Booklet N219 Rev Jan 2018.pdf

PT DIRGANTARA INDONESIA (PERSERO) BUSINESS DEVELOPMENT & MARKETING DIVISION JL Pajajaran No. 154 Bandung, 40174, Indonesia Email : [email protected] Website : www.indonesian-aerospace.com

Product Profile N219 January, 2018 Rev. E

FLIGHT DECK & AVIONIC SYSTEM

THE ADVANTAGES OF N219

N219 is equipped with modern new glass cockpit Garmin 1000 Avionics which also enhances flight safety and reduces crew work load. The digital cockpit instruments feature fully integrated avionics suite. With three large displays (two primary flight displays, and one multifunction display including engine indication) the crew have all key flight data at their fingertips at all times. The autopilot system can be provided as optionally.

LOW DIRECT OPERATING COST for more profitability

THE FASTEST AIRCRAFT IN ITS CLASS for faster flight trip SHORT TAKE-OFF AND LANDING for pioneering airstrip operation

PRATT & WHITNEY PT6 ENGINE widely operated, efficient, proven and reliable

WIDE CARGO DOOR for multi role capability

ADVANCED AVIONICS SUITE for better situational awareness

WIDEST CABIN IN ITS CLASS for passenger comfort

COMPETITIVE ACQUISITION PRICE for more profitability

QUICK CHANGE CONFIGURATION for multi mission flexibility

16

1

MEDICAL EVACUATION & TROOP TRANSPORT

N219 PRODUCT FEATURES

N219 is suitable to general military transportation duties of for troop transport and paratrooping or military cargo transport, with room for up to 2.7 tons of cargo or to accommodate 24 troops.

PRODUCT FEATURES • Certification basis CASR 23, commuter category • Twin engines with 850 SHP each

Troop Seats Stretchers

• Fixed landing gear • High wing configuration

N219 can also be configured for medical evacuation applications, then offering room for up to 9 stretchers and foldable paramedic seats.

• Unpressurized cabin

N219 IS A NEW GENERATION OF STOL AIRCRAFT TO A C C O M M O D AT E 1 9 PA S S E N G E R S , DESIGNED TO COMPLY WITH CASR 23 COMMUTER CATEGORY.

• Advanced and modern avionics suite • Short Take-Off and Landing (STOL) operation • Take-off and landing on unpaved runway capabilities • Hot and high airfield capability • Multi hop capability and quick change configuration

Accommodate 24 troops 2 15

CARGO TRANSPORT

DIMENSIONS

Cargo Transport

16.74 m

1,450 mm

6.18 m

N219 is equipped with wide cargo door to enable for carrying D2 containers

0.7 m

1,500 mm

7.5 m

19.50 m

5.08 m

Cargo Transport ● 3 (three) D2 containers, size : 1,473 mm x 1,066.8 mm x 1,143 mm ● 3 (three) pallets size : 1,534 mm x 1,346 mm

14

3.6 m

3

WEIGHTS & PERFORMANCE

Weights Max. Take-Off Weight (MTOW)

7,030 kg

Max. Landing Weight (MLW)

6,940 kg

Max. Zero Fuel Weight (MZFW) Max. Payload

6,622 kg 2,313 kg

Max. Fuel Capacity

1,600 kg

Performance Maximum Cruise Speed

210 kts

Economical Cruise Speed

170 kts

Stall Speed (Landing, SL, MLW) Rate of Climb (AEO) at MTOW, ISA Range with Max. Useable Fuel Range with 19 pax. Operating Altitude Ceiling Altitude

PASSENGER TRANSPORT Commercial Transport • Basic configuration, 19 pax, 32” pitch • Lavatory

59 kts 1,960 ft/min 828 nm

Business Transport

480 nm 10,000 ft 24,000 ft

Airline Seats 4

Simple - Foldable Seats 13

CABIN ARRANGEMENT

TAKE OFF & LANDING PERFORMANCE TAKE-OFF Condition Take-Off Ground Distance Take-Off Distance

: MTOW, ISA, SL, 35 ft obstacle : 375 m (1,230 ft) : 435 m (1,427 ft)

1,705 mm

35 ft obstacle

50 ft obstacle

192 m

375 m 435 m

509 m

19 Pax 30”seat pitch 6.65 m

1,580 mm 12

1,805 mm

Front Baggage Compartment (0.8 m3 – 130 kg)

LANDING Rear Baggage Compartment (2.95 m3 – 475 kg)

Condition Landing Ground Roll Landing Distance

: MLW, ISA, SL, 50 ft obstacle : 192 m ( 629 ft) : 509 m (1,670 ft) 5

POWER PLANT Engines 2 (Two) PT6A-42 (850 shp) turboprop engines Mechanical Horsepower Rating: 850 horsepower @2000 rpm, 41.1° C Torque Limit: 2,750 lb.ft (transient) Power/weight: 2.1 shp/lb Specific Fuel Consumption: 0.69 lb/shp/hr Weight : 350 lbs.

Propeller Hartzell 4-Blade Metal Propeller Constant Speed with Reverse Mode Single Acting Prop Blades electrically de-iced (optional) Diameter 2.361 m (93 inches; 7.7 ft) Max NP = 2000 rpm

MISSION FLEXIBILITY

Passenger transport Business transport Cargo transport Troop transport Medical Evacuation Surveillance & Patrolling Amphibious

6

11

LANDING GEARS

PAYLOAD RANGE

Airplane is equipped with tricycle fixed landing gear configuration capable of unprepared runway operations.

2,750 2,500

Max. Payload

MCR : Max. Cruise Power

2,250

LRC : Long Range Cruise (Economical Cruise)

2,000

Payload - Kg

1,750

1,724 Kg

19 Passengers

1,144 Kg

Max. Range

1,500 1,250 1,000 750

Nose and Main Landing Gears

500 250 145 NM

828 NM

690 NM

480 NM

0 0

100

200

300

400

Range - NM

10

500

600

700

800

900

The nose landing gear is a telescopic forward inclination type with an integral oleo-pneumatic shock absorber and equipped with single wheel. It is incorporated with a mechanical steering system and shimmy damper device. The main landing gear is lever suspension type with a rubber block shock absorber and equipped with single wheel. 7

RANGE CAPABILITY

RANGE CAPABILITY 480 nm range, 19 pax, Altitude 10,000 ft, holding 45 minutes

Kuala lumpur

Bangkok 480 nm

480 nm

Malaysia

Manila

480 nm

Thailand

Phillipines

INDONESIA

8

One way coverage at 19 pax --- 2-ways coverage at 19 pax

9