18413

18758

19072

11.0

16468

16813

17167

17508

17849

18214

18572

18910

19217

11.2

16695

17024

17364

17697

18033

18386

18732

19062

19362

11.4

16926

17237

17560

17887

18217

18558

18892

19214

19506

11.6

17161

17451

17756

18077

18403

18732

19053

19366

19651

11.8

17399

17667

17953

18267

18589

18906

19214

19519

19795

08.01.244

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

12.0

17640

17886

18151

18458

18775

19080

19375

19671

19938

12.2

17884

18106

18351

18650

18962

19255

19537

19823

20081

12.4

18129

18329

18552

18842

19148

19430

19699

19975

20223

12.6

18376

18554

18757

19036

19334

19604

19861

20127

20365

12.8

18625

18781

18964

19231

19519

19778

20023

20278

20505

13.0

18875

19010

19174

19428

19704

19952

20185

20429

20645

13.2

19125

19242

19386

19625

19889

20125

20347

20580

20783

13.4

19377

19475

19601

19824

20073

20299

20510

20731

20921

13.6

19629

19709

19818

20023

20257

20472

20673

20882

21058

13.8

19881

19945

20036

20224

20442

20646

20837

21032

21194

14.0

20134

20181

20255

20425

20626

20820

21001

21183

21329

14.2

20386

20418

20475

20627

20811

20995

21166

21333

21464

14.4

20639

20655

20696

20829

20996

21170

21331

21482

21597

14.6

20891

20892

20918

21032

21181

21345

21497

21632

21729

14.8

21142

21129

21139

21235

21367

21522

21663

21782

21861

15.0

21393

21366

21361

21438

21554

21698

21830

21931

21992

15.2

21645

21602

21582

21641

21741

21875

21997

22080

22122

15.4

21896

21839

21804

21845

21929

22052

22164

22228

22252

15.6

22148

22076

22025

22050

22117

22229

22329

22376

22382

15.8

22402

22313

22247

22254

22305

22406

22494

22523

22512

16.0

22656

22551

22468

22459

22494

22581

22657

22669

22641

16.2

22912

22790

22690

22664

22683

22756

22818

22814

22771

Original

07-14-08

08.01.245

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.4

23170

23029

22912

22869

22872

22930

22977

22957

22902

16.6

23431

23270

23134

23074

23061

23102

23133

23100

23033

16.8

23693

23512

23356

23280

23251

23273

23286

23240

23165

17.0

23958

23754

23578

23485

23440

23443

23436

23380

23298

17.2

24225

23997

23799

23691

23629

23611

23585

23518

23430

17.4

24494

24242

24021

23896

23819

23778

23731

23655

23563

17.6

24765

24486

24242

24102

24008

23944

23876

23791

23695

17.8

25036

24731

24463

24306

24196

24109

24019

23926

23826

18.0

25309

24977

24683

24511

24385

24274

24162

24060

23956

18.2

25582

25222

24903

24714

24573

24439

24305

24194

24084

18.4

25856

25468

25122

24917

24760

24603

24447

24326

24211

18.6

26129

25713

25340

25119

24947

24767

24590

24458

24336

18.8

26403

25959

25558

25320

25133

24931

24734

24590

24459

19.0

26677

26204

25775

25520

25318

25095

24878

24721

24579

19.2

26950

26449

25992

25719

25502

25259

25023

24852

24698

19.4

27222

26693

26208

25917

25685

25422

25168

24982

24815

19.6

27493

26937

26425

26114

25866

25584

25313

25113

24932

19.8

27764

27182

26642

26311

26045

25745

25459

25242

25047

20.0

28032

27425

26859

26507

26222

25906

25604

25372

25162

20.2

28300

27669

27077

26702

26398

26064

25748

25502

25277

20.4

28565

27913

27297

26897

26570

26221

25893

25632

25391

20.6

28828

28156

27518

27091

26740

26376

26036

25761

25507

08.01.246

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER THREE (WSTA 473.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

20.8

29089

28399

27740

27284

26908

26529

26179

25891

25623

21.0

29348

28641

27962

27477

27073

26680

26321

26020

25739

21.2

29605

28883

28186

27669

27235

26829

26462

26150

25856

FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

23242

24046

24701

25188

25562

25902

26189

26411

26661

3.2

23430

24211

24844

25319

25684

26015

26293

26508

26752

3.4

23617

24375

24987

25449

25805

26127

26397

26606

26842

3.6

23804

24540

25130

25579

25927

26240

26501

26703

26932

3.8

23991

24704

25272

25709

26048

26352

26605

26800

27022

4.0

24178

24867

25414

25839

26168

26463

26708

26896

27111

4.2

24364

25030

25556

25968

26289

26574

26811

26992

27200

4.4

24549

25192

25697

26097

26408

26684

26913

27087

27288

4.6

24734

25354

25838

26224

26527

26794

27015

27182

27376

4.8

24917

25514

25978

26352

26645

26903

27116

27276

27464

5.0

25100

25674

26117

26478

26763

27012

27216

27370

27550

Original

07-14-08

08.01.247

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

5.2

25281

25833

26256

26604

26880

27119

27316

27463

27636

5.4

25461

25990

26394

26729

26996

27226

27414

27555

27722

5.6

25640

26146

26532

26854

27111

27332

27512

27646

27807

5.8

25816

26301

26668

26977

27225

27438

27610

27737

27892

6.0

25991

26454

26803

27100

27338

27542

27706

27827

27976

6.2

26163

26606

26938

27221

27450

27646

27802

27917

28059

6.4

26332

26756

27071

27342

27562

27749

27898

28006

28142

6.6

26499

26904

27203

27461

27672

27851

27992

28095

28225

6.8

26663

27050

27333

27580

27781

27952

28086

28183

28307

7.0

26824

27194

27463

27698

27890

28052

28179

28270

28388

7.2

26983

27337

27591

27815

27997

28152

28272

28358

28470

7.4

27141

27479

27719

27931

28105

28251

28364

28445

28551

7.6

27298

27620

27847

28047

28211

28350

28456

28532

28632

7.8

27454

27761

27975

28164

28318

28449

28548

28618

28713

8.0

27609

27902

28102

28280

28425

28548

28640

28705

28794

8.2

27766

28043

28231

28397

28532

28647

28732

28792

28875

8.4

27923

28185

28359

28514

28640

28746

28825

28879

28956

8.6

28081

28328

28489

28632

28748

28847

28918

28967

29038

8.8

28241

28472

28620

28751

28857

28947

29012

29055

29119

9.0

28402

28617

28751

28870

28967

29048

29106

29143

29202

9.2

28563

28762

28882

28990

29076

29149

29200

29231

29284

9.4

28725

28907

29014

29109

29186

29251

29293

29319

29366

08.01.248

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

9.6

28886

29052

29144

29228

29295

29351

29387

29406

29447

9.8

29046

29195

29274

29346

29404

29451

29480

29494

29529

10.0

29204

29337

29403

29463

29511

29550

29572

29580

29609

10.2

29360

29477

29529

29578

29617

29648

29663

29666

29689

10.4

29513

29614

29654

29692

29722

29745

29753

29750

29768

10.6

29663

29748

29775

29803

29824

29839

29842

29833

29846

10.8

29808

29878

29894

29912

29924

29932

29928

29915

29922

11.0

29951

30006

30010

30018

30022

30023

30014

29996

29998

11.2

30090

30130

30124

30122

30119

30112

30097

30078

30072

11.4

30226

30253

30236

30225

30214

30200

30180

30154

30146

11.6

30361

30373

30346

30326

30307

30288

30262

30232

30219

11.8

30494

30493

30455

30426

30400

30374

30344

30309

30292

12.0

30625

30611

30564

30526

30493

30461

30425

30387

30365

12.2

30756

30729

30672

30626

30585

30547

30506

30464

30437

12.4

30886

30847

30780

30725

30678

30633

30588

30541

30510

12.6

31017

30965

30888

30826

30771

30720

30669

30619

30583

12.8

31148

31084

30998

30926

30864

30807

30752

30697

30656

13.0

31280

31204

31107

31028

30959

30895

30834

30776

30730

13.2

31412

31324

31217

31130

31053

30984

30917

30855

30804

13.4

31544

31445

31328

31232

31148

31072

31001

30934

30878

13.6

31677

31565

31438

31334

31243

31161

31084

31013

30952

13.8

31809

31686

31549

31436

31338

31250

31167

31092

31026

Original

07-14-08

08.01.249

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

14.0

31941

31806

31659

31538

31433

31338

31250

31171

31100

14.2

32072

31926

31769

31640

31527

31426

31333

31249

31174

14.4

32203

32045

31878

31741

31621

31514

31415

31327

31247

14.6

32333

32164

31987

31841

31715

31601

31497

31404

31319

14.8

32463

32281

32094

31940

31807

31687

31578

31481

31392

15.0

32591

32398

32201

32039

31899

31773

31658

31557

31463

15.2

32718

32513

32307

32137

31990

31857

31738

31633

31534

15.4

32844

32627

32412

32234

32080

31941

31817

31708

31605

15.6

32969

32739

32516

32329

32169

32025

31895

31782

31674

15.8

33091

32851

32618

32424

32257

32107

31973

31856

31744

16.0

33213

32961

32720

32518

32345

32189

32050

31929

31813

16.2

33332

33069

32820

32611

32432

32270

32127

32002

31882

16.4

33450

33176

32920

32704

32518

32351

32203

32074

31950

16.6

33565

33281

33018

32795

32603

32431

32279

32146

32018

16.8

33678

33385

33114

32885

32688

32510

32354

32218

32085

17.0

33790

33488

33210

32975

32771

32589

32428

32290

32152

17.2

33899

33589

33305

33063

32855

32667

32503

32361

32219

08.01.250

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE =-1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

22563

23487

24256

24819

25242

25612

25921

26168

26440

3.2

22764

23667

24415

24960

25370

25729

26030

26270

26535

3.4

22964

23846

24574

25101

25497

25846

26139

26372

26629

3.6

23164

24025

24731

25241

25624

25963

26248

26474

26723

3.8

23363

24202

24888

25380

25750

26079

26356

26575

26817

4.0

23561

24378

25042

25518

25875

26194

26464

26676

26910

4.2

23757

24552

25195

25655

26000

26309

26570

26775

27003

4.4

23952

24725

25347

25790

26124

26423

26676

26874

27094

4.6

24145

24895

25496

25924

26246

26536

26781

26972

27185

4.8

24337

25063

25642

26056

26368

26648

26885

27069

27275

5.0

24526

25229

25787

26186

26488

26759

26988

27165

27364

5.2

24715

25393

25929

26315

26607

26869

27090

27260

27452

5.4

24901

25555

26071

26443

26726

26979

27191

27354

27539

5.6

25087

25717

26211

26570

26844

27088

27292

27448

27626

5.8

25272

25877

26350

26696

26962

27197

27392

27541

27713

6.0

25455

26036

26489

26822

27079

27305

27492

27635

27800

6.2

25638

26195

26627

26948

27196

27414

27592

27728

27887

6.4

25820

26354

26765

27074

27313

27522

27692

27821

27973

6.6

26002

26513

26904

27200

27431

27631

27793

27915

28060

6.8

26184

26672

27043

27326

27548

27740

27894

28009

28148

7.0

26365

26831

27183

27453

27666

27849

27994

28104

28235

Original

07-14-08

08.01.251

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE =-1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

26546

26991

27323

27580

27784

27958

28096

28198

28323

7.4

26725

27150

27464

27707

27902

28067

28197

28293

28411

7.6

26905

27309

27604

27835

28019

28175

28297

28387

28499

7.8

27084

27467

27744

27962

28137

28284

28398

28481

28586

8.0

27262

27625

27884

28088

28253

28391

28498

28575

28674

8.2

27439

27782

28023

28214

28370

28499

28598

28669

28760

8.4

27615

27938

28162

28340

28485

28605

28697

28761

28846

8.6

27790

28094

28300

28465

28600

28711

28795

28853

28932

8.8

27963

28248

28437

28589

28714

28816

28892

28944

29017

9.0

28136

28401

28574

28712

28826

28920

28988

29034

29101

9.2

28307

28552

28709

28834

28938

29023

29084

29124

29184

9.4

28476

28702

28842

28955

29049

29125

29178

29212

29266

9.6

28643

28850

28975

29075

29159

29226

29272

29300

29348

9.8

28808

28996

29106

29193

29268

29326

29365

29387

29429

10.0

28971

29141

29235

29311

29375

29425

29457

29473

29510

10.2

29131

29283

29363

29427

29482

29524

29549

29559

29590

10.4

29289

29423

29489

29542

29587

29621

29639

29645

29670

10.6

29444

29561

29614

29655

29691

29718

29729

29729

29749

10.8

29595

29697

29737

29767

29794

29813

29819

29814

29828

11.0

29745

29830

29858

29878

29897

29908

29908

29898

29907

11.2

29892

29962

29977

29988

29998

30002

29996

29981

29985

11.4

30038

30092

30096

30097

30099

30096

30084

30065

30063

08.01.252

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE =-1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.6

30183

30222

30214

30206

30199

30190

30172

30148

30141

11.8

30327

30351

30332

30314

30299

30283

30259

30231

30219

12.0

30471

30480

30450

30422

30399

30376

30347

30314

30297

12.2

30615

30610

30568

30531

30500

30469

30434

30397

30375

12.4

30760

30740

30687

30640

30600

30563

30522

30480

30453

12.6

30906

30872

30806

30749

30701

30657

30610

30564

30531

12.8

31054

31005

30927

30860

30803

30751

30699

30647

30609

13.0

31203

31139

31048

30970

30905

30846

30788

30731

30687

13.2

31353

31274

31170

31082

31007

30941

30876

30815

30765

13.4

31503

31408

31292

31193

31110

31036

30965

30898

30843

13.6

31652

31543

31414

31303

31212

31130

31053

30982

30921

13.8

31800

31676

31534

31413

31313

31224

31141

31064

30999

14.0

31947

31809

31654

31522

31413

31317

31228

31147

31075

14.2

32091

31939

31772

31630

31513

31409

31314

31228

31152

14.4

32233

32066

31888

31736

31611

31500

31400

31309

31227

14.6

32371

32191

32001

31841

31707

31590

31484

31388

31302

14.8

32505

32312

32112

31943

31802

31678

31567

31467

31375

15.0

32636

32430

32221

32043

31895

31765

31648

31544

31448

15.2

32764

32546

32327

32142

31987

31851

31729

31621

31520

15.4

32889

32659

32432

32239

32077

31935

31809

31697

31592

15.6

33012

32771

32535

32335

32167

32019

31888

31772

31663

15.8

33134

32881

32637

32430

32255

32103

31967

31847

31734

Original

07-14-08

08.01.253

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE =-1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.0

