A320-engine Failure (no Damage)
This document was uploaded by user and they confirmed that they have the permission to share it. If you are author or own the copyright of this book, please report to us by using this DMCA report form. Report DMCA
Overview
Download & View A320-engine Failure (no Damage) as PDF for free.
More details
- Words: 1,150
- Pages: 13
PF FAILURE IN CRUISE PNF ENGINE
(WITH NO DAMAGE)
Detection
ENGINE FAILURE !
ECAM actions
SITUATION ASSESSMENT STRATEGY DECISIONS
SD analysis
STATUS
STANDARD
OBSTACLE
FIXED SPEED
A320 - Version 03
PF
PNF 1. ENG 1 FAIL
DETECTION FLIES THE AIRCRAFT NAVIGATES LAND ASAP…Short term decision CONSIDER AUTOMATION USE THRUST LEVERS………………………….MCT A/THR………………………………………..OFF
ECAM ACTIONS ECAM PROCEDURE STOP ECAM actions when :
And
Or
Deceleration Not below Green Dot
PF COMMUNICATES
PF
PNF 2. STANDARD STRATEGY
For descent : M.78/300 KT………………………..SET AND PULL LRC CEILING ALT……..………….SET AND PULL
During descent to LR ceiling ...
Thrust MCT Speed controlled by the elevator
MCT
QRH
Check LRC CEILING 4.00
REC MAX = EO LRC Ceiling
EO
EO CLR Prompt
PF
PNF 3. ENGINE RELIGHT
ORDER…………….………..…..…”CONTINUE ECAM”
ECAM ACTIONS……………………..……CONTINUE
ECAM ACTIONS ECAM PROCEDURE
QRH
, RELIGHT
DAMAGE ?
SYSTEM DISPLAY STATUS RETURN TO NORMAL TASK SHARING
DECISION Consider APU Start
FCOM
ST AT US, or SUMM ARY
LDG LDGDIS DIST T
CONS CONSIDERATIONS IDERATIONS
ATC
DIST & FUEL computations to Landing
APU normal flight envelope : 3.01.49
FCOM
+ ••••
••••
•••
WEATHER WE ATHER
OPERATIONAL AND OPERATIONAL AND COMMERCIAL COMME RCIAL
••••
••••
3.06.30 QRH 4.00
DECISION DECISIO N
PURSER / PAX
NOT IFY
OPS …
2.00
PF
PNF 4. STANDARD STRATEGY
Reaching LRC ceiling LR SPEED………………………………………….SET A/THR…………………………….………………….ON
Descent to landing RESUME MANAGED MODES
LR SPEED At LRC ceiling ...
T/D
Thrust IDLE QRH 4.00
LONG RANGE CRUISE
A/THR
PF
PNF 1. ENG 1 FAIL
DETECTION FLIES THE AIRCRAFT NAVIGATES LAND ASAP…Short term decision CONSIDER AUTOMATION USE THRUST LEVERS………………………….MCT A/THR………………………………………..OFF
A/THR A/THR is is set set to to OFF OFF immediately immediately to to avoid avoid thrust thrust reduction reduction to to IDLE IDLE
ECAM ACTIONS ECAM PROCEDURE STOP ECAM actions when :
And
Or
Deceleration Not below Green Dot
PF COMMUNICATES
PF
PNF
STRATEGY 2. STANDARD STRATEGY
For descent : M.78/300 KT………………………..SET AND PULL STANDARD LRC CEILING ALT……..………….SET AND PULL
No obstacle and time constraint
During descent to LR ceiling ...
OBSTACLE Thrust MCT
To ensure the margins over obstacles Speed controlled by the elevator
MCT
QRH
Check LRC CEILING 4.00
REC MAX = EO LRC Ceiling
FIXED SPEED
EO
ETOPS constraint
EO CLR Prompt As established before dispatch, use: M.82 / 330 KT Or M.82 / 310 KT
PF PNF LRC AND GREEN DOT GROSS CEILING QUICK CHECK 2. STANDARD STRATEGY QRH For descent : M.78/300 KT………………………..SET AND PULL
4.00
LRC CEILING ALT……..………….SET AND PULL
During descent to LR ceiling ...
