A320-Engine Failure in Cruise(No Damage)

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 ASAP…Short term decision

CONSIDER AUTOMATION USE  THRUST LEVERS……………………… LEVERS………………………….MCT ….MCT A/THR………………………………………..OFF

ECAM ACTIO ACTIONS  NS  ECAM PROCEDURE  STOP ECAM ECAM actions actions when :

And

Or 

Deceleration Not below Green Dot

PF COMMUNICATES

PF

PNF 2. STANDARD STRATEGY

For desce descent nt : 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 

QRH

MCT

Check LRC CEILING 4.00

REC MAX = EO LRC Ceiling 

EO



EO CLR Prompt 

PF

PNF 3. ENGINE RELIGHT

ORDER…………….………..…..…”CONTINUE ECAM”

ECAM ACTIONS……………………..……CO ACTIONS……………………..……CONTINUE NTINUE

ECAM ACTIO ACTIONS  NS  ECAM PROCEDURE 

QRH

, RELIGHT 

DAMAGE  ?   ? 

SYSTEM DISPLAY  STATUS 

RETURN TO NORMAL TASK SHARING  STATUS,or  SUMMARY

DECISION  Consider

APU Start

FCOM

DIST

WEATHER WEATHER L LDG D G D IST IDIST ST O PERATIONAL AND OPERATIONAL AND COMMERCIAL CONSIDERATIONS CONSIDERATIONS

ATC

& FUEL computations to Landing

APU normal flight envelope : 3.01.49

FCOM

+

3.06.30 QRH

••••

4.00

DECISION DECISION

PURSER /PAX /P AX

NOTIFY NO NOTIFY TIFY

OPS …

2.00

PF

PNF 4. STANDARD STRATEGY

Reaching Reac hing LRC ceiling  LR SPEED………………………………………….SET A/THR…………………………….………………….ON

Descent to landing  RESUME MANAGED MODES

LR SPEED  At LRC ceiling ...

T/D



QRH

4.00

LONG  RANGE  CRUISE 

A/THR

Thrust IDLE

PF

PNF 1. ENG 1 FAIL

DETECTION  FLIES THE AIRCRAFT NAVIGATES

LAND ASAP…Short ASAP…Short term decision

CONSIDER AUTOMATION USE  THRUST LEVERS……………………… LEVERS………………………….MCT ….MCT A/THR………………………………………..OFF

A/THR A/THR is is set set to to OFF OFF immediately immediately to to avoid avoid thrust reduction to IDLE thrust reduction to IDLE

ECAM ACTIO ACTIONS  NS  ECAM PROCEDURE  STOP ECAM ECAM actions actions when :

And

Or 

Deceleration Not below Green Dot

PF COMMUNICATES

PF

PNF

STRATEGY 2. STANDARD STRATEGY

For desce descent nt : 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 

QRH

MCT

Check LRC CEILING 4.00

REC MAX = EO LRC Ceiling 

FIXED SPEED

EO

ETOPS constraint



 As established  before dispatch, use: M.82 / 330 KT  Or  M.82 / 310 KT 

EO CLR Prompt 

PF PNF LRC AND GREEN DOT GROSS CEILING QUICK CHECK 2. STANDARD STRATEGY QRH

For desce descent nt : M.78/300 KT………………………..SET AND PULL

4.00

LRC CEILING ALT……..………….SET AND PULL

During descent to LR ceiling ...



Thrust MCT 

Speed controlled by the elevator  Green Green Dot Dot Gross Gross Ceiling Ceiling

QRH

MCT

Check LRC LRC CEILING LRC Ceiling Ceiling

4.00  

REC MAX = EO LRC Ceiling 

EO

GW at ENG FAIL FAIL

External Temperature 

EO CLR Prompt 

PF

PNF 2. STANDARD STRATEGY

For desce descent nt : 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 

QRH

MCT

Check LRC CEILING 4.00

REC MAX = EO LRC Ceiling 

EO



EO CLR Prompt 

! if pressed, predictions revert  to dual engine predictions

PF

PNF

DAMAGE OR NO DAMAGE ? 3. ENGINE RELIGHT

ORDER…………….………..…..…”CONTINUE ECAM”

ECAM ACTIONS……………………..……CO ACTIONS……………………..……CONTINUE NTINUE

ACTIONS  ACTIO NS  CONSIDERECAM ENGINE DAMAGE DAMAG E 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 SHARING  Page (such as N1 or N2 ~ 0) RETURN TO NORMAL STATUS,or  SUMMARY