33254

32990

32739

32525

32344

32186

32046

31922

31804

16.2

33373

33099

32840

32619

32432

32269

32124

31997

31875

16.4

33492

33207

32941

32714

32520

32352

32203

32072

31946

16.6

33611

33316

33042

32809

32609

32435

32281

32147

32017

16.8

33731

33426

33144

32904

32698

32519

32361

32223

32088

17.0

33850

33535

33246

33000

32788

32603

32440

32299

32160

17.2

33970

33646

33349

33095

32877

32687

32520

32375

32231

FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

21763

22816

23745

24410

24904

25330

25678

25954

26250

3.2

21977

23011

23920

24561

25036

25450

25791

26060

26348

3.4

22190

23205

24093

24711

25167

25570

25904

26166

26446

3.6

22403

23398

24265

24860

25298

25690

26016

26271

26544

3.8

22614

23589

24435

25008

25429

25809

26128

26375

26641

4.0

22824

23779

24603

25155

25559

25928

26239

26479

26737

4.2

23032

23966

24769

25300

25688

26046

26350

26583

26833

4.4

23239

24151

24932

25444

25816

26163

26459

26685

26928

08.01.254

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

4.6

23444

24334

25092

25586

25944

26280

26568

26787

27022

4.8

23647

24514

25249

25725

26070

26396

26675

26887

27115

5.0

23848

24691

25402

25863

26196

26511

26782

26987

27207

5.2

24047

24866

25554

26000

26321

26626

26888

27086

27298

5.4

24246

25040

25703

26135

26446

26740

26993

27184

27389

5.6

24443

25212

25851

26269

26570

26855

27098

27282

27480

5.8

24641

25384

25998

26403

26694

26969

27203

27380

27570

6.0

24838

25555

26144

26536

26818

27083

27308

27478

27660

6.2

25036

25727

26291

26670

26943

27197

27413

27575

27751

6.4

25234

25899

26437

26803

27068

27312

27518

27674

27842

6.6

25433

26071

26585

26938

27193

27427

27624

27772

27933

6.8

25634

26245

26734

27073

27319

27542

27730

27871

28024

7.0

25835

26420

26884

27209

27446

27659

27837

27971

28117

7.2

26037

26596

27035

27346

27573

27775

27945

28070

28209

7.4

26239

26771

27186

27482

27700

27891

28052

28170

28301

7.6

26441

26946

27337

27619

27826

28007

28159

28269

28393

7.8

26641

27120

27488

27754

27952

28122

28265

28368

28485

8.0

26840

27293

27637

27889

28077

28236

28370

28466

28576

8.2

27037

27465

27786

28023

28200

28350

28475

28563

28666

8.4

27231

27634

27933

28155

28322

28462

28578

28659

28756

8.6

27422

27801

28078

28286

28443

28572

28680

28754

28844

8.8

27611

27965

28221

28414

28561

28681

28780

28847

28930

Original

07-14-08

08.01.255

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

9.0

27796

28126

28362

28541

28678

28788

28879

28939

29016

9.2

27978

28285

28501

28666

28792

28893

28976

29030

29100

9.4

28157

28441

28638

28789

28906

28998

29072

29119

29184

9.6

28333

28596

28774

28911

29018

29101

29168

29208

29266

9.8

28507

28748

28908

29033

29129

29203

29262

29297

29348

10.0

28679

28899

29042

29153

29239

29305

29356

29384

29430

10.2

28848

29048

29174

29273

29349

29406

29449

29472

29511

10.4

29016

29197

29306

29392

29458

29507

29542

29559

29593

10.6

29182

29344

29437

29511

29567

29608

29635

29647

29674

10.8

29347

29490

29568

29630

29676

29709

29729

29734

29756

11.0

29511

29636

29698

29748

29785

29810

29822

29822

29838

11.2

29673

29782

29829

29867

29894

29910

29916

29910

29920

11.4

29835

29927

29959

29986

30002

30011

30009

29998

30002

11.6

29996

30071

30089

30104

30111

30112

30103

30087

30084

11.8

30157

30216

30219

30223

30220

30213

30196

30175

30166

12.0

30318

30360

30348

30341

30328

30313

30290

30263

30249

12.2

30480

30505

30478

30459

30437

30414

30383

30351

30330

12.4

30642

30650

30608

30577

30545

30514

30476

30438

30412

12.6

30804

30795

30738

30695

30653

30614

30569

30525

30494

12.8

30968

30940

30869

30813

30761

30714

30662

30612

30575

13.0

31132

31085

30999

30931

30869

30813

30754

30699

30656

13.2

31296

31230

31129

31048

30977

30911

30846

30785

30736

08.01.256

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

13.4

31459

31374

31258

31164

31083

31010

30938

30870

30816

13.6

31621

31517

31385

31279

31189

31107

31028

30955

30895

13.8

31780

31658

31512

31393

31294

31204

31118

31040

30974

14.0

31937

31796

31637

31506

31398

31299

31207

31123

31052

14.2

32091

31932

31760

31618

31501

31394

31296

31206

31130

14.4

32241

32065

31880

31727

31602

31487

31383

31288

31207

14.6

32386

32195

31998

31835

31701

31579

31469

31369

31283

14.8

32526

32321

32113

31941

31799

31670

31554

31449

31358

15.0

32662

32443

32225

32045

31895

31760

31638

31529

31433

15.2

32794

32563

32336

32147

31990

31848

31721

31607

31506

15.4

32924

32681

32444

32248

32083

31936

31803

31686

31580

15.6

33051

32797

32552

32348

32176

32024

31885

31764

31653

15.8

33176

32911

32658

32448

32269

32111

31967

31841

31726

16.0

33301

33026

32765

32547

32361

32197

32048

31919

31799

16.2

33425

33140

32871

32647

32453

32284

32130

31997

31872

16.4

33550

33255

32977

32746

32546

32371

32212

32075

31945

16.6

33677

33371

33085

32847

32640

32459

32294

32153

32019

16.8

33805

33488

33194

32948

32734

32547

32377

32232

32093

17.0

33935

33607

33303

33050

32829

32636

32461

32311

32168

17.2

34066

33726

33413

33152

32924

32725

32544

32390

32242

Original

07-14-08

08.01.257

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

20876

22036

23101

23934

24557

25026

25389

25698

26013

3.2

21100

22240

23281

24089

24692

25148

25504

25805

26114

3.4

21323

22444

23462

24245

24826

25270

25619

25914

26214

3.6

21546

22647

23642

24400

24960

25392

25734

26022

26314

3.8

21769

22849

23821

24554

25094

25514

25848

26129

26415

4.0

21990

23051

23999

24709

25228

25636

25963

26237

26515

4.2

22211

23252

24176

24862

25361

25758

26077

26344

26614

4.4

22432

23451

24353

25015

25495

25880

26192

26452

26714

4.6

22651

23649

24527

25167

25628

26002

26306

26558

26813

4.8

22669

23845

24701

25318

25761

26123

26420

26665

26912

5.0

23086

24041

24873

25469

25894

26245

26533

26772

27011

5.2

23302

24235

25044

25618

26027

26366

26647

26878

27109

5.4

23518

24428

25213

25767

26160

26487

26760

26983

27208

5.6

23733

24620

25382

25916

26292

26608

26873

27089

27305

5.8

23948

24811

25550

26063

26424

26729

26985

27194

27403

6.0

24162

25002

25717

26211

26556

26850

27098

27299

27500

6.2

24377

25192

25883

26358

26689

26971

27210

27403

27596

6.4

24591

25382

26049

26504

26821

27092

27322

27508

27693

6.6

24806

25572

26214

26650

26952

27213

27433

27611

27789

6.8

25021

25761

26379

26796

27084

27333

27544

27715

27884

7.0

25235

25951

26543

26941

27216

27453

27655

27817

27979

08.01.258

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

25450

26139

26706

27086

27347

27573

27766

27920

28074

7.4

25664

26327

26868

27230

27478

27693

27876

28021

28167

7.6

25876

26513

27029

27373

27608

27812

27985

28122

28261

7.8

26087

26698

27188

27514

27737

27930

28093

28223

28353

8.0

26297

26881

27346

27655

27866

28047

28201

28322

28445

8.2

26504

27062

27502

27794

27993

28163

28307

28421

28537

8.4

26709

27240

27656

27931

28119

28278

28413

28519

28627

8.6

26911

27416

27807

28066

28243

28392

28517

28616

28717

8.8

27111

27589

27956

28200

28366

28505

28621

28711

28806

9.0

27307

27759

28102

28331

28487

28616

28723

28806

28894

9.2

27501

27927

28247

28461

28607

28726

28825

28901

28981

9.4

27694

28093

28390

28591

28726

28836

28925

28994

29068

9.6

27885

28258

28533

28719

28845

28945

29026

29087

29155

9.8

28075

28422

28675

28847

28963

29054

29125

29180

29241

10.0

28265

28586

28816

28974

29081

29162

29225

29273

29328

10.2

28455

28750

28958

29102

29199

29271

29325

29366

29414

10.4

28645

28915

29101

29230

29317

29379

29425

29459

29500

10.6

28836

29080

29244

29359

29436

29489

29525

29552

29587

10.8

29028

29247

29389

29490

29556

29598

29626

29646

29674

11.0

29222

29415

29535

29620

29676

29709

29727

29740

29761

11.2

29415

29584

29681

29752

29797

29819

29829

29834

29849

11.4

29608

29752

29828

29883

29917

29929

29930

29928

29936

Original

07-14-08

08.01.259

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.6

29799

29920

29974

30014

30037

30039

30031

30022

30023

11.8

29990

30086

30120

30144

30157

30149

30131

30115

30109

12.0

30178

30251

30264

30274

30276

30257

30231

30208

30196

12.2

30363

30414

30407

30402

30393

30365

30330

30300

30281

12.4

30545

30574

30548

30529

30509

30471

30428

30391

30366

12.6

30722

30730

30686

30653

30623

30576

30525

30481

30450

12.8

30896

30883

30822

30776

30735

30679

30620

30570

30533

13.0

31065

31032

30955

30896

30846

30781

30714

30658

30614

13.2

31230

31178

31085

31015

30955

30881

30806

30744

30696

13.4

31392

31322

31214

31132

31062

30980

30898

30830

30776

13.6

31551

31462

31340

31247

31168

31078

30989

30915

30855

13.8

31706

31601

31465

31361

31273

31175

31079

31000

30935

14.0

31860

31737

31589

31474

31377

31271

31168

31084

31014

14.2

32011

31872

31711

31586

31481

31367

31257

31167

31092

14.4

32161

32006

31833

31698

31584

31463

31346

31251

31170

14.6

32310

32139

31953

31809

31687

31558

31435

31335

31249

14.8

32457

32271

32074

31920

31790

31653

31524

31418

31327

15.0

32604

32402

32194

32031

31893

31749

31613

31502

31406

15.2

32750

32533

32314

32142

31995

31844

31702

31585

31484

15.4

32895

32664

32433

32252

32098

31939

31790

31669

31563

15.6

33040

32794

32553

32362

32200

32034

31879

31752

31641

15.8

33184

32924

32672

32472

32302

32129

31968

31836

31719

08.01.260

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.0

33328

33053

32790

32582

32404

32223

32056

31919

31797

16.2

33472

33183

32909

32691

32505

32317

32144

32002

31875

16.4

33615

33312

33027

32800

32606

32411

32231

32084

31952

16.6

33759

33441

33145

32909

32707

32505

32319

32166

32029

16.8

33902

33570

33262

33017

32808

32598

32405

32248

32106

17.0

34045

33699

33380

33125

32908

32691

32492

32330

32182

17.2

34187

33827

33496

33233

33007

32783

32578

32410

32258

FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

19946

21205

22398

23375

24138

24667

25060

25405

25743

3.2

20175

21415

22585

23538

24278

24795

25180

25516

25846

3.4

20405

21625

22772

23701

24418

24923

25299

25627

25950

3.6

20635

21835

22959

23864

24558

25051

25418

25739

26053

3.8

20865

22045

23147

24028

24699

25179

25538

25850

26157

4.0

21095

22256

23335

24191

24839

25307

25658

25962

26261

4.2

21326

22466

23523

24355

24980

25436

25778

26074

26365

Original

07-14-08

08.01.261

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

4.4

21556

22677

23712

24518

25120

25564

25898

26186

26469

4.6

21787

22888

23901

24682

25261

25693

26019

26299

26574

4.8

22018

23100

24091

24846

25403

25821

26140

26412

26679

5.0

22250

23311

24281

25011

25544

25950

26261

26525

26784

5.2

22481

23522

24471

25175

25685

26079

26382

26637

26889

5.4

22712

23733

24661

25338

25827

26208

26503

26750

26994

5.6

22943

23944

24850

25501

25967

26336

26623

26863

27099

5.8

23173

24154

25039

25664

26108

26464

26744

26975

27203

6.0

23404

24363

25226

25825

26248

26591

26863

27086

27307

6.2

23633

24571

25412

25986

26388

26718

26982

27197

27409

6.4

23862

24777

25595

26145

26526

26844

27099

27306

27511

6.6

24090

24983

25777

26302

26664

26969

27216

27414

27611

6.8

24317

25187

25957

26458

26801

27093

27331

27522

27710

7.0

24544

25389

26134

26612

26937

27216

27445

27628

27808

7.2

24769

25590

26308

26765

27072

27339

27558

27733

27905

7.4

24993

25789

26481

26916

27206

27461

27670

27837

28001

7.6

25216

25986

26651

27065

27340

27581

27781

27940

28096

7.8

25437

26181

26820

27214

27472

27702

27891

28042

28190

8.0

25657

26375

26986

27361

27605

27822

28001

28144

28284

8.2

25875

26567

27150

27506

27736

27941

28110

28245

28377

8.4

26092

26757

27313

27651

27867

28060

28219

28346

28470

8.6

26308

26946

27474

27795

27997

28178

28327

28447

28563

08.01.262

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

8.8

26521

27132

27633

27937

28127

28296

28436

28547

28656

9.0

26733

27317

27790

28079

28257

28414

28544

28648

28748

9.2

26945

27501

27947

28220

28386

28532

28651

28748

28841

9.4

27156

27684

28103

28361

28516

28650

28759

28848

28934

9.6

27367

27866

28258

28501

28645

28767

28867

28948

29027

9.8

27578

28048

28413

28641

28774

28885

28974

29048

29119

10.0

27790

28231

28568

28781

28903

29002

29082

29147

29212

10.2

28004

28414

28723

28921

29033

29120

29189

29247

29304

10.4

28219

28598

28879

29061

29162

29238

29297

29347

29397

10.6

28436

28784

29036

29201

29292

29355

29405

29446

29489

10.8

28656

28970

29194

29342

29423

29474

29512

29545

29581

11.0

28877

29158

29352

29483

29553

29592

29620

29645

29673

11.2

29098

29346

29511

29624

29683

29709

29727

29744

29765

11.4

29319

29533

29670

29764

29813

29827

29834

29842

29857

11.6

29538

29719

29827

29904

29942

29943

29941

29940

29948

11.8

29754

29902

29983

30042

30069

30059

30046

30037

30038

12.0

29965

30083

30137

30178

30195

30173

30150

30133

30127

12.2

30172

30260

30288

30313

30320

30286

30253

30228

30216

12.4

30372

30432

30437

30445

30442

30397

30355

30322

30303

12.6

30564

30598

30581

30574

30561

30506

30454

30415

30389

12.8

30749

30759

30721

30701

30678

30613

30552

30506

30474

Original

07-14-08

08.01.263

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

13.0

30926

30915

30858

30825

30792

30718

30649

30597

30558

13.2

31097

31066

30992

30947

30904

30822

30744

30686

30642

13.4

31262

31213

31123

31067

31015

30924

30838

30774

30724

13.6

31424

31357

31252

31186

31124

31026

30931

30862

30806

13.8

31582

31500

31380

31303

31232

31126

31024

30949

30887

14.0

31739

31641

31507

31420

31340

31226

31116

31036

30969

14.2

31896

31781

31634

31537

31448

31326

31208

31123

31050

14.4

32052

31922

31761

31655

31557

31427

31301

31210

31132

14.6

32211

32065

31889

31773

31666

31527

31394

31298

31214

14.8

32372

32209

32019

31892

31776

31629

31488

31386

31297

15.0

32535

32354

32150

32011

31886

31731

31583

31475

31380

15.2

32700

32501

32282

32132

31998

31833

31678

31563

31463

15.4

32866

32648

32415

32252

32110

31936

31773

31652

31546

15.6

33032

32795

32547

32372

32221

32038

31868

31741

31630

15.8

33198

32942

32680

32493

32333

32141

31962

31829

31713

16.0

33364

33088

32811

32612

32444

32242

32057

31917

31795

16.2

33528

33233

32942

32731

32554

32343

32150

32005

31877

16.4

33690

33377

33071

32848

32663

32443

32243

32091

31958

16.6

33850

33518

33198

32964

32770

32541

32334

32177

32039

16.8

34007

33656

33323

33078

32876

32639

32424

32261

32118

17.0

34161

33792

33446

33191

32980

32735

32513

32344

32196

17.2

34312

33926

33567

33301

33083

32829

32600

32427

32273

08.01.264

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

19089

20372

21626

22712

23583

24231

24714

25103

25470

3.2

19318

20586

21823

22891

25743

24373

24840

25219

25578

3.4

19547

20800

22021

23069

23903

24514

24967

25335

25686

3.6

19776

21015

22218

23248

24062

24655

25093

25452

25794

3.8

20006

21229

22416

23426

24220

24796

25219

25568

25902

4.0

20236

21444

22614

23605

24378

24936

25346

25684

26010

4.2

20467

21660

22812

23782

24536

25076

25472

25800

26118

4.4

20699

21876

23010

23960

24692

25215

25597

25916

26226

4.6

20931

22093

23209

24137

24848

25353

25723

26033

26334

4.8

21164

22310

23408

24314

25002

25491

25848

26149

26442

5.0

21398

22528

23607

24490

25156

25628

25973

26265

26549

5.2

21632

22747

23807

24665

25309

25764

26098

26381

26657

5.4

21867

22965

24006

24840

25460

25899

26222

26496

26764

5.6

22103

23184

24204

25013

25610

26033

26346

26611

26871

5.8

22339

23402

24402

25186

25759

26167

26469

26726

26977

6.0

22575

23620

24599

25357

25907

26299

26592

26840

27083

6.2

22812

23838

24794

25527

26053

26431

26714

26954

27188

6.4

23049

24055

24988

25695

26199

26561

26835

27067

27292

6.6

23286

24271

25181

25862

26342

26691

26955

27179

27396

6.8

23523

24487

25372

26026

26485

26819

27074

27290

27499

7.0

23761

24701

25561

26189

26626

26947

27192

27400

27601

Original

07-14-08

08.01.265

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

23998

24915

25748

26351

26766

27073

27310

27510

27703

7.4

24235

25128

25935

26512

26906

27200

27427

27619

27804

7.6

24472

25340

26120

26672

27045

27325

27544

27728

27905

7.8

24708

25552

26305

26831

27183

27450

27660

27836

28005

8.0

24945

25763

26489

26989

27322

27576

27776

27944

28105

8.2

25181

25973

26672

27148

27460

27701

27892

28052

28205

8.4

25416

26184

26856

27306

27598

27826

28008

28160

28305

8.6

25551

26394

27039

27465

27737

27952

28125

28268

28404

8.8

25886

26604

27223

27624

27877

28078

28241

28376

28504

9.0

26120

26813

27406

27784

28016

28204

28358

28484

28604

9.2

26353

27022

27589

27943

28156

28330

28474

28592

28704

9.4

26586

27230

27772

28102

18296

28456

28591

28700

28803

9.6

26819

27437

27953

28260

28436

28582

28707

28808

28902

9.8

27051

27643

28133

28417

28575

28708

28823

28915

29001

10.0

27282

27847

28311

28573

28714

28833

28938

29021

29099

10.2

27513

28050

28487

28728

28851

28958

29052

29127

29196

10.4

27743

28252

28661

28880

28988

29082

29166

29232

29293

10.6

27972

28451

28832

29030

29123

29204

29278

29335

29389

10.8

28201

28649

29000

29178

29257

29326

29389

29438

29483

11.0

28429

28844

29165

29324

29389

29447

29499

29539

29577

11.2

28656

29038

29327

29467

29520

29566

29608

29640

29670

11.4

28881

29229

29488

29608

29650

29685

29716

29739

29762

08.01.266

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.6

29104

29418

29645

29748

29779

29802

29823

29838

29854

11.8

29325

29605

29801

29886

29906

29919

29930

29936

29945

12.0

29544

29789

29955

30023

30033

30035

30036

30034

30035

12.2

29760

29972

30108

30159

30158

30150

30141

30131

30125

12.4

29972

30151

30259

30293

30283

30264

30245

30228

30215

12.6

30181

30329

30409

30427

30407

30378

30350

30324

30305

12.8

30386

30504

30558

30560

30530

30491

30453

30420

30394

13.0

30588

30677

30705

30693

30653

30604

30557

30516

30484

13.2

30786

30847

30853

30825

30775

30716

30660

30612

30573

13.4

30982

31017

30999

30956

30896

30828

30763

30708

30662

13.6

31176

31184

31144

31088

31017

30939

30865

30803

30751

13.8

31368

31351

31289

31218

31137

31050

30967

30898

30839

14.0

31558

31516

31434

31348

31257

31160

31068

30993

30927

14.2

31748

31681

31578

31478

31376

31270

31169

31087

31015

14.4

31936

31846

31722

31607

31495

31379

31270

31181

31102

14.6

32125

32010

31865

31736

31614

31488

31370

31274

31189

14.8

32313

32174

32009

31865

31732

31596

31470

31367

31276

15.0

32501

32338

32151

31993

31850

31704

31569

31459

31362

15.2

32688

32501

32294

32121

31967

31811

31668

31551

31447

15.4

32874

32663

32435

32247

32083

31918

31766

31642

31532

15.6

33057

32823

32575

32373

32198

32024

31864

31733

31617

15.8

33239

32982

32714

32498

32313

32129

31961

31823

31701

Original

07-14-08

08.01.267

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.0

33417

33138

32851

32621

32426

32233

32057

31912

31784

16.2

33592

33291

32986

32743

32538

32336

32152

32001

31867

16.4

33763

33441

33119

32864

32649

32438

32246

32089

31949

16.6

22930

33588

33250

32983

32759

32539

32339

32176

32030

16.8

34092

33730

33378

33100

32867

32639

32432

32263

32111

17.0

34249

33870

33504

33215

32974

32738

32524

32349

32192

17.2

34402

34006

33627

33329

33079

32835

32614

32434

32272

FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

18210

19509

20810

21968

22949

23727

24330

24789

25186

3.2

18436

19726

21017

22164

23130

23883

24465

24912

25299

3.4

18662

19943

21224

22358

23309

24039

24599

25033

25412

3.6

18889

20160

21432

22553

23488

24194

24733

25155

25525

3.8

19117

20378

21639

22746

23665

24348

24866

25276

25638

4.0

19345

20596

21846

22939

23841

24502

24999

25397

25750

4.2

19574

20815

22053

23131

24016

24653

25132

25518

25862

08.01.268

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

4.4

19804

21034

22260

23321

24188

24804

25263

25638

25973

4.6

20035

21253

22466

23511

24359

24953

25394

25757

26083

4.8

20268

21473

22672

23699

24526

25101

25524

25876

26193

5.0

20501

21694

22878

23886

24692

25247

25653

25995

26303

5.2

20736

21916

23084

24071

24856

25391

25782

26113

26412

5.4

20971

22138

23290

24255

25017

25534

25910

26230

26520

5.6

21208

22360

23495

24438

25177

25676

26037

26348

26628

5.8

21447

22583

23699

24619

25334

25816

26164

26464

26736

6.0

21686

22806

23903

24800

25490

25956

26290

26581

26844

6.2

21927

23030

24107

24979

25645

26094

26416

26697

26951

6.4

22169

23254

24310

25156

25798

26231

26542

26813

27059

6.6

22413

23478

24512

25333

25950

26368

26667

26929

27166

6.8

22658

23702

24714

25509

26101

26504

26793

27045

27273

7.0

22904

23927

24915

25683

26251

26640

26918

27161

27380

7.2

23151

24153

25116

25857

26400

26775

27043

27277

27487

7.4

23399

24378

25318

26031

26548

26909

27167

27392

27595

7.6

23648

24605

25519

26204

26696

27043

27292

27508

27702

7.8

23899

24832

25721

26377

26844

27177

27417

27623

27809

8.0

24150

25060

25923

26551

26991

27311

27542

27739

27916

8.2

24402

25288

26127

26724

27139

27445

27667

27854

28023

8.4

24654

25518

26332

26899

27287

27579

27791

27970

28130

8.6

24908

25749

26538

27074

27436

27713

27916

28086

28237

Original

07-14-08

08.01.269

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

8.8

25162

25980

26745

27250

27585

27847

28041

28201

28343

9.0

25416

26212

26953

27426

27734

27981

28166

28317

28450

9.2

25669

26444

27161

27603

27884

28115

28291

28432

28555

9.4

25922

26675

27369

27778

28033

28249

28415

28546

28661

9.6

26174

26904

27574

27953

28181

28382

28538

28660

28765

9.8

26425

27132

27777

28126

28328

28514

28661

28773

28869

10.0

26673

27356

27977

28296

28475

28645

28782

28885

28972

10.2

26919

27578

28172

28464

28619

28775

28902

28995

29074

10.4

27163

27795

28363

28628

28762

28903

29020

29104

29174

10.6

27403

28008

28547

28788

28902

29030

29136

29212

29273

10.8

27639

28216

28725

28944

29040

29155

29251

29318

29371

11.0

27873

28419

28898

29096

29175

29278

29363

29422

29467

11.2

28104

28618

29065

29244

29309

29399

29474

29525

29562

11.4

28333

28814

29229

29390

29441

29520

29584

29626

29656

11.6

28561

29008

29389

29534

29572

29639

29693

29727

29750

11.8

28787

29200

29547

29676

29703

29759

29802

29828

29843

12.0

29013

29391

29704

29817

29833

29877

29910

29928

29936

12.2

29239

29582

29861

29958

29963

29996

30018

30028

30029

12.4

29466

29773

30018

30099

30093

30115

30127

30129

30123

12.6

29694

29965

30177

30241

30225

30235

30236

30230

30217

12.8

29923

30158

30337

30384

30357

30356

20346

29331

30311

13.0

30154

30353

30500

30529

30491

30477

30457

29434

30406

08.01.270

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

13.2

30385

30549

30664

30674

30624

30598

30569

30536

30502

13.4

30616

30745

30829

30820

30758

30720

30680

30639

30597

13.6

30847

30941

30994

30966

30892

30841

30791

30742

30693

13.8

31076

31136

31159

31111

31026

30962

30902

30844

30788

14.0

31305

31331

31323

31256

31158

31082

31012

30946

30882

14.2

31531

31523

31486

31400

31290

31201

31122

31047

30976

14.4

31754

31714

31647

31542

31420

31319

31230

31146

31068

14.6

31975

31902

31806

31682

31548

31435

31336

31245

31160

14.8

32192

32087

31962

31820

31673

31549

31441

31342

31250

15.0

32405

32269

32116

31955

31797

31662

31544

31437

31338

15.2

32614

32448

32267

32089

31919

31773

31646

31532

31426

15.4

32819

32623

32415

32221

32040

31883

31746

31625

31512

15.6

33020

32796

32562

32351

32158

31992

31846

31717

31598

15.8

33217

32965

32706

32479

32275

32099

31944

31808

31683

16.0

33409

33131

32847

32606

32391

32205

32041

31899

31767

16.2

33597

33294

32987

32731

32506

32311

32138

31989

31851

16.4

33780

33453

33125

32855

32619

32415

32234

32079

31935

16.6

33958

33609

33261

32978

32732

32519

32330

32168

32018

16.8

34131

33761

33396

33099

32843

32622

32426

32257

32102

17.0

34300

33911

33529

33220

32954

32725

32521

32346

32185

17.2

34465

34057

33660

33339

33065

32827

32616

32435

32269

Original

07-14-08

08.01.271

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

17272

18597

19939

21164

22238

23156

23896

24453

24915

3.2

17499

18817

20151

21367

22425

23320

24038

24580

25030

3.4

17727

19037

20364

21569

22612

23484

24180

24707

25146

3.6

17956

19257

20577

21771

22798

23648

24322

24833

25261

3.8

18185

19478

20789

21973

22984

23811

24464

24960

25376

4.0

18416

19700

21002

22174

23168

23974

24605

25086

25491

4.2

18648

19922

21215

22374

23351

24135

24745

25211

25606

4.4

18882

20145

21428

22574

23534

24295

24885

25336

25720

4.6

19118

20370

21641

22773

23714

24454

25024

25461

25834

4.8

19355

20595

21854

22971

23894

24612

25162

25585

25947

5.0

19595

20822

22067

23168

24072

24769

25299

25708

26060

5.2

19836

21049

22280

23364

24249

24925

25436

25832

26172

5.4

20079

21278

22493

23559

24424

25079

25572

25954

26284

5.6

20324

21507

22706

23754

24599

25233

25708

26076

26396

5.8

20569

21736

22919

23948

24772

25386

25843

26198

26508

6.0

20816

21967

23132

24141

24944

25538

25977

26320

26619

6.2

21063

22198

23345

24334

25115

25689

26112

26442

26730

6.4

21311

22429

23558

24526

25286

25840

26246

26563

26842

6.6

21560

22660

23771

24717

25456

25990

26379

26685

26953

6.8

21809

22892

23984

24908

25625

26139

26513

26806

27064

7.0

22058

23124

24196

25099

25793

26288

26646

26927

27175

08.01.272

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

22308

23356

24409

25289

25961

26436

26779

27048

27286

7.4

22559

23589

24622

25478

26127

26584

26912

27169

27397

7.6

22811

23823

24835

25668

26293

26731

27044

27290

27508

7.8

23064

24058

25048

25856

26458

26877

27176

27411

27619

8.0

23319

24293

25262

26044

26622

27023

27308

27532

27730

8.2

23575

24530

25476

26232

26785

27168

27439

27652

27840

8.4

23832

24768

25691

26420

26947

27311

27570

27772

27950

8.6

24092

25007

25906

26607

27108

27454

27700

27892

28060

8.8

24353

25248

26122

26793

27268

27596

27829

28011

28170

9.0

24616

25489

26338

26979

27427

27737

27958

28130

28279

9.2

24880

25731

26554

27164

27585

27876

28087

28248

28388

9.4

25144

25973

26769

27348

27741

28015

28214

28366

28497

9.6

25408

26214

26983

27531

27896

28153

28341

28484

28605

9.8

25672

26454

27196

27713

28050

28290

28467

28600

28712

10.0

25935

26693

27406

27893

28203

28425

28592

28716

28819

10.2

26197

26929

27615

28071

28355

28560

28716

28831

28925

10.4

26456

27163

27820

28246

28505

28694

28839

28946

29031

10.6

26713

27393

28022

28420

28654

28827

28961

29059

29135

10.8

26967

27620

28221

28591

28802

28959

29083

29171

29239

11.0

27219

27843

28416

28760

28949

29091

29203

29282

29342

11.2

27468

28064

28609

28926

29094

29221

29322

29393

29445

11.4

27716

28282

28798

29091

29239

29351

29441

29502

29547

Original

07-14-08

08.01.273

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.6

27962

28499

28986

29254

29383

29480

29559

29611

29648

11.8

28208

28713

29172

29416

29525

29609

29676

29719

29748

12.0

28453

28927

29356

29576

29668

29737

29793

29827

29848

12.2

28698

29140

29539

29736

29810

29864

29909

29934

29948

12.4

28943

29353

29721

29895

29951

29992

30025

30041

30047

12.6

29190

29567

29903

30053

30092

30119

30141

30148

30146

12.8

29437

29781

30085

30211

30233

30246

30257

30255

30244

13.0

29685

29995

30266

30369

30373

30373

30372

30361

30342

13.2

29934

30209

30447

30526

30513

30499

30487

30466

30440

13.4

30182

30423

30627

30682

30653

30625

30602

30572

30537

13.6

30429

30636

30806

30837

30791

30750

30715

30677

30634

13.8

30676

30848

30984

30991

30929

30874

30829

30781

30730

14.0

30920

31058

31160

31143

31066

30998

30941

30885

30825

14.2

31163

31266

31334

31294

31201

31120

31053

30987

30920

14.4

31402

31471

31506

31444

31335

31242

31164

31089

31014

14.6

31639

31673

31676

31591

31468

31362

31274

31191

31107

14.8

31872

31873

31843

31736

31599

31481

31382

31291

31200

15.0

32102

32069

32007

31880

31728

31599

31490

31390

31292

15.2

32328

32262

32169

32021

31857

31716

31596

31489

31383

15.4

32552

32453

32329

32161

31983

31831

31702

31586

31474

15.6

32773

32641

32487

32300

32109

31946

31807

31683

31564

15.8

32991

32827

32643

32437

32233

32059

31911

31779

31654

08.01.274

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

16.0

33207

33011

32798

32572

32357

32172

32015

31875

31743

16.2

33421

33193

32952

32707

32480

32285

32117

31970

31831

16.4

33634

33374

33104

32841

32601

32396

32220

32065

31920

16.6

33845

33553

33255

32974

32723

32507

32322

32160

32008

16.8

34055

33731

33406

33107

32843

32617

32423

32254

32096

17.0

34263

33908

33555

33238

32963

32727

32524

32348

32183

17.2

34469

34084

33704

33370

33082

32837

32625

32441

32270

FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

16365

17712

19082

20343

21481

22511

23382

24027

24560

3.2

16593

17934

19297

20547

21669

22680

23529

24158

24678

3.4

16823

18156

19512

20751

21858

22848

23677

24289

24796

3.6

17054

18379

19727

20955

22047

23016

23824

24420

24914

3.8

17286

18603

19943

21160

22236

23184

23971

24551

25032

4.0

17520

18828

20159

21365

22425

23352

24119

24682

25150

4.2

17757

19055

20376

21570

22614

23520

24266

24813

25268

Original

07-14-08

08.01.275

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

4.4

17996

19283

20594

21775

22803

23688

24413

24944

25386

4.6

18238

19514

20813

21981

22993

23856

24559

25074

25504

4.8

18483

19746

21033

22188

23183

24024

24706

25205

25623

5.0

18731

19980

21254

22394

23373

24192

24853

25336

25741

5.2

18982

20216

21475

22601

23563

24359

24999

25467

25859

5.4

19234

20454

21698

22808

23753

24527

25145

25597

25978

5.6

19488

20692

21921

23016

23943

24694

25291

25728

26096

5.8

19742

20931

22144

23223

24132

24861

25436

25858

26214

6.0

19997

21170

22368

23431

24322

25027

25581

25988

26332

6.2

20253

21410

22592

23638

24511

25193

25726

26117

26449

6.4

20507

21649

22815

23845

24700

25359

25871

26247

26567

6.6

20761

21888

23039

24052

24889

25524

26015

26376

26684

6.8

21014

22127

23263

24258

25077

25689

26158

26505

26801

7.0

21266

22365

23486

24464

25264

25853

26301

26633

26917

7.2

21518

22603

23709

24670

25450

26015

26443

26761

27033

7.4

21769

22841

23932

24874

25635

26177

26585

26888

27149

7.6

22021

23078

24154

25077

25818

26338

26726

27015

27264

7.8

22274

23317

24376

25279

25999

26497

26865

27141

27379

8.0

22528

23555

24597

25480

26178

26654

27004

27266

27493

8.2

22784

23795

24818

25678

26355

26809

27141

27391

27606

8.4

23041

24035

25038

25875

26529

26962

27278

27515

27719

8.6

23302

24276

25258

26070

26700

27113

27412

27638

27832

08.01.276

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

8.8

23565

24518

25476

26263

26868

27262

27546

27760

27944

9.0

23830

24762

25694

26453

27033

27408

27678

27881

28055

9.2

24098

25007

25912

26642

27196

27552

27809

28002

28166

9.4

24368

25252

26129

26830

27357

27695

27940

28123

28277

9.6

24639

25499

26347

27018

27517

27838

28070

28243

28388

9.8

24912

25746

26565

27205

27676

27979

28200

28363

28499

10.0

25186

25994

26784

27392

27835

28121

28329

28483

28610

10.2

25460

26242

27003

27579

27993

28262

28459

28604

28721

10.4

25735

26491

27223

27767

28153

28405

28590

28725

28833

10.6

26010

26740

27444

27956

28314

28548

28722

28846

28945

10.8

26285

26989

27667

28147

28476

28692

28854

28969

29059

11.0

26559

27238

27891

28338

28639

28838

28987

29091

29172

11.2

26832

27487

28114

28530

28803

28984

29121

29214

29286

11.4

27105

27735

28337

28722

28967

29130

29254

29337

29400

11.6

27377

27982

28559

28913

29131

29276

29387

29459

29513

11.8

27648

28227

28780

29102

29294

29421

29519

29580

29625

12.0

27918

28471

28998

29290

29455

29565

29649

29700

29736

12.2

28186

28712

29213

29475

29615

29708

29779

29819

29845

12.4

28453

28951

29424

29657

29773

29848

29906

29936

29953

12.6

28719

29187

29631

29835

29927

29986

30031

30050

30059

12.8

28982

29420

29834

30010

30079

30121

30153

30162

30162

Original

07-14-08

08.01.277

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FOUR (WSTA 603.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