Thrust MCT
MCT
Speed controlled by the elevator Green Green Dot Dot Gross Gross Ceiling Ceiling QRH Check LRC LRC CEILING LRC Ceiling Ceiling
4.00
REC MAX = EO LRC Ceiling
EO
GW at ENG FAIL
External Temperature
EO CLR Prompt
PF
PNF 2. STANDARD STRATEGY
For descent : M.78/300 KT………………………..SET AND PULL LRC CEILING ALT……..………….SET AND PULL
During descent to LR ceiling ...
Thrust MCT Speed controlled by the elevator
MCT
QRH
Check LRC CEILING 4.00
REC MAX = EO LRC Ceiling
EO
EO CLR Prompt
! if pressed, predictions revert to dual engine predictions
PF
DAMAGE OR NO DAMAGE ?
PNF
3. ENGINE RELIGHT ORDER…………….………..…..…”CONTINUE ECAM”
ECAM ACTIONS……………………..……CONTINUE
ACTIONS CONSIDERECAM ENGINE DAMAGE IF YOU NOTICE : ECAM PROCEDURE DAMAGE ?
QRH
, RELIGHT
SYSTEM DISPLAY
High vibration prior to engine stopped, loud noise
STATUS
Stall Any Abnormal Indication onTASK ENG Page (such as N1 or N2 ~ 0) RETURN TO NORMAL SHARING
DECISION
ST AT US, or SUMM ARY
LDG LDGDIS DIST T
CONS CONSIDERATIONS IDERATIONS
ATC
No attempt of RELIGHT Consider APU Start
FCOM
DIST & FUEL computations to Landing
APU normal flight envelope : 3.01.49
FCOM
+ ••••
••••
•••
WEATHER WE ATHER
OPERATIONAL AND OPERATIONAL AND COMMERCIAL COMME RCIAL
••••
••••
3.06.30 QRH 4.00
DECISION DECISIO N
PURSER / PAX
NOT IFY
OPS …
2.00
PF
PNF
PERFORMANCE CHECK 3. ENGINE RELIGHT QRH
FCOM
ORDER…………….………..…..…”CONTINUE ECAM” 1 2 3.06.30
ECAM ACTIONS……………………..……CONTINUE 4.00
ECAM ACTIONS
Descent to LR CRZ Descent from LR CRZ ceiling ceiling to landing computations computations ECAM PROCEDURE
QRH
, RELIGHT
DAMAGE ?
SYSTEM DISPLAY ΔDist ΔFuel ΔTime
Remaining distance to diversion airport STATUS Fuel used in LRC FL Down to Landing Time in LRC FL Down to Landing
RETURN TO NORMAL TASK SHARING Initial FL
Consider APU Start
DECISION FCOM
ST AT US, or SUMM ARY
LDG LDGDIS DIST T
CONS CONSIDERATIONS IDERATIONS
ATC
DIST & FUEL computations to Landing LRC ceiling
APU normal flight envelope : 3.01.49
FCOM
+ ••••
••••
•••
WEATHER WE ATHER
OPERATIONAL AND OPERATIONAL AND COMMERCIAL COMME RCIAL
••••
••••
3.06.30 QRH
Diversion4.00 Airport
DECISION DECISIO N
PURSER / PAX
NOT IFY
OPS …
2.00
PF
PNF
PERFORMANCE CHECK
3. ENGINE RELIGHT Descent to LR CRZ QRH FCOM computations ORDER…………….………..…..…”CONTINUE ECAM” ECAM ACTIONS……………………..……CONTINUE 4.00 1 2 3.06.30
ECAM ACTIONS
Descent to LR CRZ Descent from LR CRZ ceiling ceiling to landing computations computations ECAM PROCEDURE
QRH
FCOM
, RELIGHT
DAMAGE ?