DECISION 

L LDG D G D IST IDIST ST

ATC

No attempt of RELIGHT



Consider

APU Start

FCOM

DIST

WEATHER WEATHER

O PERATIONAL AND OPERATIONAL AND COMMERCIAL CONSIDERATIONS CONSIDERATIONS

& FUEL computations to Landing

APU normal flight envelope : 3.01.49

FCOM

+

3.06.30 QRH

••••

4.00

DECISION DECISION

PURSER /PAX /P AX

NOTIFY NO NOTIFY TIFY

OPS …

2.00

PF

PNF

PERFORMANCE CHECK 3. ENGINE RELIGHT QRH

FCOM

ORDER…………….………..…..…”CONTINUE ECAM” 1 2 3.06.30 Descent to LR CRZ ceiling computations

ECAM ACTIONS……………………..……CO ACTIONS……………………..……CONTINUE NTINUE 4.00

Descent from LR CRZ ECAM ACTIONS  ACTIO NS  ceiling to landing computations ECAM PROCEDURE 

QRH

, RELIGHT 

DAMAGE  ?   ? 

SYSTEM DISPLAY  Δ

Dist

Δ

Fuel

Δ

Time

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

STATUS,or  SUMMARY

DECISION  FCOM

FUEL computations to DIST & LRC ceiling

WEATHER WEATHER L LDG D G D IST IDIST ST O PERATIONAL AND OPERATIONAL AND COMMERCIAL CONSIDERATIONS CONSIDERATIONS

ATC

Landing

APU normal flight envelope : 3.01.49

FCOM

+ ••••

3.06.30 QRH

Diversion4.00 Airport

DECISION DECISION

PURSER /PAX /P AX

NOTIFY NO NOTIFY TIFY

OPS …

2.00

PF

PNF

PERFORMANCE CHECK

3. ENGINE RELIGHT Descent to LR CRZ QRH FCOM computations ORDER…………….………..…..…”CONTINUE ECAM” ECAM ACTIONS……………………..……CO ACTIONS……………………..……CONTINUE NTINUE 4.00 1 2 3.06.30

Descent to LR CRZ ceiling computations

Descent from LR CRZ ECAM ACTIONS  ACTIO NS  ceiling to landing

QRH

FCOM

computations ECAM PROCEDURE 

, RELIGHT 

DAMAGE  ?   ? 

GW at ENG FAIL

SYSTEM DISPLAY 

Δ

Dist

Δ

Fuel

Δ Time CRZ FL at Failure

3.06.30 Remaining distance to diversion airport

STATUS  Fuel used in LRC FL Down to Landing Time in LRC FL Down to Landing Δ Dist Δ Dist

RETURN TO NORMAL TASK SHARING  Δ Fuel

Fuel Δ Time Δ Time Δ

Initial FL

Consider

APU Start

LRC Ceiling

FCOM

DECISION 

FUEL computations to DIST & LRC ceiling

STATUS,or  SUMMARY

WEATHER WEATHER L LDG D G D IST IDIST ST O PERATIONAL AND OPERATIONAL AND COMMERCIAL CONSIDERATIONS CONSIDERATIONS

ATC

Landing

APU normal flight envelope : 3.01.49

FCOM

+ ••••

3.06.30 QRH

Diversion4.00 Airport

DECISION DECISION

PURSER /PAX /P AX

NOTIFY NO NOTIFY TIFY

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

Remaining distance

Descent to LR CRZ ceiling computations

ECAM ACTIONS……………………..……CO ACTIONS……………………..……CONTINUE NTINUE 4.00

Descent from LR CRZ ECAM ACTIONS  ACTIO NS  ceiling to landing computations ECAM PROCEDURE 

QRH

, RELIGHT 

DAMAGE  ?   ? 

LR CRZ Ceiling

SYSTEM DISPLAY 

Diversion Airport

Δ

Dist

Δ

Fuel

Δ

Time

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  Fuel Fuel used used in in LRC LRC FL, FL, down down to to Landing Landing based based on on ref ref weight weight

+ DECISION 

Initial FL

Consider

APU Start

FCOM

Correction Correction according according to to  compared Δ  compared Δ to to reference reference weight weight

=

Fuel Fuel used used in in LRC LRC FL FL Down to Landing Down to Landing STATUS,or  SUMMARY

L LDG D G D IST IDIST ST

ATC

Time Time in in LRC LRC FL FL down to landing down to landing & FUEL computations to Landing DIST LRC ceiling

APU normal flight envelope : 3.01.49

FCOM

+ ••••

WEATHER WEATHER

O PERATIONAL AND OPERATIONAL AND COMMERCIAL CONSIDERATIONS CONSIDERATIONS

3.06.30 QRH

Diversion4.00 Airport

DECISION DECISION

PURSER /PAX /P AX

NOTIFY NO NOTIFY TIFY

OPS …

2.00