13.0

29244

29650

30032

30180

30227

30253

30273

30272

30263

13.2

29504

29877

30226

30347

30373

30384

30391

30380

30362

13.4

29762

30101

30417

30511

30516

30512

30507

30487

30460

13.6

30018

30323

30604

30673

30658

30639

30621

30592

30556

13.8

30272

30542

30788

30832

30797

30765

30735

30696

30652

14.0

30524

30759

30969

30989

30936

30889

30847

30800

30747

14.2

30774

30974

31148

31144

31074

31013

30960

30903

30842

14.4

31023

31187

31326

31298

31211

31137

31072

31006

30937

14.6

31269

31398

31502

31451

31348

31261

31184

31109

31032

14.8

31513

31607

31677

31604

31485

31385

31297

31213

31128

15.0

31756

31815

31851

31756

31622

31509

31410

31318

31224

15.2

31998

32021

32024

31908

31760

31634

31524

31422

31321

15.4

32239

32227

32197

32060

31897

31758

31637

31527

31418

15.6

32480

32433

32369

32211

32034

31883

31751

31632

31516

15.8

32722

32639

32541

32362

32171

32007

31865

31737

31613

16.0

32965

32845

32712

32513

32308

32131

31978

31841

31710

16.2

33209

33051

32884

32664

32444

32255

32091

31946

31807

16.4

33456

33259

33056

32814

32580

32379

32204

32049

31903

16.6

33705

33468

33228

32965

32716

32502

32316

32153

31998

16.8

33956

33679

33401

33115

32852

32624

32427

32255

32093

17.0

34209

33890

33574

33265

32986

32746

32537

32357

32187

17.2

34461

34101

33745

33414

33120

32867

32647

32457

32281

08.01.278

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

30304

30815

31181

31506

31778

32010

32189

32314

32479

3.2

30435

30935

31292

31608

31870

32091

32262

32384

32546

3.4

30566

31054

31403

31709

31962

32173

32336

32455

32614

3.6

30697

31174

31513

31810

32053

32254

32410

32525

32680

3.8

30828

31294

31623

31910

32143

32335

32483

32595

32747

4.0

30960

31413

31733

32009

32233

32416

32557

32665

32814

4.2

31092

31532

31841

32107

32322

32496

32631

32736

32880

4.4

31225

31651

31950

32204

32409

32576

32705

32806

32946

4.6

31358

31770

32057

32300

32496

32655

32780

32876

33011

4.8

31491

31889

32163

32395

32581

32735

32854

32947

33076

5.0

31625

32007

32269

32488

32665

32813

32929

33017

33141

5.2

31759

32124

32374

32581

32748

32892

33004

33088

33205

5.4

31892

32241

32477

32672

32831

32970

33078

33158

33269

5.6

32025

32357

32580

32762

32913

33047

33153

33227

33332

5.8

32158

32473

32682

32852

32994

33125

33227

33297

33395

6.0

32289

32587

32782

32941

33076

33202

33301

33366

33458

6.2

32419

32699

32882

33030

33158

33279

33374

33434

33520

6.4

32547

32811

32980

33119

33239

33356

33446

33502

33581

6.6

32674

32920

33077

33207

33322

33433

33518

33568

33643

6.8

32798

33028

33173

33296

33405

33510

33589

33634

33703

7.0

32921

33135

33267

33384

33489

33587

33659

33700

33764

Original

07-14-08

08.01.279

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

33041

33240

33361

33472

33573

33663

33728

33764

33824

7.4

30160

33344

33454

33561

33657

33739

33797

33828

33884

7.6

33278

33447

33547

33649

33740

33815

33865

33892

33943

7.8

33394

33549

33640

33737

33824

33890

33933

33955

34003

8.0

33508

33651

33732

33824

33906

33965

34000

34018

34063

8.2

33621

33752

33826

33912

33988

34039

34066

34082

34123

8.4

33733

33854

33919

33999

34069

34111

34133

34145

34183

8.6

33843

33955

34013

34086

34148

34183

34199

34208

34243

8.8

33953

34056

34109

34173

34226

34254

34265

34272

34304

9.0

34061

34158

34204

34259

34302

34323

34331

34335

34365

9.2

34169

34259

34300

34344

34377

34392

34396

34399

34426

9.4

34277

34360

34396

34429

34451

34461

34462

34463

34487

9.6

34384

34461

34492

34513

34525

34528

34527

34527

34547

9.8

34491

34561

34586

34596

34597

34596

34592

34590

34608

10.0

34598

34661

34680

34679

34669

34663

34658

34654

34668

10.2

34705

34759

34772

34760

34741

34731

34723

34717

34727

10.4

34813

34857

34862

34840

34812

34798

34789

34780

34785

10.6

34921

34954

34950

34919

34884

34866

34854

34842

34842

10.8

35030

35050

35035

34996

34956

34935

34920

34904

34899

11.0

35139

35144

35118

35072

35028

35003

34985

34965

34954

11.2

35248

35237

35199

35147

35100

35072

35051

35025

35009

11.4

35356

35329

35279

35222

35172

35141

35116

35085

35063

08.01.280

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.6

35464

35420

35357

35295

35244

35210

35181

35145

35116

11.8

35570

35510

35435

35369

35316

35279

35245

35204

35169

12.0

35675

35599

35512

35442

35388

35347

35309

35263

35222

12.2

35778

35687

35589

35515

35459

35415

35372

35321

35275

12.4

35878

35774

35666

35589

35531

35482

35434

35378

35327

12.6

35975

35860

35743

35663

35602

35549

35495

35436

35380

12.8

36069

35945

35822

35737

35673

35614

35556

35492

35434

13.0

36161

36029

35900

35812

35744

35678

35615

35549

35488

13.2

36250

36113

35980

35887

35814

35742

35673

35605

35542

13.4

36337

36195

36059

35963

35884

35805

35731

35661

35596

13.6

36422

36278

36139

36038

35953

35867

35788

35716

35650

13.8

36507

36360

36219

36113

36021

35929

35845

35772

35704

14.0

36591

36441

36298

36187

36089

35990

35901

35827

35758

14.2

36675

36522

36377

36260

36156

36051

35958

35882

35812

14.4

36759

36604

36456

36333

36222

36112

36015

35938

35865

14.6

36845

36685

36534

36404

36287

36172

36072

35993

35919

14.8

36931

36766

36610

36474

36351

36232

36130

36049

35971

15.0

37019

36848

36686

36543

36415

36293

36188

36104

36023

15.2

37107

36929

36761

36611

36477

36353

36246

36160

36075

Original

07-14-08

08.01.281

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

29824

30434

30883

31251

31556

31808

32001

32146

32329

3.2

29967

30566

31005

31360

31652

31893

32079

32221

32400

3.4

30111

30697

31126

31468

31747

31978

32157

32295

32472

3.6

30255

30829

31246

31576

31842

32063

32235

32370

32543

3.8

30400

30960

31365

31682

31937

32148

32314

32445

32613

4.0

30545

31091

31484

31788

32031

32233

32392

32519

32684

4.2

30691

31221

31601

31892

32124

32317

32471

32594

32753

4.4

30838

31351

31717

31995

32216

32402

32550

32668

32822

4.6

30986

31481

31831

32096

32307

32486

32629

32742

32891

4.8

31135

31610

31944

32196

32397

32570

32708

32817

32959

5.0

31285

31739

32055

32294

32487

32654

32787

32891

33026

5.2

31435

31866

32164

32390

32575

32737

32867

32964

33092

5.4

31584

31993

32273

32486

32663

32821

32946

33038

33158

5.6

31733

32119

32379

32580

32750

32904

33025

33111

33223

5.8

31880

32243

32485

32674

32837

32987

33104

33183

33288

6.0

32025

32366

32590

32767

32924

33069

33181

33255

33353

6.2

32168

32487

32693

32861

33011

33151

33258

33326

33417

6.4

32308

32606

32796

32954

33098

33233

33335

33397

33481

6.6

32445

32723

32898

33047

33185

33314

33410

33466

33544

6.8

32578

32838

33000

33141

33273

33395

33484

33535

33608

7.0

32708

32950

33101

33235

33362

33475

33557

33603

33671

08.01.282

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

32834

33062

33202

33329

33450

33555

33629

33670

33734

7.4

32958

33171

33302

33423

33538

33635

33700

33737

33797

7.6

33080

33280

33402

33518

33626

33713

33770

33803

33860

7.8

33199

33388

33502

33612

33713

33791

33840

33869

33923

8.0

33318

33495

33602

33705

33800

33868

33910

33935

33986

8.2

33435

33602

33701

33799

33885

33945

33979

34001

34049

8.4

33552

33709

33801

33891

33969

34021

34048

34066

34112

8.6

33669

33816

33902

33983

34052

34095

34117

34133

34175

8.8

33786

33924

34002

34074

34133

34169

34186

34199

34238

9.0

33903

34032

34103

34164

34213

34242

34255

34266

34302

9.2

34021

34140

34203

34254

34292

34314

34324

34333

34365

9.4

34138

34248

34303

34342

34369

34386

34393

34399

34428

9.6

34256

34355

34403

34429

34446

34457

34462

34466

34490

9.8

34373

34463

34501

34516

34522

34528

34531

34533

34553

10.0

34490

34569

34598

34601

34597

34599

34601

34599

34614

10.2

34608

34674

34694

34686

34673

34670

34669

34665

34675

10.4

34725

34779

34787

34769

34748

34742

34738

34731

34736

10.6

34841

34881

34879

34852

34824

34813

34807

34795

34795

10.8

34958

34983

34969

34933

34899

34885

34875

34860

34854

11.0

35074

35082

35056

35013

34976

34958

34944

34923

34912

11.2

35189

35181

35142

35093

35052

35030

35011

34986

34969

11.4

35303

35277

35227

35172

35129

35103

35079

35049

35026

Original

07-14-08

08.01.283

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.6

35415

35373

35310

35251

35205

35175

35146

35110

35082

11.8

35526

35468

35393

35329

35281

35247

35212

35172

35138

12.0

35635

35561

35475

35408

35357

35318

35278

35233

35194

12.2

35742

35654

35558

35486

35433

35389

35343

35293

35250

12.4

35847

35746

35641

35564

35508

35459

35408

35353

35306

12.6

35949

35837

35724

35643

35582

35528

35471

35413

35362

12.8

36048

35928

35809

35722

35656

35595

35534

35473

35419

13.0

36145

36018

35894

35802

35729

35662

35595

35532

35476

13.2

36240

36107

35979

35881

35801

35728

35657

35591

35533

13.4

36333

36196

36065

35960

35873

35793

35717

35650

35590

13.6

36425

36285

36150

36039

35944

35857

35777

35709

35647

13.8

36517

36373

36236

36118

36014

35921

35837

35767

35704

14.0

36608

36461

36320

36196

36084

35984

35897

35826

35760

14.2

36699

36548

36404

36272

36152

36047

35957

35884

35817

14.4

36792

36636

36487

36348

36220

36110

36017

35942

35872

14.6

36885

36723

36568

36422

36288

36174

36078

36000

35927

14.8

36979

36810

36648

36494

36355

36237

36139

36058

35982

15.0

37075

36896

36726

36566

36421

36300

36200

36116

36035

15.2

37171

36982

36803

36635

36486

36364

36261

36174

36088

08.01.284

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE =-1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

29242

29979

30546

30994

31343

31625

31848

32020

32223

3.2

29403

30126

30680

31109

31442

31713

31930

32099

32298

3.4

29563

30272

30813

31224

31541

31802

32012

32177

32373

3.6

29724

30418

30945

31338

31639

31890

32095

32256

32447

3.8

29886

30564

31075

31452

31737

31979

32177

32334

32521

4.0

30049

30709

31204

31563

31835

32067

32260

32412

32594

4.2

30213

30853

31331

31674

31932

32156

32342

32490

32666

4.4

30377

30997

31455

31783

32029

32245

32426

32568

32737

4.6

30543

31139

31577

31889

32125

32334

32509

32645

32808

4.8

30711

31281

31697

31994

32220

32423

32592

32722

32877

5.0

30879

31421

31814

32097

32315

32512

32676

32798

32945

5.2

31047

31561

31929

32199

32409

32601

32760

32874

33013

5.4

31214

31698

32042

32299

32503

32690

32843

32950

33079

5.6

31380

31835

32153

32398

32596

32779

32926

33025

33146

5.8

31544

31969

32263

32497

32690

32867

33008

33099

33211

6.0

31705

32101

32372

32595

32783

32955

33090

33173

33277

6.2

31862

32232

32481

32694

32876

33042

33170

33246

33342

6.4

32016

32360

32589

32793

32969

33128

33249

33318

33407

6.6

32164

32486

32698

32892

33062

33214

33327

33389

33473

6.8

32308

32609

32806

32992

33156

33298

33403

33460

33538

7.0

32446

32730

32915

33093

33249

33382

33478

33530

33604

Original

07-14-08

08.01.285

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE =-1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

32581

32850

33024

33194

33343

33465

33552

33600

33670

7.4

32712

32967

33133

33295

33436

33547

33624

33669

33736

7.6

32840

33084

33242

33396

33528

33628

33696

33738

33803

7.8

32966

33200

33351

33497

33619

33708

33768

33806

33869

8.0

33092

33315

33459

33598

33710

33788

33839

33874

33935

8.2

33216

33430

33568

33697

33799

33867

33910

33943

34001

8.4

33341

33544

33676

33795

33887

33946

33982

34011

34066

8.6

33467

33660

33784

33892

33973

34023

34053

34080

34132

8.8

33594

33776

33891

33988

34058

34101

34126

34149

34197

9.0

33723

33892

33997

34082

34141

34177

34198

34218

34261

9.2

33852

34009

34103

34174

34222

34254

34271

34288

34326

9.4

33982

34125

34208

34266

34303

34330

34344

34357

34389

9.6

34112

34241

34311

34356

34383

34406

34418

34426

34453

9.8

34243

34356

34414

34445

34462

34481

34491

34495

34516

10.0

34373

34470

34515

34534

34541

34557

34564

34563

34578

10.2

34502

34583

34614

34621

34620

34632

34636

34631

34640

10.4

34630

34695

34712

34708

34700

34707

34708

34698

34701

10.6

34756

34804

34808

34795

34780

34783

34780

34765

34761

10.8

34881

34911

34902

34881

34860

34859

34850

34830

34821

11.0

35004

35017

34994

34967

34942

34935

34920

34895

34881

11.2

35126

35121

35085

35052

35023

35010

34989

34959

34939

11.4

35245

35223

35175

35137

35105

35086

35058

35022

34998

08.01.286

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE =-1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.6