GW at ENG FAIL
SYSTEM DISPLAY
ΔDist ΔFuel ΔTime CRZ FL at
3.06.30 airport Remaining distance to diversion STATUS Fuel used in LRC FL Down to Landing Time in LRC FL Down to Landing ΔDist ΔDist ΔFuel ΔTime ΔTime
Failure
RETURN TO NORMAL TASK SHARING ΔFuel
Initial FL
Consider APU Start
LRC Ceiling
FCOM
DECISION
ST AT US, or SUMM ARY
LDG LDGDIS DIST T
CONS CONSIDERATIONS IDERATIONS
ATC
DIST & FUEL computations to Landing LRC ceiling
APU normal flight envelope : 3.01.49
FCOM
+ ••••
••••
•••
WEATHER WE ATHER
OPERATIONAL AND OPERATIONAL AND COMMERCIAL COMME RCIAL
••••
••••
3.06.30 QRH
Diversion4.00 Airport
DECISION DECISIO N
PURSER / PAX
NOT IFY
OPS …
2.00
PF
PNF
PERFORMANCE CHECK 3. ENGINE RELIGHT
QRH
QRH LR Cruise to Landing computations
FCOM
ORDER…………….………..…..…”CONTINUE ECAM” 14.00 3.06.30 2
ECAM ACTIONS……………………..……CONTINUE 4.00
ECAM ACTIONS
Remaining distance
Descent to LR CRZ Descent from LR CRZ ceiling ceiling to landing computations computations ECAM PROCEDURE LR CRZ Ceiling
QRH
, RELIGHT
DAMAGE ?
SYSTEM DISPLAY
Diversion Airport
ΔDist ΔFuel ΔTime
RETURN TO NORMAL TASK SHARING Fuel Fuel used used in in LRC LRC FL, FL, down down to to Landing Landing based based on on ref ref weight weight
Correction Correction according according to to Δcompared Δcompared to to reference reference Time Time in in LRC LRC FL FL weight weight down to down DIST to landing landing & FUEL computations to Landing LRC ceiling
+ DECISION
Initial FL
Consider APU Start
Remaining distance to diversion airport STATUS Fuel used in LRC FL Down to Landing Time in LRC FL Down to Landing
FCOM
=
Fuel Fuel used used in in LRC LRC FL FL Down Down to toLanding Landing ST AT US, or SUMM ARY
LDG LDGDIS DIST T
CONS CONSIDERATIONS IDERATIONS
ATC
APU normal flight envelope : 3.01.49
FCOM
+ ••••
••••
•••
••••
••••
WEATHER WE ATHER
OPERATIONAL AND OPERATIONAL AND COMMERCIAL COMME RCIAL
3.06.30 QRH
Diversion4.00 Airport
DECISION DECISIO N
PURSER / PAX
NOT IFY
OPS …
2.00
(WITH NO DAMAGE)
Detection
ENGINE FAILURE !
ECAM actions
SITUATION ASSESSMENT STRATEGY DECISIONS
SD analysis
STATUS
STANDARD
OBSTACLE
FIXED SPEED
A320 - Version 03
PF
PNF 1. ENG 1 FAIL
DETECTION FLIES THE AIRCRAFT NAVIGATES LAND ASAP…Short term decision CONSIDER AUTOMATION USE THRUST LEVERS………………………….MCT A/THR………………………………………..OFF
ECAM ACTIONS ECAM PROCEDURE STOP ECAM actions when :
And
Or
Deceleration Not below Green Dot
PF COMMUNICATES
PF
PNF 2. STANDARD STRATEGY
For descent : M.78/300 KT………………………..SET AND PULL LRC CEILING ALT……..………….SET AND PULL
During descent to LR ceiling ...
Thrust MCT Speed controlled by the elevator
MCT
QRH
Check LRC CEILING 4.00
REC MAX = EO LRC Ceiling
EO
EO CLR Prompt
PF
PNF 3. ENGINE RELIGHT
ORDER…………….………..…..…”CONTINUE ECAM”
ECAM ACTIONS……………………..……CONTINUE
ECAM ACTIONS ECAM PROCEDURE
QRH
, RELIGHT
DAMAGE ?
SYSTEM DISPLAY STATUS RETURN TO NORMAL TASK SHARING
DECISION Consider APU Start
FCOM
ST AT US, or SUMM ARY
LDG LDGDIS DIST T
CONS CONSIDERATIONS IDERATIONS
ATC
DIST & FUEL computations to Landing
APU normal flight envelope : 3.01.49
FCOM
+ ••••
••••
•••
WEATHER WE ATHER
OPERATIONAL AND OPERATIONAL AND COMMERCIAL COMME RCIAL
••••
••••
3.06.30 QRH 4.00
DECISION DECISIO N
PURSER / PAX
NOT IFY
OPS …
2.00
PF
PNF 4. STANDARD STRATEGY
Reaching LRC ceiling LR SPEED………………………………………….SET A/THR…………………………….………………….ON
Descent to landing RESUME MANAGED MODES
LR SPEED At LRC ceiling ...
