A320-Engine Failure (Damage)

PF PNF ENGINE FAILURE IN CRUISE

(WITH DAMAGE)

Detection

ENGINE FAILURE !

ECAM actions

SITUATION ASSESSMENT STRATEGY DECISIONS

SD analysis

STATUS

STANDARD

OBSTACLE

FIXED SPEED

 A320- Versio Version n 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. OBSTACLE STRATEGY

For desce descent nt : GREEN DOT……………………….SET AND PULL DRIFT DOWN CEILING ALT…….SET AND PULL

During descent to LR Drift ceiling Down...Ceiling ...



Thrust MCT 

Speed controlled by the elevator 

QRH

MCT

Check GREEN DOT GROSS CEILING 4.00

REC MAX = EO LRC Ceiling 

EO



EO CLR Prompt 

PF

PNF 3. ECAM ACTIONS… DAMAGE

ORDER…………….………..…..…”CONTINUE ECAM”

ECAM ACTIONS……………………..……CONTINUE

ECAM ACTIO ACTIONS  NS  ECAM PROCEDURE 

DAMAGE ?  DAMAGE  ? 

SYSTEM DISPLAY  STATUS 

RETURN TO NORMAL TASK SHARING  STATUS,or  SUMMARY

DECISION  Consider

APU Start

FCOM

DIST

WEATHER WEATHER LDG LDGDIST DIST OPERATIONAL OP ERATIONAL AND OPERATIONAL AND COMMERCIAL CONSIDERATIONS CONSIDERATIONS

ATC

& FUEL computations computations to Landing

APU normal flight envelope : 3.01.49



DECISION DECISION

PURSER /PAX

NOTIFY

OPS …

PF

PNF 4. OBSTACLE STRATEGY

When obstacles obstacles are cleared cleared : LR CEILING………………………..SET AND PULL LR SPEED….……………… SPEED….………………………………… …………………….SET ….SET

Reaching LR Ceiling  A/THR….…………….………………………..…...ON

Descent to landing  RESUME MANAGED MODES

If obstacle : Continue Drift Down Procedure Drift Down Ceiling 

QRH

LR SPEED

LONG RANGE CRUISE

4.00 T/D LRC ceiling  

A/THR

Thrust is 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. OBSTACLE STRATEGY

For desce descent nt : GREEN DOT……………………….SET AND PULLSTANDARD DRIFT DOWN CEILING ALT…….SET AND PULL

No obstacle and time constraint During descent to LR Drift ceiling Down...Ceiling ...

OBSTACLE 

Thrust MCT 

To ensure the margins over obstacles Speed controlled by the elevator 

QRH

MCT

Check GREEN DOT GROSS 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

PERFORMANCE CHECK

PNF

2. OBSTACLE STRATEGY For desce descent nt : GREEN DOT……………………….SET AND PULL LRC and Green Dot Gross Gross Ceiling quick check check DRIFT DOWN CEILING ALT…….SET AND PULL

Green Dot Gross Ceiling Ceiling precise check

During descent to LR Drift ceiling Down...Ceiling ... CRZ FL at fail 

Thrust MCT 

Green Green Dot Dot Gross Gross MCT Ceiling Ceiling

Speed controlled by the elevator 

GW at QRH ENG FAIL

Check GREEN DOT GROSS CEILING

4.00

LRC LRC Ceiling Ceiling

REC MAX = EO LRC Ceiling  External Temperature

EO

GW at ENG FAIL

DIST TIME INIT INITIA IAL L SPEE SPEED D FUEL FUEL LEVEL OFF LEVEL OFF LEVEL OFF CLR Prompt   EO

PF

PNF 2. OBSTACLE STRATEGY

For desce descent nt : GREEN DOT……………………….SET AND PULL DRIFT DOWN CEILING ALT…….SET AND PULL

During descent to LR Drift ceiling Down...Ceiling ...



Thrust MCT 

Speed controlled by the elevator 

QRH

MCT

Check GREEN DOT GROSS 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. ECAM ACTIONS… DAMAGE

ORDER…………….………..…..…”CONTINUE ECAM”

ECAM ACTIONS……………………..……CONTINUE

ACTIONS  ACTIO NS  CONSIDERECAM ENGINE DAMAGE IF YOU NOTICE : ECAM PROCEDURE  DAMAGE  DAMAGE ?  ?  SYSTEM DISPLAY  

High vibration vibration prior to engine stopped, stopped, loud noise

STATUS 

 Stall 

Any Abnor Ab normal malTO Indica IndNORMAL icatio tion n onTASK ENG Page Pag e (such as N1 or N2 ~ 0) RETURN SHARING  STATUS,or  SUMMARY

DECISION 

LDG LDGDIST DIST

ATC

No attempt of RELIGHT



Consider

APU Start

FCOM

DIST

WEATHER WEATHER

OPERATIONAL OP ERATIONAL AND OPERATIONAL AND COMMERCIAL CONSIDERATIONS CONSIDERATIONS

& FUEL computations computations to Landing

APU normal flight envelope : 3.01.49



DECISION DECISION

PURSER /PAX

NOTIFY

OPS …