35363

35323

35264

35222

35187

35161

35125

35085

35056

11.8

35478

35423

35353

35306

35268

35235

35193

35147

35114

12.0

35591

35522

35442

35391

35349

35309

35259

35209

35173

12.2

35703

35619

35530

35475

35429

35382

35325

35271

35231

12.4

35812

35717

35620

35559

35508

35454

35390

35333

35289

12.6

35919

35813

35710

35643

35586

35525

35455

35394

35348

12.8

36024

35910

35801

35728

35663

35594

35519

35456

35407

13.0

36127

36007

35892

35811

35738

35663

35583

35518

35467

13.2

36229

36103

35984

35895

35812

35730

35646

35579

35526

13.4

36329

36199

36077

35978

35885

35797

35709

35641

35586

13.6

36429

36294

36169

36060

35957

35863

35773

35703

35646

13.8

36528

26389

36260

36142

36028

35929

35836

35764

35705

14.0

36628

36484

36350

36222

36099

35994

35899

35825

35763

14.2

36728

36578

36439

36302

36169

36060

35962

35886

35821

14.4

36828

36672

36526

36380

36238

36126

36025

35947

35879

14.6

36930

36765

36611

36456

36308

36192

36089

36007

35935

14.8

37033

36858

36694

36531

36377

36258

36153

36067

35990

15.0

37138

36950

36775

36605

36446

36325

36217

36127

36045

15.2

37242

37041

36853

36677

36515

36392

36282

36186

36098

Original

07-14-08

08.01.287

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

28503

29422

30155

30705

31109

31416

31659

31863

32083

3.2

28690

29587

30298

30827

31213

31510

31747

31946

32161

3.4

28877

29752

30441

30948

31317

31604

31835

32029

32238

3.6

29064

29916

30582

31068

31421

31697

31922

32112

32315

3.8

29251

30079

30722

31187

31524

31791

32010

32194

32391

4.0

29438

30241

30860

31305

31628

31885

32097

32276

32467

4.2

29625

30401

30996

31422

31731

31979

32185

32358

32542

4.4

29811

30560

31130

31538

31834

32074

32272

32438

32616

4.6

29998

30718

31261

31651

31937

32168

32359

32519

32689

4.8

30184

30873

31389

31763

32040

32263

32446

32598

32761

5.0

30370

31026

31515

31873

32142

32358

32533

32677

32832

5.2

30555

31177

31638

31982

32244

32453

32620

32755

32902

5.4

30737

31327

31759

32090

32346

32548

32706

32833

32971

5.6

30918

31474

31879

32197

32447

32642

32792

32910

33040

5.8

31095

31619

31998

32304

32548

32736

32876

32986

33109

6.0

31270

31762

32116

32410

32649

32829

32960

33062

33177

6.2

31440

31903

32234

32517

32749

32921

33043

33137

33245

6.4

31605

32042

32352

32623

32849

33012

33125

33212

33314

6.6

31766

32179

32470

32731

32948

33102

33206

33286

33383

6.8

31921

32313

32589

32839

33047

33190

33286

33360

33452

7.0

32072

32446

32709

32947

33145

33277

33364

33434

33522

08.01.288

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

32219

32577

32829

33056

33243

33364

33442

33507

33592

7.4

32352

32707

32949

33165

33339

33449

33519

33580

33662

7.6

32504

32835

33068

33273

33435

33533

33595

33653

33731

7.8

32643

32963

33188

33381

33530

33617

33671

33726

33801

8.0

32783

33090

33306

33488

33625

33700

33747

33798

33871

8.2

32922

33217

33424

33593

33718

33783

33823

33870

33940

8.4

33063

33344

33540

33697

33809

33866

33899

33943

34008

8.6

33205

33471

33655

33800

33900

33948

33976

34015

34076

8.8

33350

33598

33768

33899

33989

34030

34053

34088

34143

9.0

33497

33726

33880

33998

34078

34113

34131

34160

34209

9.2

33645

33854

33990

34094

34165

34195

34209

34233

34275

9.4

33794

33981

34098

34189

34252

34277

34287

34305

34339

9.6

33943

34107

34205

34283

34338

34359

34365

34376

34404

9.8

34091

34232

34310

34376

34424

34441

34443

34447

34467

10.0

34237

34355

34415

34468

34509

34522

34520

34518

34531

10.2

34382

34476

34518

34560

34595

34604

34596

34588

34593

10.4

34523

34596

34619

34651

34681

34685

34672

34657

34656

10.6

34661

34713

34720

34743

34767

34765

34746

34725

34718

10.8

34794

34827

34820

34835

34854

34845

34819

34792

34779

11.0

34924

34938

34918

34927

34942

34925

34890

34858

34841

11.2

35050

35048

35016

35020

35029

35004

34961

34923

34902

11.4

35173

35155

35114

35112

35117

35083

35031

34988

34963

Original

07-14-08

08.01.289

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.6

35294

35261

35210

35205

35204

35161

35099

35052

35024

11.8

35411

35365

35307

35297

35291

35238

35168

35116

35085

12.0

35527

35469

35404

35389

35376

35314

35235

35180

35146

12.2

35641

35572

35500

35480

35461

35389

35302

35243

35207

12.4

35754

35675

35597

35570

35544

35464

35369

35307

35268

12.6

35866

35778

35694

35660

35626

35537

35436

35371

35329

12.8

35978

35881

35791

35750

35706

35609

35503

35435

35391

13.0

36089

35984

35889

35838

35785

35680

35570

35499

35452

13.2

36200

36088

35986

35925

35862

35751

35636

35564

35514

13.4

36310

36191

36083

36012

35937

35820

35703

35628

35575

13.6

36421

36294

36180

36097

36012

35890

35770

35692

35636

13.8

36531

36397

36275

36181

36086

35959

35837

35757

35697

14.0

36641

36499

36369

36265

36160

36028

35903

35821

35757

14.2

36752

36601

36462

36347

36233

36097

35970

35884

35817

14.4

36862

36701

36553

36428

36306

36166

36037

35947

35876

14.6

36973

36800

36642

36508

36380

36235

36103

36010

35933

14.8

37084

36898

36728

36586

36453

36305

36169

36072

35990

15.0

37195

36995

36813

36664

36527

36376

36236

36133

36046

15.2

37306

37091

36896

36740

36601

36446

36302

36193

36102

08.01.290

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

27632

28763

29696

30359

30817

31158

31436

31673

31913

3.2

27847

28947

29848

30487

30927

31259

31531

31761

31993

3.4

28062

29130

30000

30614

31037

31360

31625

31849

32073

3.6

28276

29311

30151

30740

31147

31461

31720

31936

32153

3.8

28488

29492

30300

30866

31257

31562

31814

32022

32232

4.0

28700

29671

30447

30991

31367

31663

31907

32109

32310

4.2

28911

29847

30592

31115

31478

31764

32000

32194

32388

4.4

29120

30022

30735

31238

31589

31865

32093

32278

32464

4.6

29327

30194

30875

31360

31701

31966

32184

32362

32540

4.8

29533

30363

31012

31481

31813

32068

32275

32445

32616

5.0

29737

30529

31146

31601

31925

32169

32366

32526

32690

5.2

29938

30693

31278

31719

32037

32270

32455

32607

32763

5.4

30136

30854

31409

31837

32148

32371

32544

32687

32837

5.6

30332

31014

31538

31954

32260

32471

32632

32767

32909

5.8

30524

31171

31666

32071

32371

32570

32719

32846

32982

6.0

30713

31327

31794

32187

32481

32668

32805

32924

33054

6.2

30899

31481

31923

32303

32590

32766

32891

33002

33127

6.4

31080

31633

32052

32420

32698

32861

32975

33080

33200

6.6

31255

31784

32182

32536

32804

32956

33059

33158

33273

6.8

31429

31934

32314

32653

32909

33049

33142

33236

33347

7.0

31597

32083

32446

32770

33012

33140

33225

33315

33421

Original

07-14-08

08.01.291

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

31762

32231

32580

32887

33114

33230

33307

33392

33495

7.4

31925

32378

32713

33003

33215

33319

33388

33470

33570

7.6

32085

32524

32846

33118

33314

33408

33469

33548

33644

7.8

32247

32670

32978

33233

33413

33495

33551

33626

33718

8.0

32407

32814

33109

33346

33510

33583

33632

33703

33791

8.2

32568

32958

33238

33457

33607

33670

33713

33780

33863

8.4

32730

33101

33365

33567

33703

33758

33795

33857

33935

8.6

32894

33243

33489

33674

33798

33845

33878

33934

34005

8.8

33060

33385

33610

33779

33893

33934

33961

34010

34075

9.0

33229

33526

33727

33882

33987

34022

34044

34086

34143

9.2

33398

33666

33842

33983

34081

34111

34128

34162

34210

9.4

33567

33805

33955

34083

34175

34200

34211

34236

34276

9.6

33736

33942

34066

34181

34268

34289

34294

34311

34341

9.8

33902

34077

34175

34279

34362

34377

34377

34384

34406

10.0

34066

34210

34283

34376

34455

34465

34458

34457

34471

10.2

34226

34341

34389

34474

34549

34553

34538

34529

34535

10.4

34381

34468

34496

34571

34642

34639

34617

34601

34599

10.6

34531

34593

34602

34670

34736

34725

34694

34671

34664

10.8

34674

34715

34708

34769

34831

34810

34770

34741

34728

11.0

34812

34834

34814

34869

34925

34893

34843

34809

34793

11.2

34944

34950

34920

34969

35019

34976

34915

34877

34858

11.4

35073

35065

35026

35070

35113

35057

34986

34944

34923

08.01.292

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.6

35198

35178

35132

35170

35206

35138

35056

35011

34988

11.8

35321

35290

35238

35270

35298

35218

35126

35078

35053

12.0

35441

35401

35344

35370

35389

35297

35195

35145

35118

12.2

35561

35511

35450

35468

35479

35375

35264

35211

35183

12.4

35681

35622

35555

35565

35566

35452

35333

35278

35247

12.6

35801

35733

35660

35661

35652

35528

35402

35345

35312

12.8

35922

35845

35765

35754

35736

35604

35472

35412

35376

13.0

36045

35958

35870

35847

35817

35679

35543

35479

35439

13.2

36168

36070

35973

35937

35897

35753

35614

35547

35503

13.4

36292

36183

36076

36027

35976

35827

35685

35614

35565

13.6

36416

36295

36177

36115

36053

35901

35757

35682

35628

13.8

36540

36407

36278

36201

36131

35975

35828

35749

35690

14.0

36664

36517

36376

36287

36207

36048

35899

35815

35751

14.2

36786

36627

36473

36372

36284

36122

35970

35882

35812

14.4

36908

36734

36568

36456

36361

36195

36040

35947

35872

14.6

37028

36840

36660

36540

36439

36269

36110

36011

35931

14.8

37147

36943

36750

36622

36517

36343

36179

36075

35990

15.0

37264

37044

36838

36705

36597

36417

36247

36138

36047

15.2

37379

37143

36925

36787

36676

36491

36314

36200

36105

Original

07-14-08

08.01.293

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

26613

27987

29160

29934

30434

30843

31185

31468

31738

3.2

26850

28186

29321

30069

30553

30954

31288

31560

31819

3.4

27085

28383

29481

30203

30673

31064

31391

31653

31900

3.6

27320

28580

29640

30338

30792

31174

31493

31744

31981

3.8

27552

28775

29798

30472

30912

31284

31594

31835

32062

4.0

27783

28968

29955

30606

31032

31394

31695

31926

32143

4.2

28012

29159

30111

30739

31152

31503

31794

32015

32223

4.4

28238

29348

30265

30872

31273

31612

31892

32104

32302

4.6

28461

29534

30416

31005

31394

31721

31989

32191

32382

4.8

28681

29717

30566

31137

31515

31829

32084

32277

32460

5.0

28899

29898

30715

31268

31636

31937

32178

32362

32539

5.2

29113

30076

30861

31399

31757

32043

32271

32446

32617

5.4

29325

30252

31007

31529

31878

32149

32363

32530

32694

5.6

29535

30426

31152

31659

31998

32254

32453

32612

32772

5.8

29742

30599

31296

31788

32117

32358

32543

32695

32849

6.0

29947

30771

31439

31916

32234

32461

32633

32777

32926

6.2

30151

30942

31583

32044

32350

32563

32721

32859

33004

6.4

30353

31113

31727

32170

32464

32663

32810

32941

33081

6.6

30554

31283

31871

32296

32576

32762

32898

33023

33158

6.8

30753

31454

32017

32421

32686

32859

32986

33105

33236

7.0

30952

31625

32162

32546

32794

32955

33074

33188

33313

7.2

31149

31795

32308

32669

32899

33050

33162

33271

33390

08.01.294

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.4

31345

31965

32453

32791

33004

33144

33250

33354

33468

7.6

31541

32134

32597

32912

33107

33237

33338

33437

33544

7.8

31736

32302

32739

33031

33209

33330

33426

33519

33621

8.0

31930

32469

32880

33149

33310

33423

33514

33602

33696

8.2

32123

32634

33018

33265

33411

33516

33601

33683

33771

8.4

32316

32797

33153

33379

33511

33609

33689

33764

33845

8.6

32509

32957

33286

33492

33612

33702

33776

33845

33918

8.8

32701

33116

33414

33603

33713

33796

33863

33924

33989

9.0

32892

33271

33539

33712

33815

33890

33950

34003

34060

9.2

33081

33424

33661

33819

33916

33985

34037

34080

34129

9.4

33268

33575

33781

33926

34018

34080

34123

34157

34198

9.6

33452

33723

33900

34031

34119

34174

34208

34234

34267

9.8

33632

33869

34017

34137

34220

34268

34292

34309

34335

10.0

33808

34011

34133

34242

34321

34361

34376

34384

34403

10.2

33980

34152

34248

34347

34422

34453

34459

34459

34470

10.4

34145

34289

34364

34452

34522

34544

34540

34533

34538

10.6

34305

34424

34480

34559

34621

34634

34620

34606

34607

10.8

34458

34556

34598

34666

34720

34722

34698

34680

34676

11.0

34606

34686

34716

34774

34817

34809

34776

34752

34745

11.2

34749

34814

34834

34882

34914

34894

34852

34825

34815

11.4

34888

34941

34953

34990

35010

34978

34927

34897

34884

11.6

35024

35066

35072

35097

35105

35061

35002

34969

34954

11.8

35159

35190

35190

35204

35198

35143

35077

35040

35023

Original

07-14-08

08.01.295

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

12.0

35293

35313

35307

35309

35290

35224

35151

35112

35092

12.2

35428

35436

35423

35413

35381

35305

35225

35183

35161

12.4

35564

35560

35537

35515

35471

35386

35300

35254

35228

12.6

35702

35684

35649

35615

35559

35466

35375

35325

35295

12.8

35844

35808

35760

35712

35646

35546

35451

35397

35361

13.0

35987

35933

35868

35807

35731

35626

35527

35468

35426

13.2

36133

36058

35974

35900

35816

35706

35604

35538

35490

13.4

36279

36182

36079

35991

35899

35786

35680

35609

35554

13.6

36425

36305

36182

36081

35982

35866

35757

35679

35617

13.8

36570

36427

36283

36169

36065

35946

35833

35748

35679

14.0

36712

36547

36382

36257

36147

36025

35908

35817

35740

14.2

36852

36665

36481

36344

36230

36104

35983

35885

35802

14.4

36987

36780

36577

36432

36312

36183

36057

35953

35863

14.6

37118

36892

36673

36519

36396

36261

36129

36019

35923

14.8

37243

37001

36768

36607

36479

36339

36200

36084

35984

15.0

37363

37106

36861

36695

36564

36416

36270

36148

36044

15.2

37478

37208

36954

36783

36648

36493

36339

36212

36104

08.01.296

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

27632

28763

29696

30359

30817

31158

31436

31673

31913

3.2

27847

28947

29848

30487

30927

31259

31531

31761

31993

3.4

28062

29130

30000

30614

31037

31360

31625

31849

32073

3.6

28276

29311

30151

30740

31147

31461

31720

31936

32153

3.8

28488

29492

30300

30866

31257

31562

31814

32022

32232

4.0

28700

29671

30447

30991

31367

31663

31907

32109

32310

4.2

28911

29847

30592

31115

31478

31764

32000

32194

32388

4.4

29120

30022

30735

31238

31589

31865

32093

32278

32464

4.6

29327

30194

30875

31360

31701

31966

32184

32362

32540

4.8

29533

30363

31012

31481

31813

32068

32275

32445

32616

5.0

29737

30529

31146

31601

31925

32169

32366

32526

32690

5.2

29938

30693

31278

31719

32037

32270

32455

32607

32763

5.4

30136

30854

31409

31837

32148

32371

32544

32687

32837

5.6

30332

31014

31538

31954

32260

32471

32632

32767

32909

5.8

30524

31171

31666

32071

32371

32570

32719

32846

32982

6.0

30713

31327

31794

32187

32481

32668

32805

32924

33054

6.2

30899

31481

31923

32303

32590

32766

32891

33002

33127

6.4

31080

31633

32052

32420

32698

32861

32975

33080

33200

6.6

31255

31784

32182

32536

32804

32956

33059

33158

33273

6.8

31429

31934

32314

32653

32909

33049

33142

33236

33347

7.0

31597

32083

32446

32770

33012

33140

33225

33315

33421

Original

07-14-08

08.01.297

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

31762

32231

32580

32887

33114

33230

33307

33392

33495

7.4

31925

32378

32713

33003

33215

33319

33388

33470

33570

7.6

32085

32524

32846

33118

33314

33408

33469

33548

33644

7.8

32247

32670

32978

33233

33413

33495

33551

33626

33718

8.0

32407

32814

33109

33346

33510

33583

33632

33703

33791

8.2

32568

32958

33238

33457

33607

33670

33713

33780

33863

8.4

32730

33101

33365

33567

33703

33758

33795

33857

33935

8.6

32894

33243

33489

33674

33798

33845

33878

33934

34005

8.8

33060

33385

33610

33779

33893

33934

33961

34010

34075

9.0

33229

33526

33727

33882

33987

34022

34044

34086

34143

9.2

33398

33666

33842

33983

34081

34111

34128

34162

34210

9.4

33567

33805

33955

34083

34175

34200

34211

34236

34276

9.6

33736

33942

34066

34181

34268

34289

34294

34311

34341

9.8

33902

34077

34175

34279

34362

34377

34377

34384

34406

10.0

34066

34210

34283

34376

34455

34465

34458

34457

34471

10.2

34226

34341

34389

34474

34549

34553

34538

34529

34535

10.4

34381

34468

34496

34571

34642

34639

34617

34601

34599

10.6

34531

34593

34602

34670

34736

34725

34694

34671

34664

10.8

34674

34715

34708

34769

34831

34810

34770

34741

34728

11.0

34812

34834

34814

34869

34925

34893

34843

34809

34793

11.2

34944

34950

34920

34969

35019

34976

34915

34877

34858

11.4

35073

35065

35026

35070

35113

35057

34986

34944

34923

11.6

35198

35178

35132

35170

35206

35138

35056

35011

34988

08.01.298

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.8

35321

35290

35238

35270

35298

35218

35126

35078

35053

12.0

35441

35401

35344

35370

35389

35297

35195

35145

35118

12.2

35561

35511

35450

35468

35479

35375

35264

35211

35183

12.4

35681

35622

35555

35565

35566

35452

35333

35278

35247

12.6

35801

35733

35660

35661

35652

35528

35402

35345

35312

12.8

35922

35845

35765

35754

35736

35604

35472

35412

35376

13.0

36045

35958

35870

35847

35817

35679

35543

35479

35439

13.2

36168

36070

35973

35937

35897

35753

35614

35547

35503

13.4

36292

36183

36076

36027

35976

35827

35685

35614

35565

13.6

36416

36295

36177

36115

36053

35901

35757

35682

35628

13.8

36540

36407

36278

36201

36131

35975

35828

35749

35690

14.0

36664

36517

36376

36287

36207

36048

35899

35815

35751

14.2

36786

36627

36473

36372

36284

36122

35970

35882

35812

14.4

36908

36734

36568

36456

36361

36195

36040

35947

35872

14.6

37028

36840

36660

36540

36439

36269

36110

36011

35931

14.8

37147

36943

36750

36622

36517

36343

36179

36075

35990

15.0

37264

37044

36838

36705

36597

36417

36247

36138

36047

15.2

37379

37143

36925

36787

36676

36491

36314

36200

36105

Original

07-14-08

08.01.299

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

26613

27987

29160

29934

30434

30843

31185

31468

31738

3.2

26850

28186

29321

30069

30553

30954

31288

31560

31819

3.4

27085

28383

29481

30203

30673

31064

31391

31653

31900

3.6

27320

28580

29640

30338

30792

31174

31493

31744

31981

3.8

27552

28775

29798

30472

30912

31284

31594

31835

32062

4.0

27783

28968

29955

30606

31032

31394

31695

31926

32143

4.2

28012

29159

30111

30739

31152

31503

31794

32015

32223

4.4

28238

29348

30265

30872

31273

31612

31892

32104

32302

4.6

28461

29534

30416

31005

31394

31721

31989

32191

32382

4.8

28681

29717

30566

31137

31515

31829

32084

32277

32460

5.0

28899

29898

30715

31268

31636

31937

32178

32362

32539

5.2

29113

30076

30861

31399

31757

32043

32271

32446

32617

5.4

29325

30252

31007

31529

31878

32149

32363

32530

32694

5.6

29535

30426

31152

31659

31998

32254

32453

32612

32772

5.8

29742

30599

31296

31788

32117

32358

32543

32695

32849

6.0

29947

30771

31439

31916

32234

32461

32633

32777

32926

6.2

30151

30942

31583

32044

32350

32563

32721

32859

33004

6.4

30353

31113

31727

32170

32464

32663

32810

32941

33081

6.6

30554

31283

31871

32296

32576

32762

32898

33023

33158

6.8

30753

31454

32017

32421

32686

32859

32986

33105

33236

7.0

30952

31625

32162

32546

32794

32955

33074

33188

33313

7.2

31149

31795

32308

32669

32899

33050

33162

33271

33390

08.01.300

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.4

31345

31965

32453

32791

33004

33144

33250

33354

33468

7.6

31541

32134

32597

32912

33107

33237

33338

33437

33544

7.8

31736

32302

32739

33031

33209

33330

33426

33519

33621

8.0

31930

32469

32880

33149

33310

33423

33514

33602

33696

8.2

32123

32634

33018

33265

33411

33516

33601

33683

33771

8.4

32316

32797

33153

33379

33511

33609

33689

33764

33845

8.6

32509

32957

33286

33492

33612

33702

33776

33845

33918

8.8

32701

33116

33414

33603

33713

33796

33863

33924

33989

9.0

32892

33271

33539

33712

33815

33890

33950

34003

34060

9.2

33081

33424

33661

33819

33916

33985

34037

34080

34129

9.4

33268

33575

33781

33926

34018

34080

34123

34157

34198

9.6

33452

33723

33900

34031

34119

34174

34208

34234

34267

9.8

33632

33869

34017

34137

34220

34268

34292

34309

34335

10.0

33808

34011

34133

34242

34321

34361

34376

34384

34403

10.2

33980

34152

34248

34347

34422

34453

34459

34459

34470

10.4

34145

34289

34364

34452

34522

34544

34540

34533

34538

10.6

34305

34424

34480

34559

34621

34634

34620

34606

34607

10.8

34458

34556

34598

34666

34720

34722

34698

34680

34676

11.0

34606

34686

34716

34774

34817

34809

34776

34752

34745

11.2

34749

34814

34834

34882

34914

34894

34852

34825

34815

11.4

34888

34941

34953

34990

35010

34978

34927

34897

34884

11.6

35024

35066

35072

35097

35105

35061

35002

34969

34954

Original

07-14-08

08.01.301

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.8

35159

35190

35190

35204

35198

35143

35077

35040

35023

12.0

35293

35313

35307

35309

35290

35224

35151

35112

35092

12.2

35428

35436

35423

35413

35381

35305

35225

35183

35161

12.4

35564

35560

35537

35515

35471

35386

35300

35254

35228

12.6

35702

35684

35649

35615

35559

35466

35375

35325

35295

12.8

35844

35808

35760

35712

35646

35546

35451

35397

35361

13.0

35987

35933

35868

35807

35731

35626

35527

35468

35426

13.2

36133

36058

35974

35900

35816

35706

35604

35538

35490

13.4

36279

36182

36079

35991

35899

35786

35680

35609

35554

13.6

36425

36305

36182

36081

35982

35866

35757

35679

35617

13.8

36570

36427

36283

36169

36065

35946

35833

35748

35679

14.0

36712

36547

36382

36257

36147

36025

35908

35817

35740

14.2

36852

36665

36481

36344

36230

36104

35983

35885

35802

14.4

36987

36780

36577

36432

36312

36183

36057

35953

35863

14.6

37118

36892

36673

36519

36396

36261

36129

36019

35923

14.8

37243

37001

36768

36607

36479

36339

36200

36084

35984

15.0

37363

37106

36861

36695

36564

36416

36270

36148

36044

15.2

37478

37208

36954

36783

36648

36493

36339

36212

36104

08.01.302

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

25415

27032

28509

29405

29977

30504

30924

31255

31546

3.2

25669

27244

28679

29553

30109

30625

31036

31352

31629

3.4

25921

27455

28849

29700

30241

30746

31146

31448

31712

3.6

26173

27665

29018

29847

30373

30866

31256

31544

31795

3.8

26422

27874

29187

29994

30505

30985

31365

31639

31878

4.0

26670

28082

29355

30141

30637

31104

31472

31734

31961

4.2

26915

28289

29523

30287

30770

31222

31578

31827

32044

4.4

27158

28493

29691

30434

30902

31338

31681

31920

32127

4.6

27397

28696

29857

30581

31034

31454

31783

32011

32211

4.8

27633

28896

30023

30727

31166

31568

31882

32102

32294

5.0

27866

29095

30188

30873

31298

31681

31980

32191

32378

5.2

28097

29292

30352

31019

31429

31793

32076

32280

32461

5.4

28326

29487

30516

31163

31559

31903

32170

32368

32544

5.6

28553

29682

30679

31307

31688

32012

32263

32455

32628

5.8

28779

29875

30841

31450

31816

32121

32356

32542

32711

6.0

29005

30068

31003

31591

31941

32228

32448

32628

32793

6.2

29231

30260

31164

31731

32065

32333

32540

32715

32876

6.4

29458

30453

31324

31869

32186

32438

32633

32801

32958

6.6

29685

30646

31484

32005

32305

32542

32726

32888

33039

6.8

29914

30839

31644

32139

32421

32645

32820

32976

33121

7.0

30144

31032

31802

32271

32534

32747

32914

33063

33201

Original

07-14-08

08.01.303

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

30375

31225

31959

32401

32645

32849

33009

33151

33281

7.4

30605

31417

32115

32529

32754

32949

33104

33238

33360

7.6

30835

31608

32269

32656

32862

33050

33200

33325

33439

7.8

31065

31797

32421

32780

32969

33150

33295

33412

33517

8.0

31292

31985

32571

32904

33076

33249

33389

33499

33594

8.2

31518

32170

32718

33026

33182

33349

33483

33584

33671

8.4

31742

32352

32862

33147

33289

33449

33577

33668

33747

8.6

31963

32531

33002

33267

33398

33548

33669

33752

33822

8.8

32180

32706

33140

33385

33507

33648

33760

33834

33896

9.0

32394

32878

33274

33503

33617

33748

33849

33915

33969

9.2

32604

33046

33405

33620

33728

33848

33938

33995

34042

9.4

32810

33212

33535

33737

33839

33947

34026

34074

34114

9.6

33012

33374

30663

33853

33950

34046

34112

34152

34187

9.8

33209

33534

30790

33968

34060

34144

34198

34230

34259

10.0

33401

33692

33917

34084

34170

34241

34283

24307

34331

10.2

33588

33847

34044

34199

34278

34337

34366

34384

34403

10.4

33771

34000

34172

34314

34385

34431

34450

34461

34476

10.6

33947

34151

34302

34429

34490

34524

34532

34539

34549

10.8

34118

34301

34433

34544

34593

34615

34614

34616

34622

11.0

34285

34448

34566

34659

34694

34704

34695

34693

34696

11.2

34448

34595

34700

34774

34792

34792

34775

34770

34771

11.4

34607

34740

34833

34887

34889

34879

34856

34848

34845

11.6

34765

34884

34966

35000

34985

34965

34936

34925

34919

08.01.304

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.8

34922

35027

35098

35112

35079

35050

35016

35002

34992

12.0

35078

35169

35228

35222

35172

35135

35096

35078

35065

12.2

35236

35310

35356

35330

35265

35220

35177

35154

35136

12.4

35395

35450

35481

35436

35356

35304

35257

35230

35207

12.6

35557

35590

35602

35540

35447

35389

35338

35305

35276

12.8

35722

35730

35718

35641

35538

35475

35420

35380

35344

13.0

35890

35868

35832

35739

35628

35561

35502

35454

35410

13.2

36058

36006

35941

35836

35718

35647

35584

35527

35475

13.4

36227

36142

36048

35931

35808

35734

35665

35600

35539

13.6

36394

36276

36153

36024

35898

35820

35747

35672