T/D
Thrust IDLE QRH 4.00
LONG RANGE CRUISE
A/THR
PF
PNF 1. ENG 1 FAIL
DETECTION FLIES THE AIRCRAFT NAVIGATES LAND ASAP…Short term decision CONSIDER AUTOMATION USE THRUST LEVERS………………………….MCT A/THR………………………………………..OFF
A/THR A/THR is is set set to to OFF OFF immediately immediately to to avoid avoid thrust thrust reduction reduction to to IDLE IDLE
ECAM ACTIONS ECAM PROCEDURE STOP ECAM actions when :
And
Or
Deceleration Not below Green Dot
PF COMMUNICATES
PF
PNF
STRATEGY 2. STANDARD STRATEGY
For descent : M.78/300 KT………………………..SET AND PULL STANDARD LRC CEILING ALT……..………….SET AND PULL
No obstacle and time constraint
During descent to LR ceiling ...
OBSTACLE Thrust MCT
To ensure the margins over obstacles Speed controlled by the elevator
MCT
QRH
Check LRC CEILING 4.00
REC MAX = EO LRC Ceiling
FIXED SPEED
EO
ETOPS constraint
EO CLR Prompt As established before dispatch, use: M.82 / 330 KT Or M.82 / 310 KT
PF PNF LRC AND GREEN DOT GROSS CEILING QUICK CHECK 2. STANDARD STRATEGY QRH For descent : M.78/300 KT………………………..SET AND PULL
4.00
LRC CEILING ALT……..………….SET AND PULL
During descent to LR ceiling ...
Thrust MCT
MCT
Speed controlled by the elevator Green Green Dot Dot Gross Gross Ceiling Ceiling QRH Check LRC LRC CEILING LRC Ceiling Ceiling
4.00
REC MAX = EO LRC Ceiling
EO
GW at ENG FAIL
External Temperature
EO CLR Prompt
PF
PNF 2. STANDARD STRATEGY
For descent : M.78/300 KT………………………..SET AND PULL LRC CEILING ALT……..………….SET AND PULL
During descent to LR ceiling ...
Thrust MCT Speed controlled by the elevator
MCT
QRH
Check LRC CEILING 4.00
REC MAX = EO LRC Ceiling
EO
EO CLR Prompt
! if pressed, predictions revert to dual engine predictions
PF
DAMAGE OR NO DAMAGE ?
PNF
3. ENGINE RELIGHT ORDER…………….………..…..…”CONTINUE ECAM”
ECAM ACTIONS……………………..……CONTINUE
ACTIONS CONSIDERECAM ENGINE DAMAGE IF YOU NOTICE : ECAM PROCEDURE DAMAGE ?
QRH
, RELIGHT
SYSTEM DISPLAY
High vibration prior to engine stopped, loud noise
STATUS
Stall Any Abnormal Indication onTASK ENG Page (such as N1 or N2 ~ 0) RETURN TO NORMAL SHARING
DECISION
ST AT US, or SUMM ARY
LDG LDGDIS DIST T
CONS CONSIDERATIONS IDERATIONS
ATC
No attempt of RELIGHT Consider APU Start
FCOM
DIST & FUEL computations to Landing
APU normal flight envelope : 3.01.49
FCOM
+ ••••
••••
•••
WEATHER WE ATHER
OPERATIONAL AND OPERATIONAL AND COMMERCIAL COMME RCIAL
••••
••••
3.06.30 QRH 4.00
DECISION DECISIO N
PURSER / PAX
NOT IFY
OPS …
2.00
PF
PNF
PERFORMANCE CHECK 3. ENGINE RELIGHT QRH
FCOM
ORDER…………….………..…..…”CONTINUE ECAM” 1 2 3.06.30
ECAM ACTIONS……………………..……CONTINUE 4.00
ECAM ACTIONS
Descent to LR CRZ Descent from LR CRZ ceiling ceiling to landing computations computations ECAM PROCEDURE
QRH
, RELIGHT
DAMAGE ?