35602

13.8

36559

36408

36256

36117

35988

35906

35827

35743

35665

14.0

36720

36538

36357

36210

36078

35991

35907

35813

35727

14.2

36875

36665

36458

36302

36167

36075

35985

35883

35789

14.4

37025

36789

36558

36395

36257

36159

36062

35952

35852

14.6

37167

36909

36659

36488

36347

36241

36136

36020

35914

14.8

37300

37025

36760

36583

36437

36323

36209

36087

35977

15.0

37426

37138

36861

36678

36526

36403

36281

36154

36040

15.2

37545

37248

36962

36773

36616

36481

36350

36220

36104

Original

07-14-08

08.01.305

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

24068

25855

27546

28738

29545

30165

30650

31022

31341

3.2

24327

26081

27739

28906

29694

30294

30763

31121

31430

3.4

24586

26307

27933

29074

29842

30423

30875

31220

31518

3.6

24844

26532

28126

29242

29989

30552

30987

31319

31607

3.8

25101

26758

28320

29410

30135

30679

31098

31418

31696

4.0

25357

26983

28514

29577

30280

30805

31208

31516

31785

4.2

25613

27208

28708

29744

30424

30929

31317

31614

31873

4.4

25867

27433

28902

29910

30566

31052

31426

31712

31962

4.6

26120

27657

29096

30075

30706

31173

31532

31809

32051

4.8

26372

27881

29291

30240

30844

31292

31638

31905

32140

5.0

26623

28105

29486

30404

30981

31409

31742

32001

32229

5.2

26873

28328

29680

30566

31115

31524

31846

32096

32318

5.4

27122

28550

29873

30727

31248

31638

31948

32191

32406

5.6

27371

28772

30064

30887

31379

31751

32050

32285

32494

5.8

27620

28992

30254

31044

31509

31863

32151

32379

32582

6.0

27869

29211

30441

31200

31638

31974

32252

32473

32668

6.2

28119

29429

30626

31353

31765

32085

32353

32566

32755

6.4

28369

29645

30808

31503

31891

32196

32453

32659

32840

6.6

28621

29860

30986

31651

32016

32306

32554

32752

32924

6.8

28873

30073

31160

31795

32140

32417

32656

32844

33008

7.0

29126

30285

31331

31937

32264

32528

32757

32936

33090

7.2

29380

30494

31498

32077

32386

32639

32859

33028

33172

08.01.306

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.4

29632

30702

31662

32214

32508

32750

32960

33119

33253

7.6

29884

30907

31824

32350

32629

32861

33061

33209

33333

7.8

30135

31111

31984

32484

32750

32971

33161

33299

33412

8.0

30383

31312

32142

32617

32870

33081

33260

33388

33491

8.2

30629

31512

32298

32749

32990

33190

33358

33476

33570

8.4

30871

31708

32453

32881

33110

33298

33455

33563

33648

8.6

31110

31903

32608

33013

33229

33405

33551

33649

33727

8.8

31345

32095

32762

33145

33348

33511

33645

33734

33805

9.0

31575

32285

32915

33277

33467

33616

33737

33818

33883

9.2

31802

32473

33067

33408

33585

33720

33828

33901

33960

9.4

32026

32659

33219

33539

33702

33823

33918

33983

34038

9.6

32246

32843

33371

33670

33819

33925

34007

34065

34115

9.8

32464

33026

33521

33800

33934

34026

34095

34147

34193

10.0

32679

33206

33671

33928

34048

34125

34183

34228

34270

10.2

32893

33386

33820

34056

34160

34223

34270

34309

34346

10.4

33104

33564

33967

34182

34270

34320

34358

34390

34423

10.6

33314

33741

34114

34306

34378

34417

34445

34472

34499

10.8

33523

33917

34260

34428

34484

34511

34532

34553

34575

11.0

33731

34092

34404

34548

34587

34605

34620

34635

34651

11.2

33937

34266

34547

34667

34689

34698

34707

34717

34726

11.4

34142

34438

34688

34784

34790

34791

34795

34798

34801

11.6

34345

34608

34827

34899

34890

34883

34882

34880

34875

Original

07-14-08

08.01.307

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.8

34546

34776

34964

35013

34989

34974

34969

34961

34948

12.0

34746

34942

35099

35125

35087

35066

35056

35041

35021

12.2

34943

35106

35231

35236

35185

35157

35142

35121

35093

12.4

35138

35266

35361

35346

35283

35248

35228

35200

35165

12.6

35330

35424

35488

35454

35382

35340

35313

35277

35235

12.8

35520

35579

35611

35562

35481

35432

35397

35354

35304

13.0

35707

35731

35732

35668

35581

35524

35480

35429

35373

13.2

35890

35880

35851

35773

35681

35616

35563

35504

35441

13.4

36070

36026

35968

35878

35781

35708

35644

35577

35508

13.6

36246

36169

36083

35982

35881

35799

35725

35650

35575

13.8

36417

36310

36197

36085

35980

35889

35805

35722

35642

14.0

36584

36449

36311

36188

36078

35979

35884

35794

35708

14.2

36746

36585

36425

36291

36176

36067

35963

35865

35774

14.4

36902

36719

36538

36394

36272

36154

36040

35936

35841

14.6

37053

36851

36653

36498

36366

36239

36116

36007

35907

14.8

37197

36981

36768

36601

36459

36322

36192

36077

35974

15.0

37337

37108

36884

36704

36550

36404

36266

36148

36041

15.2

37471

37234

37001

36807

36640

36484

36340

36218

36109

08.01.308

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

22744

24660

26530

27923

28958

29693

30263

30685

31044

3.2

23007

24899

26746

28114

29124

29833

30379

30789

31141

3.4

23270

25139

26963

28304

29290

29971

30494

30893

31237

3.6

23534

25380

27180

28494

29453

30109

30610

30997

31334

3.8

23798

25621

27398

28683

29615

30245

30725

31101

31430

4.0

24063

25864

27617

28871

29774

30380

30840

31206

31527

4.2

24328

26107

27837

29059

29931

30513

30955

31310

31623

4.4

24594

26351

28058

29245

30084

30644

31069

31415

31719

4.6

24860

26597

28281

29430

30234

30773

31184

31519

31816

4.8

25128

26844

28504

29614

30380

30899

31298

31624

31912

5.0

25396

27092

28728

29796

30523

31024

31412

31728

32008

5.2

25665

27341

28952

29976

30663

31146

31526

31833

32104

5.4

25935

27589

29174

30155

30800

31268

31639

31937

32199

5.6

26205

27837

29395

30331

30936

31388

31752

32041

32293

5.8

26476

28083

29612

30504

31071

31507

31865

32144

32387

6.0

26747

28327

29825

30675

31204

31627

31978

32246

32479

6.2

27019

28568

30034

30843

31338

31746

32090

32348

32571

6.4

27291

28807

30236

31008

31471

31866

32202

32449

32661

6.6

27564

29042

30433

31170

31606

31986

32313

32549

32750

6.8

27837

29273

30622

31328

31741

32108

32424

32648

32837

7.0

28109

29500

30804

31483

31878

32230

32534

32746

32922

Original

07-14-08

08.01.309

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

28381

29723

30981

31635

32015

32353

32644

32842

33007

7.4

28652

29943

31154

31785

32153

32476

32753

32938

33091

7.6

28921

30161

31323

31933

32291

32599

32860

33033

33174

7.8

29188

30376

31490

32080

32429

32721

32967

33127

33256

8.0

29453

30589

31656

32227

32566

32842

33072

33220

33338

8.2

29714

30801

31822

32373

32702

32963

33176

33312

33421

8.4

29972

31011

31988

32519

32838

33081

33278

33404

33504

8.6

30226

31221

32156

32666

32972

33198

33379

33495

33587

8.8

30476

31429

32326

32813

33104

33313

33477

33585

33671

9.0

30723

31637

32499

32962

33235

33425

33574

33674

33755

9.2

30966

31845

32673

33111

33364

33536

33670

33763

33840

9.4

31208

32052

32848

33259

33491

33645

33765

33851

33925

9.6

31448

32259

33023

33407

33616

33753

33859

33940

34009

9.8

31688

32466

33198

33553

33739

33859

33952

34027

34094

10.0

31928

32672

33372

33698

33861

33965

34046

34115

34178

10.2

32169

32878

33544

33840

33980

34069

34139

34203

34261

10.4

32412

33083

33713

33980

34097

34173

34233

34290

34343

10.6

32658

33289

33879

34117

34213

34276

34328

34378

34424

10.8

32907

33494

34042

34251

34326

34378

34424

34466

34504

11.0

33157

33698

34201

34381

34437

34481

34520

34553

34582

11.2

33409

33902

34356

34509

34547

34583

34617

34641

34659

11.4

33661

34103

34508

34634

34655

34684

34714

34728

34736

11.6

33910

34301

34657

34756

34763

34785

34811

34814

34811

08.01.310

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER FIVE (WSTA 707.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.8

34157

34497

34803

34878

34871

34886

34907

34900

34885

12.0

34400

34688

34945

34997

34978

34987

35002

34985

34959

12.2

34637

34875

35085

35116

35086

35088

35096

35069

35033

12.4

34867

35058

35222

35233

35195

35188

35188

35152

35106

12.6

35089

35234

35356

35351

35305

35288

35278

35233

35178

12.8

35302

35405

35488

35468

35416

35388

35365

35312

35251

13.0

35507

35570

35617

35585

35529

35487

35451

35390

35323

13.2

35704

35730

35745

35702

35641

35586

35535

35467

35395

13.4

35893

35886

35872

35819

35754

35684

35618

35543

35468

13.6

36075

36038

35998

35936

35866

35781

35699

35619

35540

13.8

36252

36187

36124

36052

35977

35877

35779

35693

35612

14.0

36423

36334

36250

36168

36086

35971

35858

35768

35684

14.2

36590

36480

36376

36283

36193

36064

35937

35842

35756

14.4

36752

36624

36504

36398

36297

36155

36016

35917

35828

14.6

36911

36768

36633

36512

36398

36244

36095

35991

35900

14.8

37068

36912

36763

36625

36495

36330

36175

36066

35972

15.0

37222

37055

36895

36738

36589

36415

36254

36142

36044

15.2

37374

37198

37027

36849

36680

36499

36334

36217

36116

Original

07-14-08

08.01.311

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

34414

34795

35055

35262

35430

35585

35708

35793

35911

3.2

34523

34886

35135

35338

35503

35650

35765

35847

35964

3.4

34631

34976

35214

35413

35576

35714

35822

35901

36016

3.6

34738

35067

35294

35489

35648

35779

35879

35955

36068

3.8

34846

35157

35374

35563

35720

35843

35936

36009

36120

4.0

34952

35248

35453

35638

35790

35907

35993

36064

36171

4.2

35058

35338

35533

35712

35860

35970

36051

36118

36221

4.4

35164

35428

35612

35785

35928

36033

36108

36172

36272

4.6

35269

35518

35692

35857

35996

36095

36166

36226

36321

4.8

35372

35608

35771

35929

36062

36157

36224

36280

36370

5.0

35475

35698

35850

35999

36126

36218

36282

36334

36418

5.2

35577

35787

35930

36070

36190

36278

36340

36388

36466

5.4

35677

35876

36008

36139

36253

36338

36398

36442

36513

5.6

35777

35965

36087

36208

36315

36398

36456

36495

36560

5.8

35875

36052

36166

36277

36376

36456

36514

36549

36607

6.0

35971

36139

36244

36346

36438

36515

36570

36602

36653

6.2

36066

36225

36322

36414

36498

36573

36627

36654

36700

6.4

36159

36310

36399

36483

36559

36630

36682

36706

36747

6.6

36250

36393

36476

36551

36620

36687

36737

36758

36794

6.8

36340

36476

36553

36620

36681

36743

36791

36809

36841

7.0

36428

36557

36629

36688

36742

36800

36844

36860

36889

7.2

36515

36637

36704

36757

36803

36855

36896

36910

36937

08.01.312

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.4

36601

36716

36779

36825

36865

36911

36947

36960

36985

7.6

36686

36795

36853

36893

36926

36966

36998

37009

37033

7.8

36771

36872

36926

36960

36988

37021

37049

37058

37080

8.0

36856

36949

36998

37027

37049

37076

37099

37107

37128

8.2

36942

37026

37069

37093

37110

37131

37149

37155

37175

8.4

37028

37102

37139

37159

37171

37186

37198

37203

37221

8.6

37115

37178

37208

37223

37232

37241

37248

37251

37267

8.8

37203

37254

37275

37286

37292

37296

37298

37298

37312

9.0

37291

37329

37341

37349

37352

37351

37348

37345

37357

9.2

37381

37404

37407

37411

37412

37405

37397

37392

37401

9.4

37470

37479

37472

37472

37471

37460

37447

37439

37444

9.6

37558

37553

37536

37532

37529

37514

37497

37486

37488

9.8

37646

37628

37600

37592

37587

37568

37547

37532

37530

10.0

37732

37701

37664

37651

37644

37622

37597

37579

37573

10.2

37817

37774

37728

37711

37701

37675

37646

37625

37615

10.4

37899

37847

37793

37770

37756

37728

37696

37672

37657

10.6

37978

37919

37858

37829

37811

37780

37746

37718

37699

10.8

38055

37990

37924

37889

37865

37831

37795

37764

37741

11.0

38128

38050

37991

37948

37918

37881

37844

37810

37782

11.2

38200

38130

38057

38007

37970

37931

37893

37856

37824

11.4

38270

38199

38124

38066

38022

37980

37942

37902

37866

11.6

38338

38267

38190

38125

38073

38029

37990

37948

37907

Original

07-14-08

08.01.313

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = -2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.8

38405

38334

38256

38184

38124

38078

38038

37993

37949

12.0

38471

38401

38321

38242

38175

38126

38085

38038

37991

12.2

38537

38466

38385

38300

38226

38174

38132

38083

38033

12.4

38603

38531

38448

38357

38278

38222

38178

38127

38074

12.6

38669

38594

38509

38414

38329

38270

38224

38170

38116

12.8

38737

38657

38568

38470

38382

38319

38268

38213

38158

13.0

38804

38718

38626

38525

38434

38367

38312

38256

38199

13.2

38873

38779

38682

38579

38487

38415

38356

38298

38241

13.4

38941

38839

38736

38633

38540

38463

38399

38340

38282

13.6

39010

38898

38790

38686

38593

38511

38442

38381

38323

FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

34110

34554

34860

35090

35278

35448

35582

35679

35808

3.2

34228

34651

34945

35170

35355

35516

35643

35736

35863

3.4

34345

34749

35030

35251

35432

35585

35703

35793

35918

3.6

34462

34846

35115

35330

35508

35653

35763

35850

35972

3.8

34579

34943

35199

35410

35583

35721

35824

35906

36026

08.01.314

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

4.0

34695

35040

35284

35489

35658

35789

35884

35963

36080

4.2

34810

35137

35369

35567

35731

35856

35945

36020

36133

4.4

34925

35233

35453

35644

35803

35922

36006

36077

36186

4.6

35038

35330

35538

35721

35874

35988

36067

36134

36237

4.8

35151

35427

35622

35796

35943

36053

36128

36191

36289

5.0

35262

35523

35707

35871

36012

36117

36189

36248

36339

5.2

35372

35619

35791

35945

36079

36181

36250

36305

36389

5.4

35481

35715

35875

36019

36145

36244

36311

36362

36439

5.6

35588

35810

35959

36092

36210

36306

36372

36418

36489

5.8

35694

35904

36042

36164

36275

36368

36433

36474

36538

6.0

35798

35997

36125

36237

36339

36429

36492

36530

36587

6.2

35900

36090

36208

36309

36403

36490

36552

36586

36636

6.4

36001

36181

36291

36381

36467

36550

36610

36641

36686

6.6

36100

36270

36372

36454

36531

36610

36667

36695

36735

6.8

36196

36358

36454

36527

36595

36669

36724

36749

36785

7.0

36291

36445

36534

36599

36660

36728

36779

36802

36836

7.2

36384

36531

36614

36672

36725

36786

36834

36855

36886

7.4

36477

36615

36693

36744

36790

36845

36888

36907

36936

7.6

36569

36699

36772

36816

36855

36903

36941

36958

36986

7.8

36660

36781

36849

36888

36919

36961

36994

37009

37036

8.0

36751

36863

36925

36959

36984

37018

37046

37060

37086

8.2

36843

36945

37000

37029

37048

37076

37099

37111

37135

Original

07-14-08

08.01.315

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

8.4

36935

37026

37074

37098

37112

37134

37151

37161

37184

8.6

37029

37107

37147

37166

37176

37191

37203

37210

37232

8.8

37123

37187

37218

37232

37239

37249

37255

37260

37279

9.0

37219

37267

37288

37298

37302

37307

37308

37309

37326

9.2

37314

37347

37357

37363

37364

37364

37360

37358

37371

9.4

37410

37427

37426

37426

37426

37421

37413

37407

37417

9.6

37505

37506

37494

37490

37487

37478

37465

37456

37461

9.8

37599

37585

37561

37552

37547

37535

37517

37505

37506

10.0

37692

37663

37629

37615

37606

37591

37570

37553

37550

10.2

37782

37741

37697

37677

37665

37647

37622

37602

37594

10.4

37870

37818

37765

37739

37723

37701

37674

37650

37637

10.6

37955

37895

37834

37801

37780

37756

37725

37698

37681

10.8

38037

37970

37904

37863

37836

37809

37777

37746

37724

11.0

38115

38045

37974

37926

37892

37861

37828

37795

37768

11.2

38191

38119

38044

37988

37947

37913

37879

37843

37812

11.4

38265

38192

38114

38050

38001

37964

37929

37890

37855

11.6

38337

38264

38184

38113

38055

38015

37979

37938

37899

11.8

38408

38336

38254

38175

38109

38066

38029

37985

37942

12.0

38478

38406

38322

38236

38162

38116

38078

38032

37986

12.2

38547

38475

38389

38297

38216

38166

38126

38078

38029

12.4

38617

38543

38455

38357

38270

38216

38174

38124

38073

12.6

38687

38610

38519

38416

38324

38266

38221

38170

38116

12.8

38758

38676

38581

38475

38379

38316

38268

38214

38159

08.01.316

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

13.0

38830

38740

38641

38533

38434

38367

38314

38258

38203

13.2

38902

38804

38700

38590

38489

38417

38359

38302

38246

13.4

38974

38867

38757

38646

38544

38467

38404

38345

38288

13.6

39047

38928

38813

38701

38598

38517

38449

38388

38331

FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

33749

34273

34648

34928

35143

35337

35492

35603

35743

3.2

33879

34378

34738

35013

35225

35409

35554

35661

35800

3.4

34008

34483

34828

35098

35307

35482

35616

35720

35856

3.6

34137

34588

34918

35183

35388

35554

35679

35778

35912

3.8

34265

34694

35008

35267

35469

35626

35741

35837

35968

4.0

34393

34799

35098

35350

35548

35697

35804

35895

36023

4.2

34519

34904

35189

35433

35625

35767

35868

35954

36078

4.4

34645

35009

35279

35515

35702

35837

35931

36013

36132

4.6

34769

35113

35369

35596

35777

35906

35995

36072

36185

4.8

34892

35218

35460

35676

35850

35975

36058

36131

36238

5.0

35014

35323

35550

35755

35921

36042

36123

36190

36290

Original

07-14-08

08.01.317

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

5.2

35134

35427

35641

35834

35991

36109

36187

36249

36341

5.4

35252

35530

35731

35912

36060

36174

36251

36308

36392

5.6

35369

35633

35821

35989

36128

36240

36314

36367

36443

5.8

35483

35735

35910

36066

36196

36304

36377

36425

36494

6.0

35596

35836

36000

36143

36263

36368

36440

36483

36545

6.2

35707

35935

36088

36219

36330

36431

36502

36540

36595

6.4

35816

36033

36176

36296

36396

36494

36562

36597

36646

6.6

35923

36129

36264

36373

36463

36556

36622

36653

36697

6.8

36027

36224

36351

36450

36531

36618

36680

36709

36749

7.0

36129

36317

36436

36526

36599

36680

36738

36763

36801

7.2

36230

36408

36521

36603

36667

36741

36794

36817

36852

7.4

36330

36499

36605

36680

36735

36802

36850

36871

36904

7.6

36429

36588

36688

36756

36803

36862

36904

36924

36956

7.8

36528

36676

36770

36831

36871

36923

36959

36976

37008

8.0

36627

36764

36851

36906

36939

36983

37013

37028

37059

8.2

36726

36851

36930

36980

37007

37043

37066

37080

37110

8.4

36825

36937

37009

37053

37075

37103

37120

37131

37160

8.6

36927

37024

37085

37124

37142

37164

37174

37182

37209

8.8

37030

37110

37161

37195

37209

37224

37228

37233

37258

9.0

37134

37197

37235

37264

37275

37284

37282

37284

37305

9.2

37238

37283

37308

37332

37340

37344

37336

37334

37352

9.4

37342

37369

37380

37399

37405

37404

37390

37385

37399

9.6

37446

37454

37452

37465

37469

37464

37445

37435

37444

08.01.318

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

9.8

37548

37539

37524

37531

37532

37523

37499

37485

37490

10.0

37648

37623

37595

37596

37594

37582

37553

37535

37535

10.2

37746

37707

37668

37662

37656

37639

37608

37585

37580

10.4

37841

37789

37740

37727

37716

37697

37662

37635

37624

10.6

37932

37871

37813

37793

37776

37753

37715

37685

37669

10.8

38019

37952

37887

37858

37834

37808

37769

37735

37714

11.0

38102

38032

37962

37924

37892

37863

37822

37784

37759

11.2

38182

38110

38037

37990

37949

37917

37875

37834

37803

11.4

38260

38188

38112

38056

38005

37970

37927

37883

37848

11.6

38336

38264

38187

38122

38061

38023

37979

37932

37893

11.8

38410

38339

38260

38187

38117

38075

38030

37981

37938

12.0

38484

38413

38333

38252

38173

38127

38081

38029

37983

12.2

38557

38486

38404

38316

38229

38179

38131

38077

38028

12.4

38630

38558

38474

38380

38285

38231

38180

38124

38072

12.6

38704

38628

38541

38442

38342

38283

38229

38170

38117

12.8

38779

38697

38606

38504

38399

38336

38277

38216

38162

13.0

38856

38765

38669

38564

38457

38388

38324

38261

38206

13.2

38933

38832

38730

38624

38515

38441

38371

38306

38250

13.4

39010

38898

38790

38682

38573

38493

38417

38350

38294

13.6

39087

38963

38848

38740

38631

38546

38463

38394

38337

Original

07-14-08

08.01.319

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

33297

33930

34398

34757

35026

35221

35371

35501

35654

3.2

33442

34046

34495

34847

35113

35299

35437

35562

35713

3.4

33586

34161

34592

34938

35200

35376

35504

35623

35771

3.6

33730

34276

34689

35028

35287

35453

35570

35684

35829

3.8

33872

34391

34786

35117

35372

35529

35636

35745

35886

4.0

34014

34506

34883

35206

35456

35605

35703

35806

35943

4.2

34154

34621

34980

35295

35539

35680

35770

35868

36000

4.4

34293

34736

35077

35382

35620

35754

35837

35929

36056

4.6

34430

34851

35175

35469

35700

35828

35904

35991

36111

4.8

34566

34966

35272

35555

35778

35900

35971

36052

36166

5.0

34699

35080

35370

35639

35854

35971

36039

36114

36220

5.2

34831

35193

35468

35723

35929

36042

36106

36176

36274

5.4

34961

35306

35565

35807

36002

36111

36173

36237

36327

5.6

35088

35418

35662

35890

36075

36180

36240

36299

36380

5.8

35214

35529

35759

35972

36147

36248

36306

36359

36433

6.0

35337

35638

35855

36054

36218

36315

36372

36420

36486

6.2

35458

35746

35950

36136

36289

36382

36436

36480

36539

6.4

35577

35852

36045

36218

36361

36448

36499

36539

36592

6.6

35694

35956

36138

36300

36432

36514

36562

36597

36646

6.8

35808

36058

36231

36382

36504

36579

36622

36655

36700

7.0

35920

36158

36322

36464

36577

36644

36682

36711

36754

7.2

36031

36257

36412

36546

36650

36708

36740

36767

36808

08.01.320

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.4

36140

36354

36501

36627

36723

36772

36798

36823

36862

7.6

36249

36450

36589

36708

36796

36836

36855

36877

36916

7.8

36358

36544

36676

36788

36868

36900

36911

36931

36970

8.0

36466

36639

36761

36867

36941

36964

36967

36985

37023

8.2

36575

36732

36845

36946

37013

37027

37023

37038

37076

8.4

36685

36825

36928

37023

37085

37091

37079

37092

37128

8.6

36796

36919

37010

37098

37156

37154

37136

37144

37179

8.8

36909

37012

37090

37173

37226

37218

37192

37197

37229

9.0

37023

37106

37170

37246

37296

37281

37249

37250

37278

9.2

37137

37199

37248

37318

37364

37344

37306

37302

37326

9.4

37250

37293

37326

37389

37432

37408

37363

37354

37373

9.6

37363

37385

37403

37459

37499

37470

37420

37406

37420

9.8

37475

37477

37480

37529

37566

37532

37478

37459

37466

10.0

37583

37569

37557

37598

37631

37594

37535

37510

37513

10.2

37689

37659

37635

37667

37696

37655

37591

37562

37559

10.4

37792

37748

37713

37736

37759

37715

37648

37614

37605

10.6

37890

37836

37791

37806

37822

37774

37704

37666

37651

10.8

37983

37923

37870

37876

37884

37832

37759

37717

37697

11.0

38072

38008

37950

37946

37946

37889

37814

37768

37743

11.2

38158

38092

38030

38017

38006

37945

37869

37820

37790

11.4

38241

38174

38109

38087

38067

38001

37922

37870

37837

11.6

38321

38255

38188

38157

38127

38056

37976

37921

37884

Original

07-14-08

08.01.321

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.8

38400

38335

38267

38227

38187

38111

38029

37971

37930

12.0

38477

38413

28343

38296

38246

38165

38081

38021

37977

12.2

38555

38490

38419

38365

38306

38220

38132

38070

38024

12.4

38633

38565

38492

38432

38366

38274

38184

38118

38070

12.6

38712

38640

38563

38498

38427

38329

38234

38166

38116

12.8

38792

38713

38631

38563

38488

38385

38284

38214

38162

13.0

38874

38784

38697

38627

38549

38440

38333

38260

38208

13.2

38957

38855

38761

38690

38611

38496

38382

38307

38253

13.4

39040

38925

38823

38751

38672

38551

38431

38352

38298

13.6

39123

38994

38884

38812

38733

38607

38479

38398

38343

FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE =0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

32743

33509

34088

34539

34865

35066

35223

35373

35543

3.2

32910

33640

34193

34636

34960

35149

35292

35437

35604

3.4

33076

33770

34297

34733

35054

35232

35362

35501

35664

3.6

33240

33900

34402

34829

35147

35314

35431

35565

35725

3.8

33403

34030

34507

34924

35239

35395

35501

35629

35785

08.01.322

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE =0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

4.0

33565

34159

34612

35020

35330

35476

35571

35693

35844

4.2

33724

34288

34718

35114

35419

35556

35642

35758

35903

4.4

33880

34416

34824

35208

35507

35635

35713

35822

35962

4.6

34034

34544

34930

35301

35592

35713

35784

35887

36020

4.8

34185

34671

35036

35394

35675

35790

35855

35952

36077

5.0

34333

34796

35143

35485

35756

35865

35927

36017

36134

5.2

34478

34921

35250

35576

35836

35940

35999

36082

36190

5.4

34620

35045

35356

35666

35914

36014

36070

36147

36246

5.6

34760

35167

35462

35755

35991

36086

36141

36211

36302

5.8

34897

35288

35568

35845

36067

36158

36211

36275

36357

6.0

35031

35407

35672

35933

36143

36230

36280

36339

36413

6.2

35163

35524

35776

36022

36219

36300

36349

36402

36468

6.4

35293

35638

35879

36110

36295

36370

36416

36464

36524

6.6

35420

35751

35980

36198

36371

36440

36481

36525

36581

6.8

35545

35861

36079

36286

36449

36510

36545

36585

36637

7.0

35669

35969

36177

36373

36527

36579

36607

36644

36695

7.2

35791

36076

36273

36461

36605

36647

36668

36703

36752

7.4

35912

36180

36368

36548

36684

36716

36728

36761

36809

7.6

36033

36284

36461

36634

36763

36784

36787

36818

36866

7.8

36153

36386

36553

36719

36841

36852

36846

36874

36923

8.0

36273

36488

36644

36803

36920

36920

36904

36930

36979

8.2

36394

36589

36733

36886

36997

36988

36962

36986

37034

Original

07-14-08

08.01.323

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE =0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

8.4

36516

36690

36821

36968

37075

37055

37020

37041

37088

8.6

36639

36791

36907

37048

37151

37122

37079

37096

37141

8.8

36763

36893

36993

37127

37226

37190

37138

37151

37193

9.0

36889

36995

37077

37204

37300

37257

37198

37206

37244

9.2

37014

37097

37161

37280

37373

37324

37258

37261

37294

9.4

37139

37198

37244

37355

37444

37390

37318

37316

37343

9.6

37263

37300

37327

37429

37515

37456

37378

37371

37391

9.8

37385

37400

37409

37503

37585

37521

37439

37425

37439

10.0

37504

37499

37492

37576

37654

37586

37499

37480

37487

10.2

37619

37597

37575

37650

37722

37650

37558

37534

37535

10.4

37730

37694

37659

37723

37789

37712

37618

37588

37582

10.6

37836

37789

37743

37797

37855

37774

37677

37642

37630

10.8

37936

37882

37828

37872

37920

37835

37735

37695

37678

11.0

38031

37973

37914

37947

37985

37895

37792

37749

37727

11.2

38122

38062

38000

38022

38049

37954

37849

37802

37775

11.4

38210

38150

38086

38097

38112

38012

37905

37855

37824

11.6

38295

38236

38171

38172

38175

38070

37960

37907

37873

11.8

38379

38321

38255

38247

38239

38127

38015

37959

37922

12.0

38462

38403

38337

38321

38302

38184

38069

38010

37971

12.2

38544

38485

38418

38393

38366

38242

38123

38061

38020

12.4

38628

38565

38496

38465

38430

38299

38176

38111

38068

12.6

38712

38644

38571

38535

38494

38357

38228

38161

38116

12.8

38799

38722

38643

38604

38560

38416

38280

38210

38164

08.01.324

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE =0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

13.0

38888

38798

38712

38671

38625

38474

38331

38258

38211

13.2

38978

38874

38778

38737

38691

38533

38381

38306

38258

13.4

39069

38948

38843

38802

38757

38592

38432

38353

38305

13.6

39159

39022

38906

38865

38823

38651

38482

38400

38350

FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

32018

32975

33728

34252

34595

34851

35056

35236

35425

3.2

32220

33128

33844

34354

34694

34939

35131

35303

35488

3.4

32419

33281

33960

34457

34792

35027

35206

35371

35550

3.6

32616

33434

34076

34559

34890

35114

35281

35438

35612

3.8

32811

33585

34193

34661

34986

35200

35356

35506

35674

4.0

33001

33735

34310

34763

35081

35286

35431

35574

35736

4.2

33188

33883

34427

34864

35175

35370

35506

35642

35797

4.4

33370

34030

34544

34965

35267

35454

35581

35710

35858

4.6

33546

34175

34662

35066

35357

35536

35656

35778

35919

4.8

33717

34317

34780

35166

35445

35617

35732

35846

35979

5.0

33882

34458

34899

35265

35531

35696

35807

35914

36039

Original

07-14-08

08.01.325

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

5.2

34042

34597

35017

35364

35616

35775

35882

35983

36098

5.4

34198

34733

35134

35462

35700

35852

35956

36051

36157

5.6

34350

34867

35251

35560

35782

35929

36030

36118

36216

5.8

34499

34999

35367

35657

35864

36005

36103

36186

36275

6.0

34644

35128

35481

35754

35946

36080

36176

36252

36334

6.2

34787

35255

35594

35850

36028

36155

36247

36318

36393

6.4

34928

35380

35705

35945

36110

36229

36317

36383

36452

6.6

35067

35502

35814

36040

36193

36304

36386

36447

36512

6.8

35206

35622

35921

36134

36276

36378

36453

36510

36571

7.0

35343

35739

36025

36227

36360

36452

36519

36572

36631

7.2

35480

35855

36127

36320

36444

36526

36584

36633

36690

7.4

35616

35969

36227

36412

36529

36599

36647

36694

36750

7.6

35753

36081

36325

36502

36613

36673

36711

36754

36809

7.8

35889

36193

36422

36592

36697

36746

36774

36813

36868

8.0

36025

36305

36517

36680

36780

36819

36836

36872

36926

8.2

36162

36415

36611

36767

36863

36891

36899

36930

36983

8.4

36299

36526

36705

36853

36944

36963

36961

36988

37039

8.6

36436

36638

36797

36937

37023

37035

37024

37047

37094

8.8

36575

36749

36889

37020

37102

37106

37088

37105

37148

9.0

36714

36861

36981

37101

37178

37177

37152

37163

37201

9.2

36852

36973

37072

37182

37253

37247

37216

37221

37252

9.4

36989

37085

37162

37261

37327

37316

37280

37279

37303

9.6

37124

37196

37253

37340

37400

37385

37344

37337

37354

08.01.326

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

9.8

37256

37306

37343

37418

37472

37453

37408

37395

37404

10.0

37385

37415

37433

37496

37543

37520

37472

37453

37454

10.2

37510

37522

37524

37574

37613

37586

37535

37510

37504

10.4

37630

37627

37614

37652

37683

37651

37597

37567

37554

10.6

37744

37730

37705

37730

37752

37715

37658

37623

37604

10.8

37853

37830

37796

37809

37820

37779

37719

37679

37655

11.0

37956

37927

37887

37889

37888

37841

37778

37735

37706

11.2

38055

38023

37978

37969

37957

37903

37837

37790

37758

11.4

38150

38116

38068

38048

38024

37964

37894

37845

37810

11.6

38242

38208

38157

38128

38092

38025

37951

37899

37861

11.8

38333

38297

38245

38206

38160

38085

38007

37952

37913

12.0

38424

38385

38331

38284

38227

38145

38063

38005

37964

12.2

38514

38472

38415

38361

38295

38205

38118

38058

38015

12.4

38605

38558

38496

38436

38363

38266

38173

38110

38065

12.6

38698

38643

38575

38510

38431

38326

38227

38161

38115

12.8

38794

38726

38651

38582

38499

38388

38282

38212

38165

13.0

38892

38809

38725

38652

38567

38449

38336

38262

38213

13.2

38992

38892

38796

38721

38635

38511

38389

38312

38261

13.4

39091

38973

38865

38788

38703

38572

38443

38362

38308

13.6

39191

39053

38933

38854

38770

38633

38496

38411

38355

Original

07-14-08

08.01.327

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

31052

32240

33263

33911

34287

34622

34884

35100

35302

3.2

31289

32418

33391

34021

34392

34715

34964

35171

35366

3.4

31524

32595

33519

34131

34497

34808

35044

35243

35431

3.6

31755

32771

33647

34242

34600

34900

35123

35315

35496

3.8

31983

32946

33776

34352

34703

34991

35203

35386

35560

4.0

32205

33119

33905

34462

34804

35081

35283

35458

35624

4.2

32422

33290

34035

34571

34903

35170

35362

35529

35688

4.4

32631

33458

34166

34681

35001

35258

35442

35601

35752

4.6

32834

33624

34297

34791

35097

35344

35521

35672

35816

4.8

33028

33787

34430

34900

35191

35429

35600

35744

35879

5.0

33215

33946

34562

35009

35282

35512

35679

35815

35942

5.2

33395

34103

34695

35118

35372

35594

35757

35886

36004

5.4

33571

34257

34828

35226

35461

35675

35835

35957

36067

5.6

33741

34409

34959

35333

35549

35755

35912

36028

36129

5.8

33907

34557

35089

35439

35637

35835

35989

36098

36192

6.0

34071

34703

35217

35545

35724

35914

36064

36167

36254

6.2

34232

34846

35343

35649

35811

35992

36138

36235

36316

6.4

34392

34986

35466

35753

35899

36071

36211

36302

36378

6.6

34551

35124

35585

35855

35988

36150

36283

36369

36440

6.8

34711

35259

35701

35955

36077

36229

36353

36434

36502

7.0

34871

35392

35814

36054

36168

36308

36422

36499

36564

7.2

35031

35523

35923

36151

36259

36387

36490

36562

36626

08.01.328

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.4

35192

35653

36030

36248

36350

36466

36557

36625

36687

7.6

35352

35781

36134

36342

36440

36545

36624

36687

36748

7.8

35513

35908

36237

36436

36530

36623

36690

36749

36809

8.0

35672

36034

36338

36528

36620

36701

36756

36810

36869

8.2

35832

36159

36438

36619

36708

36778

36823

36871

36928

8.4

35991

36285

36538

36709

36794

36855

36889

36933

36986

8.6

36149

36410

36637

36797

36878

36931

36956

36994

37043

8.8

36306

36536

36737

36885

36960

37006

37024

37056

37099

9.0

36462

36661

36837

36971

37040

37080

37092

37117

37154

9.2

36615

36786

36936

37057

37119

37153

37160

37179

37208

9.4

36767

36911

37036

37142

37195

37225

37229

37241

37262

9.6

36915

37034

37136

37226

37271

37296

37297

37302

37315

9.8

37060

37156

37236

37310

37345

37367

37365

37364

37368

10.0

37200

37276

37335

37393

37418

37436

37432

37425

37420

10.2

37336

37394

37435

37477

37490

37505

37499

37485

37473

10.4

37467

37509

37534

37561

37562

37572

37565

37545

37526

10.6

37591

37621

37632

37645

37634

37639

37629

37604

37579

10.8

37710

37730

37731

37729

37706

37705

37692

37663

37633

11.0

37824

37837

37828

37813

37778

37771

37753

37721

37687

11.2

37933

37940

37925

37897

37850

37835

37814

37778

37741

11.4

38039

38041

38021

37981

37922

37899

37873

37834

37795

11.6

38142

38140

38115

38064

37993

37963

37932

37890

37850

Original

07-14-08

08.01.329

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.8

38244

38237

38208

38147

38065

38027

37990

37945

37904

12.0

38345

38333

38298

38228

38137

38090

38047

37999

37958

12.2

38447

38427

38387

38308

38209

38153

38104

38053

38011

12.4

38550

38521

38473

38387

38280

38217

38160

38107

38063

12.6

38655

38614

38556

38463

38351

38280

38216

38160

38115

12.8

38764

38706

38636

38538

38423

38344

38273

38213

38166

13.0

38874

38798

38714

38611

38494

38408

38329

38265

38216

13.2

38986

38889

38790

38682

38564

38472

38385

38317

38265

13.4

39098

38979

38863

38752

38634

38536

38441

38369

38314

13.6

39210

39068

38935

38820

38703

38599

38497

38420

38362

FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

29689

31244

32655

33528

34030

34406

34711

34958

35182

3.2

29944

31444

32805

33651

34139

34504

34799

35035

35249

3.4

30196

31643

32955

33773

34247

34601

34886

35111

35316

3.6

30447

31840

33105

33895

34354

34698

34972

35188

35383

3.8

30694

32037

33255

34017

34461

34794

35058

35264

35450

08.01.330

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

4.0

30937

32232

33406

34139

34567

34888

35143

35340

35517

4.2

31175

32425

33556

34261

34671

34982

35228

35416

35584

4.4

31408

32616

33707

34382

34775

35074

35312

35492

35651

4.6

31636

32805

33857

34504

34877

35164

35395

35567

35718

4.8

31857

32991

34008

34625

34977

35253

35476

35641

35785

5.0

32073

33175

34159

34746

35076

35340

35557

35716

35852

5.2

32284

33356

34309

34867

35174

35427

35637

35790

35919

5.4

32491

33534

34457

34986

35272

35512

35716

35863

35986

5.6

32694

33710

34604

35105

35368

35596

35794

35935

36052

5.8

32896

33884

34748

35222

35464

35680

35871

36007

36118

6.0

33096

34054

34890

35338

35559

35763

35947

36078

36184

6.2

33295

34223

35028

35451

35655

35846

36022

36148

36249

6.4

33495

34389

35162

35563

35750

35929

36097

36217

36314

6.6

33696

34552

35292

35672

35846

36013

36171

36286

36378

6.8

33898

34713

35418

35778

35942

36097

36244

36353

36441

7.0

34102

34872

35539

35882

36038

36182

36317

36419

36504

7.2

34306

35029

35657

35984

36134

36266

36389

36485

36567

7.4

34510

35183

35772

36085

36230

36351

36461

36550

36628

7.6

34713

35336

35884

36183

36325

36435

36533

36615

36690

7.8

34914

35487

35995

36280

36419

36519

36604

36679

36750

8.0

35115

35637

36105

36376

36511

36603

36676

36743

36810

8.2

35309

35785

36214

36471

36603

36685

36747

36807

36870

Original

07-14-08

08.01.331

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

8.4

35501

35932

36324

36566

36692

36766

36819

36872

36929

8.6

35689

36078

36435

36660

36780

36846

36891

36936

36987

8.8

35871

36223

36547

36754

36865

36925

36963

37001

37045

9.0

36049

36366

36660

36848

36948

37002

37035

37067

37103

9.2

36221

36509

36774

36941

37029

37078

37108

37132

37160

9.4

36388

36649

36889

37034

37109

37153

37180

37198

37216

9.6

36551

36788

37003

37127

37187

37227

37251

37263

37273

9.8

36708

36924

37117

37220

37265

37300

37322

37328

37329

10.0

36861

37057

37229

37312

37342

37372

37393

37392

37386

10.2

37009

37188

37341

37404

37419

37443

37462

37456

37442

10.4

37153

37316

37451

37495

37496

37514

37529

37519

37498

10.6

37292

37440

37559

37586

37573

37584

37596

37581

37555

10.8

37426

37561

37664

37676

37651

37654

37660

37642

37612

11.0

37557

37678

37767

37766

37729

37723

37723

37701

37669

11.2

37685

37793

37868

37855

37808

37792

37785

37760

37726

11.4

37811

37904

37967

37943

37886

37861

37846

37818

37783

11.6

37934

38014

38063

38030

37965

37929

37906

37875

37839

11.8

38057

38122

38157

38115

38043

37997

37966

37931

37895

12.0

38180

38229

38249

38199

38120

38065

38025

37987

37951

12.2

38303

38334

38340

38282

38197

38132

38084

38043

38005

12.4

38426

38439

38428

38363

38273

38200

38143

38098

38059

12.6

38552

38543

38515

38442

38348

38267

38202

38153

38112

12.8

38680

38647

38600

38519

38421

38334

38261

38208

38164

08.01.332

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

13.0

38809

38751

38684

38595

38494

38400

38321

38263

38215

13.2

38938

38855

38766

38668

38565

38467

38381

38317

38265

13.4

39066

38957

38847

38741

38635

38533

38442

38372

38315

13.6

39192

39058

38928

38812

38703

38598

38502

38426

38363

FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

28305

30185

31965

32987

33624

34082

34450

34735

34991

3.2

28573

30402

32136

33124

33740

34187

34546

34819

35061

3.4

28839

30619

32306

33262

33855

34291

34641

34902

35132

3.6

29104

30836

32477

33399

33970

34395

34736

34985

35203

3.8

29367

31052

32648

33536

34085

34498

34830

35067

35275

4.0

29628

31266

32819

33673

34199

34600

34924

35150

35346

4.2

29885

31480

32989

33810

34313

34701

35015

35231

35417

4.4

30140

31692

33160

33947

34425

34801

35106

35313

35489

4.6

30390

31903

33331

34084

34537

34899

35195

35393

35561

4.8

30637

32112

33501

34221

34647

34995

35282

35473

35634

5.0

30881

32320

33671

34357

34757

35090

35368

35552

35706

Original

07-14-08

08.01.333

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

5.2

31122

32525

33839

34492

34866

35184

35453

35631

35778

5.4

31361

32729

34006

34627

34974

35277

35536

35708

35851

5.6

31600

32932

34171

34760

35082

35369

35618

35785

35923

5.8

31838

33132

34332

34891

35189

35460

35699

35861

35994

6.0

32076

33331

34490

35020

35297

35552

35779

35937

36065

6.2

32316

33527

34645

35147

35404

35643

35859

36011

36136

6.4

32558

33722

34794

35271

35511

35734

35938

36085

36205

6.6

32803

33915

34938

35392

35618

35826

36017

36157

36273

6.8

33050

34106

35077

35510

35725

35919

36096

36229

36341

7.0

33300

34295

35211

35625

35833

36012

36174

36300

36407

7.2

33551

34481

35340

35738

35940

36105

36252

36370

36472

7.4

33801

34666

35467

35848

36046

36198

36330

36440

36537

7.6

34050

34847

35591

35956

36151

36290

36408

36509

36601

7.8

34295

35027

35713

36063

36255

36382

36486

36578

36664

8.0

34535

35204

35835

36169

36357

36473

36564

36647

36726

8.2

34770

35378

35956

36274

36457

36563

36643

36716

36788

8.4

34997

35550

36079

36378

36555

36651

36721

36785

36849

8.6

35215

35719

36203

36482

36650

36738

36799

36854

36911

8.8

35424

35885

36329

36587

36741

36823

36877

36924

36971

9.0

35623

36047

36458

36691

36831

36905

36955

36994

37032

9.2

35814

36207

36587

36796

36918

36987

37033

37064

37093

9.4

35997

36364

36717

36900

37003

37067

37111

37134

37153

9.6

36173

36517

36847

37004

37087

37145

37188

37204

37214

08.01.334

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SIX (WSTA 785.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

9.8

36343

36668

36976

37107

37170

37223

37264

37273

37274

10.0

36507

36814

37103

37209

37252

37300

37338

37341

37334

10.2

36667

36958

37228

37311

37335

37376

37412

37409

37395

10.4

36823

37098

37349

37411

37418

37451

37483

37476

37455

10.6

36976

37234

37468

37511

37502

37527

37553

37541

37516

10.8

37127

37367

37581

37609

37587

37602

37621

37605

37577

11.0

37275

37496

37691

37706

37673

37677

37688

37668

37638

11.2

37422

37623

37797

37801

37760

37752

37752

37730

37699

11.4

37568

37747

37900

37895

37847

37826

37816

37791

37759

11.6

37713

37869

38000

37988

37934

37901

37879

37851

37819

11.8

37858

37989

38098

38079

38021

37975

37941

37911

37879

12.0

38003

38108

38193

38168

38106

38048

38003

37970

37938

12.2

38148

38226

38287

38255

38191

38121

38065

38028

37995

12.4

38293

38344

38380

38341

38274

38194

38128

38086

38052

12.6

38440

38462

38471

38425

38354

38266

38191

38145

38107

12.8

38587

38579

38562

38507

38433

38338

38254

38203

38161

13.0

38735

38697

38653

38588

38509

38408

38319

38261

38214

13.2

38882

38813

38743

38667

38584

38478

38383

38319

38266

13.4

39027

38929

38832

38745

38656

38548

38448

38377

38317

13.6

39168

39042

38921

38821

38727

38616

38513

38434

38367

Original

07-14-08

08.01.335

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE =-2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

37456

37704

37870

38016

38142

38252

38338

38397

38482

3.2

37545

37780

37938

38075

38195

38299

38381

38438

38519

3.4

37633

37856

38005

38134

38247

38346

38424

38478

38557

3.6

37720

37930

38071

38193

38299

38393

38467

38519

38594

3.8

37805

38004

38137

38251

38352

38440

38510

38560

38631

4.0

37889

38077

38202

38310

38404

38487

38553

38600

38669

4.2

37970

38148

38266

38367

38456

38534

38597

38641

38706

4.4

38050

38218

38329

38424

38508

38582

38641

38682

38743

4.6

38126

38286

38391

38481

38560

38629

38685

38723

38780

4.8

38200

38352

38452

38537

38612

38677

38729

38764

38818

5.0

38272

38417

38511

38593

38664

38725

38773

38805

38855

5.2

38341

38480

38570

38648

38715

38773

38817

38846

38892

5.4

38409

38541

38628

38702

38766

38820

38861

38887

38929

5.6

38476

38602

38684

38756

38817

38867

38905

38927

38966

5.8

38542

38662

38741

38809

38867

38914

38949

38968

39003

6.0

38607

38721

38796

38861

38916

38960

38992

39008

39039

6.2

38672

38780

38851

38912

38964

39006

39034

39048

39076

6.4

38738

38840

38905

38963

39012

39050

39076

39088

39112

6.6

38805

38899

38959

39013

39059

39094

39117

39127

39149

6.8

38872

38959

39013

39062

39104

39136

39158

39165

39185

7.0

38941

39019

39066

39110

39149

39178

39197

39203

39221

7.2

39010

39079

39119

39158

39193

39219

39236

39240

39256

08.01.336

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE =-2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.4

39079

39139

39172

39206

39236

39259

39274

39277

39292

7.6

39148

39199

39225

39253

39279

39298

39311

39314

39327

7.8

39217

39259

39278

39300

39322

39338

39348

39350

39362

8.0

39286

39319

39330

39347

39364

39377

39385

39386

39396

8.2

39353

39378

39383

39394

39407

39416

39422

39422

39430

8.4

39419

39437

39436

39441

39449

39455

39458

39457

39464

8.6

39483

39494

39489

39489

39492

39494

39495

39492

39497

8.8

39546

39551

39542

39537

39536

39534

39532

39527

39530

9.0

39606

39608

39595

39585

39580

39574

39568

39561

39562

9.2

39665

39663

39647

39634

39624

39614

39605

39596

39594

9.4

39723

39717

39700

39683

39669

39654

39642

39630

39625

9.6

39779

39770

39751

39731

39713

39694

39679

39665

39657

9.8

39834

39823

39802

39779

39757

39734

39716

39699

39688

10.0

39887

39874

39852

39826

39800

39774

39752

39733

39720

10.2

39940

39924

39901

39872

39843

39813

39789

39767

39751

10.4

39992

39974

39949

39917

39885

39852

39825

39801

39782

10.6

40043

40022

39995

39961

39926

39891

39862

39836

39814

10.8

40093

40069

40040

40003

39966

39929

39898

39870

39846

11.0

40143

40115

40083

40044

40005

39967

39934

39904

39878

11.2

40192

40160

40125

40084

40044

40004

39969

39938

39911

11.4

40241

40205

40166

40123

40081

40040

40005

39973

39943

11.6

40289

40249

40206

40160

40118

40076

40040

40006

39975

Original

07-14-08

08.01.337

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE =-2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.8