SYSTEM DISPLAY ΔDist ΔFuel ΔTime
Remaining distance to diversion airport STATUS Fuel used in LRC FL Down to Landing Time in LRC FL Down to Landing
RETURN TO NORMAL TASK SHARING Initial FL
Consider APU Start
DECISION FCOM
ST AT US, or SUMM ARY
LDG LDGDIS DIST T
CONS CONSIDERATIONS IDERATIONS
ATC
DIST & FUEL computations to Landing LRC ceiling
APU normal flight envelope : 3.01.49
FCOM
+ ••••
••••
•••
WEATHER WE ATHER
OPERATIONAL AND OPERATIONAL AND COMMERCIAL COMME RCIAL
••••
••••
3.06.30 QRH
Diversion4.00 Airport
DECISION DECISIO N
PURSER / PAX
NOT IFY
OPS …
2.00
PF
PNF
PERFORMANCE CHECK
3. ENGINE RELIGHT Descent to LR CRZ QRH FCOM computations ORDER…………….………..…..…”CONTINUE ECAM” ECAM ACTIONS……………………..……CONTINUE 4.00 1 2 3.06.30
ECAM ACTIONS
Descent to LR CRZ Descent from LR CRZ ceiling ceiling to landing computations computations ECAM PROCEDURE
QRH
FCOM
, RELIGHT
DAMAGE ?
GW at ENG FAIL
SYSTEM DISPLAY
ΔDist ΔFuel ΔTime CRZ FL at
3.06.30 airport Remaining distance to diversion STATUS Fuel used in LRC FL Down to Landing Time in LRC FL Down to Landing ΔDist ΔDist ΔFuel ΔTime ΔTime
Failure
RETURN TO NORMAL TASK SHARING ΔFuel
Initial FL
Consider APU Start
LRC Ceiling
FCOM
DECISION
ST AT US, or SUMM ARY
LDG LDGDIS DIST T
CONS CONSIDERATIONS IDERATIONS
ATC
DIST & FUEL computations to Landing LRC ceiling
APU normal flight envelope : 3.01.49
FCOM
+ ••••
••••
•••
WEATHER WE ATHER
OPERATIONAL AND OPERATIONAL AND COMMERCIAL COMME RCIAL
••••
••••
3.06.30 QRH
Diversion4.00 Airport
DECISION DECISIO N
PURSER / PAX
NOT IFY
OPS …
2.00
PF
PNF
PERFORMANCE CHECK 3. ENGINE RELIGHT
QRH
QRH LR Cruise to Landing computations
FCOM
ORDER…………….………..…..…”CONTINUE ECAM” 14.00 3.06.30 2
ECAM ACTIONS……………………..……CONTINUE 4.00
ECAM ACTIONS
Remaining distance
Descent to LR CRZ Descent from LR CRZ ceiling ceiling to landing computations computations ECAM PROCEDURE LR CRZ Ceiling
QRH
, RELIGHT
DAMAGE ?
SYSTEM DISPLAY
Diversion Airport
ΔDist ΔFuel ΔTime
RETURN TO NORMAL TASK SHARING Fuel Fuel used used in in LRC LRC FL, FL, down down to to Landing Landing based based on on ref ref weight weight
Correction Correction according according to to Δcompared Δcompared to to reference reference Time Time in in LRC LRC FL FL weight weight down to down DIST to landing landing & FUEL computations to Landing LRC ceiling
+ DECISION
Initial FL
Consider APU Start
Remaining distance to diversion airport STATUS Fuel used in LRC FL Down to Landing Time in LRC FL Down to Landing
FCOM
=
Fuel Fuel used used in in LRC LRC FL FL Down Down to toLanding Landing ST AT US, or SUMM ARY
LDG LDGDIS DIST T
CONS CONSIDERATIONS IDERATIONS
ATC
APU normal flight envelope : 3.01.49
FCOM
+ ••••
••••
•••
••••
••••
WEATHER WE ATHER
OPERATIONAL AND OPERATIONAL AND COMMERCIAL COMME RCIAL
3.06.30 QRH
Diversion4.00 Airport
DECISION DECISIO N
PURSER / PAX
NOT IFY
OPS …
2.00
Related Documents
A320-engine Failure (no Damage)
May 2020 1
A320-engine Failure (damage)
May 2020 4
The Damage, Cause Of Takoma Bridge Failure
June 2020 0
Failure
August 2019 49
Failure
November 2019 31