40337

40293

40245

40198

40154

40112

40074

40040

40007

12.0

40384

40336

40284

40235

40190

40147

40109

40073

40039

FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

37246

37534

37732

37893

38032

38158

38254

38320

38410

3.2

37342

37616

37803

37954

38087

38207

38299

38363

38450

3.4

37438

37696

37873

38016

38141

38256

38344

38406

38490

3.6

37532

37777

37943

38078

38196

38305

38389

38449

38530

3.8

37625

37856

38012

38139

38251

38354

38435

38492

38570

4.0

37716

37934

38081

38200

38305

38403

38480

38535

38610

4.2

37805

38011

38149

38261

38360

38453

38526

38578

38649

4.4

37892

38086

38217

38322

38416

38503

38571

38620

38689

4.6

37976

38160

38283

38383

38471

38553

38617

38663

38728

4.8

38057

38232

38349

38444

38526

38604

38663

38706

38767

5.0

38135

38302

38414

38504

38582

38654

38710

38749

38806

5.2

38211

38371

38478

38563

38637

38705

38756

38791

38844

5.4

38286

38439

38541

38623

38692

38755

38802

38834

38883

08.01.338

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

5.6

38359

38505

38603

38681

38747

38806

38848

38876

38921

5.8

38430

38570

38664

38739

38801

38855

38893

38918

38960

6.0

38501

38635

38724

38795

38854

38904

38939

38960

38998

6.2

38572

38699

38783

38851

38906

38953

38983

39002

39036

6.4

38643

38762

38842

38906

38957

39000

39027

39043

39074

6.6

38714

38825

38899

38959

39006

39046

39071

39084

39112

6.8

38785

38889

38956

39011

39054

39091

39113

39125

39150

7.0

38858

38952

39012

39061

39101

39135

39155

39165

39188

7.2

38930

39015

39068

39111

39147

39178

39196

39205

39226

7.4

39003

39078

39123

39160

39192

39220

39236

39244

39263

7.6

39076

39140

39177

39209

39236

39261

39276

39283

39301

7.8

39148

39203

39232

39257

39279

39302

39316

39322

39337

8.0

39220

39265

39286

39305

39323

39343

39355

39360

39374

8.2

39291

39327

39341

39353

39367

39383

39394

39397

39410

8.4

39362

39389

39396

39402

39410

39424

39432

39435

39446

8.6

39431

39451

39452

39452

39455

39465

39471

39472

39481

8.8

39499

39512

39508

39502

39500

39506

39509

39508

39515

9.0

39566

39573

39564

39553

39545

39547

39547

39544

39548

9.2

39631

39633

39620

39604

39591

39588

39585

39580

39582

9.4

39695

39692

39677

39656

39637

39630

39624

39616

39614

9.6

39757

39751

39732

39707

39683

39671

39662

39651

39647

9.8

39818

39808

39787

39758

39729

39712

39699

39686

39679

Original

07-14-08

08.01.339

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

10.0

39877

39864

39841

39808

39774

39754

39737

39721

39711

10.2

39935

39919

39893

39857

39819

39795

39775

39757

39744

10.4

39991

39972

39944

39904

39863

39836

39813

39792

39776

10.6

40046

40023

39993

39951

39906

39876

39851

39827

39809

10.8

40099

40073

40040

39995

39949

39916

39889

39863

39841

11.0

40150

40120

40085

40038

39990

39956

39927

39899

39874

11.2

40200

40167

40128

40080

40030

39995

39964

39934

39908

11.4

40249

40212

40170

40120

40070

40034

40002

39970

39941

11.6

40297

40256

40211

40159

40109

40072

40039

40005

39974

11.8

40344

40299

40251

40198

40147

40110

40076

40040

40007

12.0

40390

40342

40290

40236

40185

40147

40112

40075

40039

FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

36998

37338

37585

37786

37950

38095

38201

38271

38366

3.2

37103

37426

37659

37852

38006

38145

38247

38316

38408

3.4

37207

37513

37733

37916

38063

38196

38293

38360

38450

3.6

37311

37599

37807

37981

38120

38247

38340

38404

38492

3.8

37412

37684

37880

38045

38177

38298

38386

38448

38533

08.01.340

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

4.0

37512

37769

37954

38110

38234

38349

38433

38493

38574

4.2

37609

37852

38026

38174

38292

38401

38480

38537

38615

4.4

37705

37934

38098

38239

38350

38453

38527

38580

38656

4.6

37797

38014

38170

38304

38408

38505

38574

38624

38696

4.8

37886

38093

38241

38368

38467

38558

38621

38668

38736

5.0

37973

38170

38312

38433

38526

38611

38668

38711

38776

5.2

38058

38246

38382

38498

38585

38663

38715

38755

38815

5.4

38140

38320

38451

38562

38644

38716

38762

38798

38854

5.6

38220

38393

38518

38625

38703

38769

38809

38841

38893

5.8

38299

38465

38585

38687

38761

38821

38856

38884

38932

6.0

38377

38535

38651

38749

38817

38872

38903

38926

38971

6.2

38454

38605

38716

38809

38873

38923

38949

38969

39010

6.4

38531

38674

38779

38867

38927

38973

38994

39011

39049

6.6

38608

38742

38841

38924

38980

39022

39040

39054

39088

6.8

38684

38810

38901

38979

39031

39069

39084

39096

39127

7.0

38761

38876

38960

39033

39080

39115

39128

39138

39167

7.2

38838

38943

39019

39085

39128

39161

39172

39180

39206

7.4

38915

39009

39076

39136

39174

39205

39215

39221

39245

7.6

38991

39075

39133

39187

39220

39249

39257

39262

39284

7.8

39068

39140

39190

39237

39266

39292

39299

39303

39323

8.0

39144

39205

39247

39287

39311

39335

39340

39343

39361

8.2

39220

39271

39304

39337

39355

39377

39381

39383

39399

Original

07-14-08

08.01.341

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

8.4

39296

39336

39361

39387

39400

39419

39422

39422

39436

8.6

39370

39402

39420

39438

39446

39461

39462

39460

39472

8.8

39445

39468

39479

39491

39492

39503

39501

39497

39507

9.0

39518

39534

39539

39544

39538

39546

39540

39535

39542

9.2

39591

39600

39599

39597

39585

39588

39579

39571

39576

9.4

39662

39665

39659

39651

39632

39630

39618

39607

39609

9.6

39732

39729

39719

39704

39680

39673

39657

39643

39642

9.8

39800

39791

39778

39758

39727

39715

39695

39679

39675

10.0

39865

39853

39836

39810

39774

39757

39734

39714

39707

10.2

39929

39912

39892

39862

39820

39800

39773

39750

39740

10.4

39990

39969

39946

39912

39866

39842

39811

39786

39773

10.6

40049

40024

39998

39961

39911

39884

39851

39822

39806

10.8

40105

40077

40048

40008

39956

39926

39890

39859

39839

11.0

40158

40126

40095

40053

40000

39968

39930

39895

39872

11.2

40209

40174

40140

40097

40043

40010

39969

39932

39906

11.4

40258

40220

40184

40140

40085

40051

40009

39969

39940

11.6

40305

40265

40226

40181

40127

40091

40048

40006

39974

11.8

40352

40308

40266

40222

40168

40132

40087

40042

40008

12.0

40398

40351

40307

40262

40208

40171

40125

40078

40041

08.01.342

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

36686

37101

37416

37693

37912

38043

38126

38203

38306

3.2

36801

37195

37495

37761

37972

38097

38174

38250

38350

3.4

36915

37289

37573

37829

38032

38150

38223

38296

38394

3.6

37028

37382

37652

37897

38092

38204

38272

38343

38438

3.8

37139

37474

37730

37965

38152

38258

38321

38389

38481

4.0

37249

37566

37809

38034

38213

38312

38370

38435

38524

4.2

37357

37657

37887

38102

38274

38366

38419

38480

38567

4.4

37462

37746

37965

38171

38335

38420

38468

38526

38609

4.6

37565

37834

38042

38241

38397

38475

38517

38571

38651

4.8

37665

37921

38120

38310

38460

38530

38566

38616

38692

5.0

37762

38007

38196

38380

38522

38586

38615

38661

38733

5.2

37857

38091

38273

38449

38585

38641

38664

38706

38773

5.4

37950

38173

38348

38518

38647

38697

38713

38750

38814

5.6

38041

38254

38423

38586

38709

38752

38762

38794

38854

5.8

38129

38334

38496

38654

38770

38806

38811

38838

38894

6.0

38217

38413

38568

38720

38831

38860

38859

38883

38934

6.2

38303

38489

38638

38785

38890

38914

38908

38927

38974

6.4

38387

38565

38707

38848

38948

38966

38955

38971

39014

6.6

38471

38639

38774

38909

39004

39018

39003

39015

39055

6.8

38555

38712

38839

38968

39059

39068

39050

39059

39096

7.0

38637

38783

38902

39025

39112

39118

39096

39102

39137

Original

07-14-08

08.01.343

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

38719

38854

38963

39081

39163

39166

39142

39146

39178

7.4

38801

38924

39024

39135

39213

39214

39188

39190

39219

7.6

38883

38993

39084

39189

39263

39261

39233

39233

39260

7.8

38964

39062

39143

39242

39312

39307

39277

39276

39300

8.0

39045

39131

39203

39294

39360

39353

39321

39318

39341

8.2

39127

39200

39262

39347

39408

39398

39364

39360

39380

8.4

39208

39270

39322

39400

39456

39442

39407

39400

39419

8.6

39290

39340

39383

39454

39504

39487

39449

39440

39456

8.8

39372

39411

39445

39508

39553

39531

39490

39479

39493

9.0

39454

39482

39508

39563

39601

39575

39531

39518

39529

9.2

39535

39553

39572

39619

39651

39619

39571

39555

39564

9.4

39616

39624

39635

39675

39700

39663

39611

39592

39598

9.6

39694

39694

39698

39731

39749

39707

39651

39629

39632

9.8

39771

39763

39760

39786

39798

39751

39690

39666

39666

10.0

39845

39830

39821

39841

39847

39795

39730

39702

39699

10.2

39916

39895

39880

39895

39896

39838

39770

39739

39732

10.4

39984

39957

39938

39948

39944

39882

39810

39775

39766

10.6

40048

40016

39993

40000

39992

39926

39850

39812

39800

10.8

40107

40071

40046

40050

40039

39971

39891

39850

39834

11.0

40163

40124

40096

40099

40086

40015

39932

39888

39868

11.2

40215

40174

40145

10146

40132

40059

39973

39926

39903

11.4

40265

40221

40191

40192

40177

40102

40015

39964

39938

11.6

40312

40267

40236

40236

40221

40145

40056

40002

39972

08.01.344

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.8

40358

40312

40279

40279

40264

40188

40096

40040

40007

12.0

40403

40355

40321

40322

40307

40229

40136

40077

40042

FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

36319

36822

37203

37561

37841

37956

38024

38115

38230

3.2

36445

36924

37287

37633

37905

38013

38076

38165

38277

3.4

36571

37026

37372

37706

37969

38070

38128

38214

38323

3.6

36696

37127

37456

37778

38033

38127

38180

38263

38370

3.8

36819

37227

37540

37851

38098

38184

38232

38312

38416

4.0

36940

37327

37624

37924

38163

38242

38283

38360

38461

4.2

37060

37427

37709

37997

38228

38299

38335

38409

38506

4.4

37177

37525

37793

38071

38293

38357

38387

38457

38551

4.6

37293

37623

37878

38145

38359

38415

38438

38504

38595

4.8

37405

37719

37962

38220

38425

38473

38490

38551

38638

5.0

37515

37814

38046

38294

38492

38531

38541

38598

38681

5.2

37622

37908

38130

38369

38558

38590

38592

38645

38723

5.4

37727

38001

38213

38443

38624

38648

38643

38691

38765

Original

07-14-08

08.01.345

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

5.6

37830

38091

38295

38517

38690

38705

38694

38737

38807

5.8

37930

38181

38375

38590

38755

38763

38745

38783

38848

6.0

38029

38268

38454

38661

38819

38820

38796

38829

38890

6.2

38125

38353

38532

38731

38882

38876

38846

38874

38932

6.4

38219

38437

38607

38799

38944

38932

38896

38920

38974

6.6

38312

38518

38679

38865

39005

38987

38946

38966

39016

6.8

38403

38597

38749

38928

39063

39040

38995

39013

39059

7.0

38493

38674

38817

38990

39120

39093

39045

39059

39102

7.2

38581

38749

38883

39049

39176

39146

39094

39105

39145

7.4

38669

38823

38947

39108

39231

39197

39142

39151

39188

7.6

38756

38897

39010

39165

39284

39247

39190

39196

39231

7.8

38843

38970

39073

39221

39337

39297

39237

39241

39273

8.0

38930

39043

39135

39277

39389

39346

39284

39286

39315

8.2

39018

39116

39197

39333

39441

39395

39330

39330

39357

8.4

39106

39190

39260

39389

39492

39443

39375

39373

39397

8.6

39195

39265

39324

39445

39544

39490

39419

39415

39437

8.8

39286

39341

39390

39502

39595

39537

39462

39455

39475

9.0

39377

39418

39456

39560

39647

39583

39505

39495

39513

9.2

39468

39496

39522

39618

39699

39630

39547

39535

39549

9.4

39558

39573

39589

39676

39750

39675

39588

39573

39585

9.6

39647

39650

39655

39735

39802

39721

39630

39611

39621

9.8

39733

39725

39721

39793

39853

39767

39671

39649

39656

10.0

39816

39798

39786

39850

39904

39812

39712

39687

39690

08.01.346

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = 0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

10.2

39896

39868

39849

39907

39956

39858

39753

39725

39725

10.4

39971

39936

39911

39963

40006

39904

39794

39763

39759

10.6

40041

40000

39970

40017

40057

39950

39836

39801

39794

10.8

40105

40060

40026

40071

40107

39996

39878

39840

39830

11.0

40164

40116

40080

40123

40157

40043

39921

39879

39865

11.2

40218

40168

40132

40174

40206

40089

39964

39918

39901

11.4

40269

40218

40182

40223

40254

40135

40007

39957

39936

11.6

40317

40266

40230

40271

40301

40180

40050

39997

39972

11.8

40362

40312

40276

40318

40347

40225

40092

40036

40008

12.0

40406

40356

40322

40363

40392

40269

40134

40074

40043

FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

35860

36487

36973

37356

37625

37796

37915

38024

38148

3.2

36001

36599

37063

37432

37692

37857

37970

38077

38197

3.4

36142

36711

37154

37509

37760

37918

38026

38129

38247

3.6

36281

36822

37245

37586

37828

37979

38082

38181

38296

3.8

36420

36933

37336

37663

37897

38040

38137

38233

38344

Original

07-14-08

08.01.347

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

4.0

36556

37044

37427

37741

37965

38101

38193

38285

38392

4.2

36691

37154

37519

37819

38034

38162

38248

38336

38440

4.4

36824

37264

37610

37898

38103

38223

38303

38387

38487

4.6

36955

37373

37703

37977

38173

38285

38357

38437

38533

4.8

37083

37481

37795

38057

38243

38346

38412

38487

38578

5.0

37208

37588

37888

38137

38313

38407

38466

38536

38623

5.2

37331

37694

37980

38218

38383

38468

38520

38585

38667

5.4

37451

37798

38071

38297

38453

38529

38574

38633

38711

5.6

37568

37900

38161

38377

38522

38590

38628

38681

38755

5.8

37683

38001

38250

38455

38591

38650

38681

38729

38798

6.0

37795

38099

38337

38532

38659

38710

38734

38777

38841

6.2

37903

38194

38421

38607

38726

38770

38787

38825

38885

6.4

38009

38287

38503

38680

38791

38829

38840

38873

38928

6.6

38113

38376

38582

38751

38855

38887

38893

38922

38972

6.8

38213

38463

38658

38819

38918

38944

38945

38970

39017

7.0

38311

38546

38731

38884

38979

39001

38998

39019

39061

7.2

38407

38627

38801

38948

39038

39056

39050

39067

39106

7.4

38501

38707

38870

39010

39097

39111

39101

39115

39151

7.6

38595

38785

38937

39071

39154

39166

39152

39163

39196

7.8

38689

38863

39003

39131

39211

39219

39203

39211

39241

8.0

38782

38941

39069

39190

39266

39272

39252

39258

39285

8.2

38877

39019

39135

39249

39321

39323

39301

39304

39328

8.4

38973

39098

39201

39308

39376

39375

39349

39349

39370

08.01.348

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

8.6

39071

39179

39269

39367

39430

39425

39396

39393

39412

8.8

39171

39261

39337

39427

39485

39474

39442

39436

39452

9.0

39272

39345

39407

39487

39539

39523

39487

39478

39491

9.2

39374

39430

39478

39548

39592

39572

39531

39519

39530

9.4

39476

39515

39549

39608

39646

39619

39574

39560

39567

9.6

39575

39599

39619

39669

39700

39667

39617

39599

39604

9.8

39672

39681

39689

39730

39753

39715

39660

39639

39641

10.0

39766

39761

39758

39790

39807

39762

39703

39678

39677

10.2

39855

39839

39826

39850

39860

39810

39745

39717

39713

10.4

39939

39913

39891

39909

39913

39857

39789

39757

39749

10.6

40016

39982

39955

39967

39966

39906

39832

39797

39785

10.8

40085

40047

40015

40023

40019

39954

39876

39837

39822

11.0

40149

40107

40074

40079

40072

40003

39921

39877

39859

11.2

40206

40163

40129

40134

40124

40052

39965

39918

39896

11.4

40259

40216

40183

40187

40176

40100

40010

39959

39933

11.6

40308

40266

40234

40239

40227

40148

40055

40000

39969

11.8

40354

40313

40284

40289

40276

40196

40099

40040

40006

12.0

40398

40359

40332

40338

40325

40242

40142

40080

40043

Original

07-14-08

08.01.349

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

35199

35990

36659

37115

37382

37621

37799

37937

38064

3.2

35364

36119

36758

37196

37454

37686

37858

37992

38117

3.4

35528

36248

36858

37278

37526

37750

37917

38047

38168

3.6

35691

36376

36958

37359

37598

37814

37975

38102

38220

3.8

35852

36504

37058

37442

37670

37878

38034

38156

38271

4.0

36012

36631

37159

37525

37743

37943

38092

38211

38322

4.2

36170

36758

37260

37608

37816

38007

38150

38264

38371

4.4

36325

36884

37362

37693

37889

38072

38208

38317

38421

4.6

36477

37010

37464

37778

37963

38136

38266

38370

38469

4.8

36627

37134

37566

37863

38037

38201

38323

38422

38517

5.0

36773

37257

37669

37950

38111

38265

38380

38473

38563

5.2

36916

37379

37772

38036

38186

38330

38437

38524

38610

5.4

37056

37499

37873

38122

38260

38394

38494

38575

38655

5.6

37192

37616

37973

38208

38333

38458

38550

38625

38701

5.8

37325

37731

38072

38292

38406

38522

38606

38676

38746

6.0

37454

37843

38168

38375

38479

38585

38662

38726

38791

6.2

37580

37951

38262

38456

38550

38648

38718

38776

38837

6.4

37701

38056

38352

38534

38619

38710

38774

38826

38882

6.6

37818

38157

38439

38610

38687

38771

38829

38877

38928

6.8

37932

38254

38521

38683

38754

38832

38885

38928

38975

7.0

38042

38347

38600

38753

38819

38892

38940

38979

39021

7.2

38149

38437

38677

38821

38882

38951

38995

39030

39068

08.01.350

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.4

38255

38525

38750

38887

38944

39009

39049

39080

39115

7.6

38359

38611

38822

38951

39005

39066

39103

39131

39162

7.8

38463

38697

38893

39014

39065

39123

39157

39180

39209

8.0

38568

38782

38963

39076

39124

39178

39209

39230

39255

8.2

38673

38868

39034

39138

39183

39233

39260

39278

39300

8.4

38781

38955

39104

39200

39240

39287

39311

39325

39344

8.6

38891

39045

39177

39262

39298

39340

39360

39371

39387

8.8

39004

39136

39250

39325

39355

39391

39408

39416

39429

9.0

39119

39230

39325

39388

39411

39443

39455

39460

39470

9.2

39235

39325

39401

39452

39468

39493

39501

39503

39510

9.4

39350

39419

39477

39516

39524

39543

39546

39545

39550

9.6

39464

39513

39553

39580

39580

39593

39591

39586

39588

9.8

39575

39605

39628

39644

39637

39642

39635

39627

39626

10.0

39682

39695

39703

39707

39693

39692

39679

39668

39664

10.2

39783

39781

39775

39771

39749

39742

39724

39709

39702

10.4

39877

39863

39846

39833

39805

39792

39769

39750

39739

10.6

39963

39940

39914

39894

39861

39842

39814

39791

39777

10.8

40040

40010

39980

39955

39917

39893

39860

39833

39815

11.0

40108

40076

40042

40014

39973

39945

39907

39875

39854

11.2

40170

40136

40102

40073

40029

39996

39954

39918

39892

11.4

40226

40193

40160

40130

40084

40048

40001

39960

39930

11.6

40277

40246

40215

40185

40138

40099

40047

40003

39969

Original

07-14-08

08.01.351

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

11.8

40325

40296

40269

40239

40190

40149

40093

40045

40007

12.0

40370

40344

40320

40291

40242

40198

40139

40087

40045

FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

32985

34444

35812

36512

36919

37243

37513

37700

37860

3.2

33237

34631

35939

36612

37004

37317

37578

37761

37917

3.4

33487

34817

36066

36711

37089

37391

37644

37822

37974

3.6

33735

35003

36194

36811

37175

37466

37709

37882

38031

3.8

33979

35186

36322

36912

37261

37540

37774

37943

38087

4.0

34220

35368

36449

37013

37347

37615

37840

38003

38143

4.2

34455

35548

36577

37115

37434

37690

37905

38062

38198

4.4

34685

35726

36706

37217

37522

37765

37971

38122

38252

4.6

34910

35901

36834

37321

37610

37841

38036

38180

38306

4.8

35127

36073

36962

37425

37690

37917

38102

38239

38358

5.0

35338

36242

37090

37530

37788

37993

38167

38297

38410

5.2

35543

36407

37218

37634

37877

38069

38232

38355

38462

5.4

35741

36568

37343

37738

37966

38145

38297

38412

38513

08.01.352

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

5.6

35933

36726

37467

37841

38054

38220

38362

38469

38564

5.8

36119

36879

37589

37943

38141

38295

38427

38526

38614

6.0

36299

37028

37707

38042

38227

38369

38491

38583

38665

6.2

36473

37171

37821

38139

38311

38442

38555

38640

38716

6.4

36641

37310

37931

38232

38392

38514

38618

38697

38767

6.6

36803

37443

38037

38322

38472

38585

38681

38754

38819

6.8

36960

37571

38137

38407

38548

38654

38744

38811

38871

7.0

37112

37694

38233

38489

38622

38721

38806

38868

38924

7.2

37260

37813

38325

38568

38694

38787

38867

38925

38976

7.4

37406

37929

38414

38644

38764

38852

38927

38982

39029

7.6

37550

38043

38501

38719

38833

38916

38987

39038

39082

7.8

37693

38155

38586

38792

38900

38979

39046

39093

39134

8.0

37837

38268

38671

38864

38966

39041

39103

39147

39185

8.2

37982

38381

38756

38936

39031

39101

39160

39201

39235

8.4

38129

38496

38842

39007

39096

39161

39216

39253

39284

8.6

38279

38614

38929

39080

39161

39220

39270

39304

39331

8.8

38433

38735

39019

39154

39226

39279

39323

39353

39377

9.0

38590

38858

39111

39229

39291

39337

39375

39401

39421

9.2

38747

38982

39203

39305

39357

39394

39426

39448

39464

9.4

38902

39105

39297

39381

39422

39452

39477

39493

39506

9.6

39055

39227

39389

39456

39487

39508

39527

39539

39547

9.8

39204

39347

39481

39532

39553

39565

39577

39584

39588

Original

07-14-08

08.01.353

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER SEVEN (WSTA 865.7) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

10.0

39346

39462

39571

39607

39617

39622

39627

39629

39628

10.2

39479

39572

39658

39680

39682

39679

39678

39673

39668

10.4

39603

39675

39742

39753

39746

39736

39728

39719

39709

10.6

39714

39771

39822

39823

39810

39793

39780

39765

39750

10.8

39813

39858

39898

39892

39873

39851

39832

39811

39791

11.0

39900

39937

39969

39959

39936

39909

39885

39859

39833

11.2

39975

40009

40036

40023

39997

39967

39938

39907

39876

11.4

40044

40074

40100

40086

40058

40024

39991

39954

39918

11.6

40105

40135

40161

40146

40117

40081

40044

40002

39961

11.8

40161

40192

40219

40204

40174

40136

40096

40049

40003

12.0

40214

40246

40274

40260

40230

40190

40147

40096

40045

FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE =-2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

39202

39373

39491

39592

39677

39749

39806

39844

39900

3.2

39274

39436

39547

39641

39722

39790

39843

39880

39933

3.4

39346

39499

39602

39691

39767

39831

39881

39915

39965

3.6

39415

39560

39656

39740

39811

39871

39918

39950

39997

08.01.354

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE =-2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.8

39484

39620

39710

39787

39855

39911

39955

39984

40029

4.0

39550

39678

39762

39834

39897

39950

39991

40018

40060

4.2

39614

39734

39812

39880

39939

39988

40027

40052

40091

4.4

39676

39789

39861

39924

39980

40026

40062

40085

40122

4.6

39734

39841

39908

39967

40019

40062

40095

40117

40151

4.8

39790

39890

39954

40009

40057

40097

40128

40148

40180

5.0

39843

39937

39997

40049

40094

40131

40160

40178

40208

5.2

39894

39983

40039

40088

40130

40165

40192

40208

40236

5.4

39943

40026

40080

40125

40165

40197

40223

40237

40263

5.6

39990

40069

40120

40163

40200

40230

40253

40266

40290

5.8

40037

40111

40159

40199

40234

40261

40283

40295

40317

6.0

40083

40152

40198

40236

40268

40293

40313

40323

40344

6.2

40128

40194

40237

40272

40302

40325

40342

40352

40370

6.4

40174

40235

40276

40308

40336

40356

40372

40380

40397

6.6

40221

40278

40316

40345

40370

40388

40402

40409

40423

6.8

40269

40321

40356

40383

40405

40421

40433

40437

40450

7.0

40317

40365

40397

40421

40440

40453

40463

40466

40477

7.2

40366

40410

40439

40459

40476

40486

40494

40496

40504

7.4

40415

40455

40480

40497

40511

40519

40525

40525

40531

7.6

40465

40500

40522

40535

40547

40553

40556

40554

40558

7.8

40514

40545

40563

40574

40582

40585

40587

40583

40585

8.0

40562

40589

40604

40612

40617

40618

40617

40612

40612

Original

07-14-08

08.01.355

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE =-2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

8.2

40610

40633

40644

40649

40652

40651

40648

40641

40639

8.4

40657

40676

40683

40685

40686

40682

40677

40669

40666

8.6

40702

40718

40722

40721

40720

40714

40707

40697

40692

8.8

40746

40758

40759

40756

40752

40744

40736

40724

40718

9.0

40788

40797

40795

40790

40784

40774

40764

40752

40744

9.2

40829

40835

40830

40823

40815

40804

40792

40778

40769

9.4

40868

40871

40864

40855

40845

40832

40819

40804

40794

9.6

40905

40906

40896

40885

40874

40860

40846

40830

40818

9.8

40941

40939

40927

40915

40902

40887

40872

40855

40842

10.0

40975

40971

40958

40944

40930

40914

40897

40880

40866

10.2

41007

41002

40987

40972

40956

40939

40922

40904

40889

10.4

41038

41031

41014

40998

40982

40964

40946

40927

40911

10.6

41067

41058

41041

41024

41007

40988

40969

40950

40934

10.8

41095

41084

41066

41048

41031

41011

40992

40973

40955

11.0

41120

41109

41090

41072

41054

41034

41014

40994

40976

08.01.356

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

39054

39253

39392

39502

39594

39678

39743

39789

39851

3.2

39129

39318

39450

39553

39640

39720

39782

39825

39884

3.4

39203

39382

39506

39604

39686

39762

39820

39861

39918

3.6

39276

39446

39563

39654

39731

39803

39859

39897

39951

3.8

39348

39508

39618

39704

39776

39845

39897

39933

39984

4.0

39418

39570

39672

39753

39820

39885

39934

39968

40016

4.2

39487

39630

39726

39801

39864

39925

39972

40003

40048

4.4

39554

39689

39778

39848

39907

39965

40008

40037

40080

4.6

39619

39745

39829

39894

39949

40003

40044

40071

40112

4.8

39682

39800

39878

39939

39990

40041

40079

40105

40143

5.0

39742

39853

39926

39983

40030

40078

40114

40137

40173

5.2

39800

39905

39973

40026

40070

40115

40148

40170

40203

5.4

39857

39955

40019

40067

40108

40151

40182

40202

40233

5.6

39912

40003

40063

40109

40146

40186

40215

40233

40262

5.8

39966

40051

40107

40149

40184

40221

40248

40264

40291

6.0

40018

40098

40150

40189

40221

40255

40280

40295

40320

6.2

40070

40144

40192

40228

40257

40289

40312

40326

40348

6.4

40120

40189

40234

40267

40294

40323

40344

40356

40376

6.6

40170

40234

40276

40306

40330

40356

40376

40386

40404

6.8

40220

40279

40317

40345

40365

40390

40407

40416

40432

7.0

40269

40323

40359

40383

40401

40423

40438

40445

40460

Original

07-14-08

08.01.357

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE = -1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

40318

40367

40400

40421

40437

40456

40469

40475

40487

7.4

40366

40412

40441

40459

40472

40489

40501

40504

40515

7.6

40415

40456

40482

40497

40508

40522

40532

40534

40542

7.8

40463

40500

40523

40536

40543

40556

40563

40563

40570

8.0

40511

40544

40564

40574

40579

40589

40594

40593

40597

8.2

40559

40588

40605

40612

40615

40622

40625

40622

40625

8.4

40608

40633

40646

40650

40650

40655

40656

40652

40652

8.6

40656

40677

40687

40688

40686

40689

40688

40681

40680

8.8

40704

40722

40728

40727

40722

40722

40719

40711

40708

9.0

40753

40766

40769

40764

40758

40756

40751

40741

40736

9.2

40800

40810

40810

40803

40793

40789

40782

40770

40763

9.4

40847

40854

40850

40840

40828

40822

40813

40800

40791

9.6

40892

40896

40889

40876

40863

40854

40843

40829

40818

9.8

40936

40936

40926

40912

40896

40885

40873

40857

40845

10.0

40978

40975

40962

40945

40928

40916

40902

40884

40871

10.2

41017

41012

40997

40978

40959

40945

40929

40911

40896

10.4

41053

41046

41029

41008

40988

40973

40956

40937

40920

10.6

41087

41077

41058

41037

41015

40999

40981

40961

40944

10.8

41117

41105

41085

41063

41040

41023

41005

40984

40966

11.0

41143

41130

41110

41087

41064

41046

41027

41006

40988

08.01.358

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

38880

39114

39291

39434

39539

39637

39704

39752

39821

3.2

38958

39182

39350

39486

39586

39679

39743

39789

39855

3.4

39036

39249

39409

39538

39633

39722

39782

39826

39889

3.6

39113

39315

39467

39590

39680

39765

39822

39862

39922

3.8

39189

39381

39525

39642

39727

39807

39860

39898

39955

4.0

39265

39447

39583

39693

39773

39849

39899

39934

39989

4.2

39339

39511

39639

39744

39819

39891

39937

39970

40022

4.4

39413

39575

39696

39794

39864

39932

39976

40006

40055

4.6

39486

39638

39751

39844

39909

39974

40013

40041

40087

4.8

39557

39700

39806

39893

39954

40014

40051

40076

40119

5.0

39627

39761

39859

39941

39997

40054

40088

40111

40152

5.2

39695

39820

39912

39989

40040

40094

40124

40145

40183

5.4

39761

39878

39964

40035

40083

40133

40161

40179

40215

5.6

39826

39935

40014

40081

40125

40171

40196

40213

40246

5.8

39890

39991

40064

40126

40166

40209

40231

40246

40277

6.0

39951

40045

40112

40170

40206

40247

40266

40279

40307

6.2

40010

40097

40159

40213

40245

40283

40300

40311

40337

6.4

40067

40147

40205

40255

40284

40319

40333

40343

40366

6.6

40121

40196

40249

40296

40322

40354

40366

40374

40395

6.8

40174

40242

40292

40335

40358

40388

40398

40404

40424

7.0

40224

40288

40334

40374

40394

40422

40430

40434

40452

Original

07-14-08

08.01.359

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE = -1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

40273

40332

40375

40412

40430

40455

40461

40464

40479

7.4

40320

40375

40415

40450

40465

40487

40492

40493

40507

7.6

40367

40417

40455

40487

40500

40520

40523

40523

40534

7.8

40414

40460

40495

40524

40535

40552

40554

40552

40562

8.0

40461

40502

40535

40561

40570

40585

40585

40581

40589

8.2

40508

40546

40575

40599

40605

40618

40616

40611

40617

8.4

40556

40590

40616

40637

40641

40652

40648

40641

40645

8.6

40606

40635

40658

40676

40678

40686

40680

40671

40673

8.8

40657

40682

40702

40716

40715

40721

40713

40702

40702

9.0

40710

40730

40746

40757

40753

40756

40746

40733

40731

9.2

40763

40778

40790

40797

40791

40791

40779

40765

40760

9.4

40815

40827

40834

40838

40830

40827

40812

40796

40790

9.6

40867

40874

40878

40878

40867

40862

40845

40827

40818

9.8

40917

40920

40920

40917

40904

40896

40877

40857

40847

10.0

40966

40965

40961

40954

40939

40929

40908

40886

40874

10.2

41011

41006

40999

40990

40973

40960

40938

40915

40901

10.4

41053

41045

41035

41024

41004

40990

40967

40942

40927

10.6

41091

41080

41068

41054

41034

41018

40993

40968

40951

10.8

41124

41111

41097

41082

41060

41043

41018

40992

40974

11.0

41153

41138

71123

41107

41084

41067

41041

41014

40996

08.01.360

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

38667

38950

39178

39388

39547

39620

39655

39704

39781

3.2

38749

39019

39238

39442

39596

39664

39695

39741

39815

3.4

38830

39089

39299

39496

39644

39708

39735

39779

39849

3.6

38912

39159

39360

39550

39693

39752

39775

39816

39883

3.8

38993

39229

39421

39604

39742

39796

39815

39853

39917

4.0

39075

39299

39482

39658

39790

39840

39855

39890

39951

4.2

39157

39370

39543

39712

39839

39884

39895

39927

39985

4.4

39239

39440

39604

39766

39888

39928

39935

39964

40020

4.6

39322

39511

39665

39821

39937

39972

39976

40001

40054

4.8

39404

39581

39726

39875

39985

40016

40016

40039

40088

5.0

39487

39562

39787

39929

40034

40060

40056

40076

40122

5.2

39568

39722

39848

39982

40082

40104

40096

40113

40156

5.4

39648

39790

39907

40035

40130

40147

40135

40149

40190

5.6

39727

39858

39966

40087

40177

40189

40174

40185

40223

5.8

39803

39923

40023

40138

40223

40231

40212

40221

40256

6.0

39876

39987

40078

40187

40268

40272

40250

40256

40289

6.2

39947

40047

40131

40235

40311

40312

40287

40290

40321

6.4

40013

40105

40182

40281

40353

40350

40322

40324

40352

6.6

40075

40159

40231

40325

40393

40387

40357

40357

40382

6.8

40132

40209

40276

40366

40431

40422

40390

40388

40412

7.0

40186

40257

40319

40405

40467

40456

40423

40419

40440

Original

07-14-08

08.01.361

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE = -.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

40236

40301

40361

40443

40502

40489

40454

40449

40469

7.4

40283

40344

40400

40480

40535

40521

40485

40479

40496

7.6

40329

40385

40439

40515

40569

40553

40516

40508

40524

7.8

40373

40425

40477

40551

40601

40584

40546

40537

40551

8.0

40417

40465

40515

40586

40634

40616

40577

40566

40579

8.2

40461

40506

40553

40621

40667

40647

40607

40596

40606

8.4

40507

40548

40592

40657

40700

40679

40638

40625

40634

8.6

40554

40591

40632

40695

40735

40712

40670

40656

40662

8.8

40603

40636

40674

40733

40770

40746

40703

40687

40691

9.0

40655

40684

40718

40773

40807

40780

40736

40718

40720

9.2

40707

40732

40762

40813

40844

40815

40769

40749

40750

9.4

40760

40780

40806

40853

40881

40850

40803

40781

40779

9.6

40813

40829

40850

40893

40918

40885

40836

40812

40808

9.8

40865

40877

40893

40932

40954

40919

40868

40843

40837

10.0

40915

40923

40935

40971

40989

40953

40900

40874

40866

10.2

40963

40967

40976

41007

41023

40985

40931

40903

40894

10.4

41009

41009

41014

41042

41055

41016

40961

40932

40920

10.6

41051

41047

41049

41074

41085

41045

40989

40959

40946

10.8

41088

41082

41081

41104

41113

41071

41015

40984

40970

11.0

41122

41114

41111

41131

41138

41096

41040

41008

40994

08.01.362

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE =0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

38424

38763

39034

39313

39530

39575

39585

39645

39732

3.2

38510

38836

39098

39369

39581

39620

39626

39683

39767

3.4

38597

38909

39161

39425

39631

39666

39668

39721

39802

3.6

38684

38983

39225

39482

39682

39712

39709

39760

39837

3.8

38772

39058

39289

39538

39733

39757

39751

39798

39872

4.0

38861

39133

39354

39596

39785

39804

39792

39836

39908

4.2

38951

39209

39419

39653

39837

39850

39834

39875

39943

4.4

39042

39286

39485

39711

39889

39897

39877

39914

39979

4.6

39134

39364

39552

39770

39942

39944

39919

39953

40015

4.8

39228

39443

39619

39829

39995

39992

39962

39993

40051

5.0

39322

39523

39687

39888

40048

40039

40005

40032

40088

5.2

39417

39602

39755

39948

40102

40087

40047

40071

40124

5.4

39510

39681

39821

40006

40154

40134

40090

40111

40160

5.6

39602

39758

39887

40064

40207

40181

40132

40149

40196

5.8

39691

39833

39952

40120

40257

40226

40174

40188

40231

6.0

39776

39906

40014

40175

40307

40271

40214

40225

40266

6.2

39858

39975

40074

40228

40354

40314

40254

40262

40300

6.4

39935

40041

40131

40278

40400

40355

40292

40298

40333

6.6

40005

40102

40184

40326

40442

40395

40329

40332

40365

6.8

40070

40158

40234

40370

40482

40432

40364

40366

40396

7.0

40129

40209

40280

40412

40520

40468

40398

40398

40426

Original

07-14-08

08.01.363

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE =0.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

40183

40257

40324

40451

40556

40502

40431

40429

40455

7.4

40233

40301

40365

40488

40589

40534

40463

40460

40484

7.6

40280

40344

40405

40524

40622

40566

40494

40490

40512

7.8

40324

40384

40443

40559

40654

40597

40525

40519

40539

8.0

40368

40424

40481

40594

40685

40628

40555

40549

40567

8.2

40411

40464

40518

40628

40716

40659

40586

40578

40595

8.4

40455

40504

40556

40663

40748

40690

40617

40608

40622

8.6

40500

40546

40595

40698

40780

40722

40648

40638

40651

8.8

40548

40590

40636

40735

40813

40754

40680

40668

40679

9.0

40597

40635

40677

40773

40847

40787

40712

40699

40708

9.2

40647

40681

40719

40811

40882

40821

40745

40730

40737

9.4

40699

40728

40762

40849

40917

40855

40778

40761

40766

9.6

40750

40775

40805

40888

40952

40889

40811

40793

40796

9.8

40802

40822

40847

40926

40987

40922

40843

40824

40825

10.0

40853

40868

40889

40964

41021

40955

40876

40854

40853

10.2

40902

40913

40930

41000

41054

40987

40907

40884

40882

10.4

40950

40957

40969

41036

41087

41019

40938

40913

40909

10.6

40995

40998

41007

41070

41117

41049

40967

40942

40936

10.8

41038

41037

41043

41102

41147

41077

40996

40969

40962

11.0

41079

41074

41076

41132

41174

41104

41023

40996

40987

08.01.364

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

38133

38549

38886

39164

39356

39457

39518

39589

39679

3.2

38226

38628

38953

39222

39409

39505

39561

39629

39716

3.4

38320

38707

39021

39281

39461

39552

39604

39668

39752

3.6

38415

38786

39088

39341

39514

39600

39647

39708

39788

3.8

38510

38866

39156

39400

39568

39648

39691

39748

39825

4.0

38607

38947

39225

39460

39622

39696

39734

39788

39861

4.2

38704

39029

39295

39521

39676

39745

39778

39828

39898

4.4

38803

39112

39365

39582

39731

39794

39823

39869

39935

4.6

38903

39196

39436

39644

39786

39844

39867

39910

39973

4.8

39005

39282

39508

39707

39842

39894

39912

39951

40010

5.0

39108

39368

39581

39770

39898

39944

39957

39992

40048

5.2

39210

39454

39654

39833

39955

39994

40003

40033

40086

5.4

39312

39540

39726

39896

40010

40044

40048

40075

40123

5.6

39413

39624

39797

39957

40066

40094

40092

40115

40161

5.8

39511

39707

39867

40018

40120

40142

40136

40156

40198

6.0

39605

39786

39934

40077

40173

40190

40179

40195

40234

6.2

39696

39863

40000

40134

40224

40236

40221

40234

40270

6.4

39782

39936

40062

40188

40273

40280

40262

40272

40304

6.6

39862

40004

40121

40240

40319

40323

40301

40308

40338

6.8

39937

40067

40175

40289

40363

40363

40339

40344

40371

7.0

40005

40126

40227

40334

40405

40402

40375

40378

40403

Original

07-14-08

08.01.365

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE = .50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

40069

40181

40275

40378

40444

40439

40410

40411

40433

7.4

40128

40232

40321

40419

40482

40474

40444

40443

40464

7.6

40184

40280

40365

40458

40518

40509

40477

40474

40493

7.8

40237

40327

40407

40497

40554

40542

40509

40505

40522

8.0

40288

40372

40448

40534

40588

40575

40541

40536

40551

8.2

40338

40416

40488

40571

40622

40608

40573

40566

40580

8.4

40387

40459

40528

40607

40656

40640

40605

40596

40608

8.6

40436

40503

40568

40644

40690

40673

40636

40627

40637

8.8

40486

40548

40609

40681

40725

40706

40668

40657

40666

9.0

40537

40593

40650

40719

40760

40739

40701

40688

40695

9.2

40588

40639

40692

40757

40795

40773

40733

40719

40724

9.4

40639

40685

40733

40795

40830

40807

40765

40750

40753

9.6

40690

40732

40775

40833

40866

40840

40798

40781

40782

9.8

40742

40778

40817

40871

40901

40874

40830

40812

40811

10.0

40793

40824

40859

40909

40936

40907

40862

40843

40840

10.2

40843

40869

40900

40946

40970

40940

40894

40873

40869

10.4

40893

40914

40940

40983

41004

40973

40926

40903

40898

10.6

40941

40958

40980

41019

41038

41005

40956

40933

40926

10.8

40989

41001

41018

41054

41070

41036

40987

40962

40953

11.0

41035

41042

41056

41088

41102

41066

41016

40998

40980

08.01.366

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHDS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

37720

38238

38683

38985

39159

39322

39441

39535

39627

3.2

37825

38325

38755

39047

39215

39372

39486

39576

39664

3.4

37930

38413

38828

39109

39270

39421

39531

39617

39702

3.6

38036

38501

38901

39172

39326

39471

39576

39659

39740

3.8

38143

38590

38974

39235

39382

39521

39621

39700

39778

4.0

38251

38679

39048

39298

39438

39572

39667

39741

39816

4.2

38359

38770

39123

39362

39495

39623

39712

39783

39854

4.4

38469

38861

39198

39426

39553

39674

39758

39825

39892

4.6

38580

38953

39274

39491

39610

39725

39805

39868

39931

4.8

38692

39046

39351

39557

39669

39777

39852

39910

39970

5.0

38805

39140

39428

39623

39727

39830

39899

39953

40009

5.2

38918

39234

39506

39689

39786

39882

39946

39996

40048

5.4

39030

39328

39583

39754

39844

39934

39992

40038

40087

5.6

39141

39420

39659

39819

39902

39985

40039

40081

40126

5.8

39250

39511

39733

39883

39959

40036

40084

40122

40164

6.0

39356

39599

39806

39946

40015

40086

40129

40164

40202

6.2

39458

39684

39877

40006

40069

40135

40174

40204

40239

6.4

39556

39766

39945

40065

40122

40182

40216

40243

40275

6.6

39649

39844

40010

40121

40172

40228

40258

40282

40310

6.8

39737

39918

40072

40174

40220

40271

40298

40319

40345

7.0

39819

39987

40130

40225

40267

40313

40337

40355

40378

Original

07-14-08

08.01.367

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE = 1.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHDS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

39897

40053

40186

40274

40311

40354

40374

40390

40411

7.4

39970

40115

40238

40320

40354

40393

40411

40424

40443

7.6

40039

40174

40289

40365

40395

40431

40446

40457

40474

7.8

40105

40230

40338

40408

40435

40467

40481

40490

40505

8.0

40169

40284

40385

40450

40474

40504

40515

40522

40535

8.2

40229

40336

40430

40491

40512

40539

40548

40554

40565

8.4

40288

40387

40475

40531

40550

40574

40581

40585

40595

8.6

40345

40437

40519

40570

40587

40609

40614

40616

40624

8.8

40401

40486

40562

40610

40624

40643

40647

40648

40654

9.0

40455

40534

40605

40649

40661

40678

40680

40679

40683

9.2

40509

40582

40648

40688

40697

40713

40712

40710

40713

9.4

40563

40629

40690

40727

40734

40747

40745

40741

40742

9.6

40615

40676

40733

40766

40770

40781

40778

40772

40772

9.8

40668

40723

40775

40804

40807

40816

40810

40803

40801

10.0

40720

40770

40817

40843

40843

40850

40843

40834

40830

10.2

40773

40817

40858

40881

40879

40884

40875

40864

40859

10.4

40825

40864

40900

40919

40915

40918

40907

40895

40889

10.6

40878

40911

40942

40958

40951

40952

40939

40926

40918

10.8

40931

40958

40984

40996

40987

40985

40971

40956

40947

11.0

40984

41005

41025

41034

41023

41019

41003

40986

40975

08.01.368

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

37044

37776

38431

38820

39037

39215

39363

39476

39577

3.2

37169

37877

38510

38887

39096

39267

39410

39519

39616

3.4

37294

37978

38590

38953

39154

39319

39457

39562

39655

3.6

37420

38080

38670

39020

39213

39372

39504

39605

39694

3.8

37546

38181

38750

39086

39272

39424

39552

39648

39733

4.0

37673

38284

38831

39154

39332

39477

39599

39691

39773

4.2

37801

38387

38912

39222

39391

39531

39647

39735

39812

4.4

37931

38492

38994

39290

39451

39584

39695

39778

39852

4.6

38061

38597

39077

39359

39512

39638

39743

39822

39892

4.8

38193

38703

39161

39428

39573

39693

39792

39866

39932

5.0

38325

38810

39244

39498

39635

39747

39841

39911

39973

5.2

38457

38917

39328

39568

39696

39802

39890

39955

40013

5.4

38589

39023

39412

39637

39757

39856

39939

39999

40053

5.6

38719

39128

39494

39706

39818

39910

39987

40043

40093

5.8

38847

39232

39576

39774

39877

39964

40035

40087

40133

6.0

38972

39333

39655

39840

39936

40016

40082

40129

40172

6.2

39094

39432

39733

39905

39993

40067

40128

40171

40210

6.4

39212

39527

39808

39968

40049

40117

40173

40212

40248

6.6

39325

39619

39881

40028

40103

40166

40217

40253

40284

6.8

39433

39706

39950

40086

40154

40212

40259

40291

40320

7.0

39535

39789

40016

40142

40204

40257

40300

40329

40355

Original

07-14-08

08.01.369

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE = 1.50 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

39632

39868

40079

40195

40252

40301

40340

40366

40389

7.4

39726

39944

40139

40246

40298

40343

40378

40402

40423

7.6

39813

40016

40197

40296

40343

40383

40416

40437

40455

7.8

39896

40085

40252

40343

40386

40423

40452

40471

40487

8.0

39975

40150

40306

40389

40428

40462

40488

40505

40519

8.2

40051

40213

40357

40434

40469

40499

40523

40538

40550

8.4

40123

40273

40407

40478

40509

40537

40558

40570

40581

8.6

40191

40331

40455

40520

40548

40573

40592

40602

40611

8.8

40256

40386

40502

40562

40587

40609

40626

40634

40641

9.0

40318

40440

40548

40603

40625

40645

40659

40666

40671

9.2

40378

40491

40592

40643

40662

40680

40693

40698

40701

9.4

40436

40542

40636

40683

40700

40715

40726

40729

40731

9.6

40494

40592

40680

40723

40737

40750

40759

40761

40761

9.8

40550

40642

40723

40762

40774

40785

40792

40792

40791

10.0

40607

40691

40767

40802

40811

40820

40825

40823

40820

10.2

40664

40741

40810

40841

40848

40855

40858

40854

40850

10.4

40721

40792

40854

40881

40885

40890

40891

40886

40880

10.6

40781

40843

40899

40921

40923

40925

40924

40917

40910

10.8

40842

40896

40944

40962

40961

40961

40958

40949

40940

11.0

40904

40950

40990

41003

40999

40996

40991

40981

40970

08.01.370

07-14-08

Original

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES

FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

3.0

36343

37268

38136

38590

38859

39071

39249

39379

39492

3.2

36488

37384

38224

38663

38923

39128

39299

39425

39534

3.4

36634

37500

38312

38736

38987

39184

39350

39470

39575

3.6

36780

37616

38400

38809

39051

39241

39400

39516

39617

3.8

36927

37733

38489

38883

39116

39298

39451

39562

39658

4.0

37075

37850

38578

38957

39181

39356

39502

39608

39700

4.2

37224

37969

38668

39032

39246

39413

39553

39655

39742

4.4

37373

38088

38759

39107

39312

39471

39605

39701

39784

4.6

37525

38208

38850

39183

39378

39530

39657

39748

39827

4.8

37677

38329

38942

39259

39445

39589

39709

39795

39870

5.0

37830

38451

39035

39336

39512

39648

39762

39843

39912

5.2

37983

38573

39127

39413

39579

39707

39814

39890

39955

5.4

38136

38694

39220

39489

39646

39766

39866

39937

39998

5.6

38287

38814

39311

39565

39712

39825

39918

39984

40040

5.8

38436

38933

39401

39640

39778

39882

39970

40030

40083

6.0

38582

39049

39489

39713

39842

39939

40020

40076

40124

6.2

38724

39162

39575

39785

39905

39995

40070

40121

40165

6.4

38863

39273

39659

39854

39966

40049

40118

40165

40205

6.6

38996

39379

39740

39922

40025

40102

40165

40208

40244

6.8

39124

39481

39818

39987

40082

40153

40211

40249

40282

7.0

39246

39579

39892

40049

40137

40202

40255

40290

40320

Original

07-14-08

08.01.371

AIR TRANSPORT INTERNATIONAL B767 FUELING MANUAL 08 - FUEL MEASURING STICK TABLES FUEL MEASURING STICK NUMBER EIGHT (WSTA 920.2) PITCH ATTITUDE = 2.00 DEGREES (POSITIVE IS NOSE HIGH) USABLE FUEL IN POUNDS BASED ON FUEL DENSITY OF 6.7 LB.S/GAL.

STICK LEVEL IN INCHS

ROLL ATTITUDE IN DEGREES (POSITIVE IS WING HIGH) -2.00

-1.50

-1.00

-.50

0.00

.50

1.00

1.50

2.00

7.2

39363

39672

39963

40108

40190

40249

40298

40329

40356

7.4

39475

39762

40032

40166

40241

40295

40339

40367

40391

7.6

39580

39847

40097

40221

40290

40339

40379

40405

40426

7.8

39681

39928

40160

40274

40338

40382

40419

40441

40460

8.0

39776

40005

40220

40326

40384

40424

40457

40477

40493

8.2

39866

40078

40278

40375

40428

40465

40494

40512

40526

8.4

39951

40148

40333

40423

40471

40504

40531

40546

40558

8.6

40030

40214

40386

40469

40513

40543

40567

40580

40590

8.8

40105

40276

40436

40513

40554

40581

40602

40613

40621

9.0

40175

40335

40485

40557

40594

40618

40637

40646

40652

9.2

40241

40392

40533

40599

40633

40655

40671

40679

40683

9.4

40305

40447

40580

40641

40672

40691

40705

40711

40714

9.6

40368

40500

40625

40683

40711

40727

40739

40743

40744

9.8

40429

40554

40671

40724

40749

40763

40773

40775

40775

10.0

40490

40607

40716

40765

40787

40799

40807

40808

40806

10.2

40553

40660

40762

40807

40826

40835

40841

40840

40836

10.4

40616

40715

40809

40849

40865

40872

40876

40872

40867

10.6

40683

40772

40857

40891

40905

40909

40910

40905

40898

10.8

40752

40831

40906

40935

40945

40947

40946

40938

40930

11.0

40823

40892

40956

40980

40986

40984

40981

40972

40961

08.01.372

07-14-08

Original