ENG FAILURE AFTER TAKEOFF

ENGINE FAILURE

EO ACC ALT

At EO ACCEL ALT

V1

400 ft mini

EO ACCELERATION ALTITUDE

Green dot-°

Beta target

L/G up

PITCH : 12,5°MCT

-S-F Flaps 1 Flaps 0

CONTINUE ECAM

DECISION

At Green Dot

REV09

LEVEL OFF

PRESS ALT P/B to…

OP CLB

APPROACH PREPARATION

FMGS PREP

APPROACH BRIEFING

ENG FAIL

ENG FAIL

DETECTION

Above 400 ft and established on appropriate flight path :

ECAM ACTIONSECAM PROCEDURE

ECAM actions can be stopped at any time on PF request for trajectory, configuration, etc...

DAMAGE ?

FLY THE AIRCRAFT

CONSIDER AUTOMATION USE

NAVIGATE ⇒ LAND ASAP

PFCOMMUNICATE

400 ft AGLNO ACTION until

NO DAMAGE ?

ANNOUNCE .………………………..……”ENGINE FAILURE”The first who detects :

PF PNF

EO ACC ALT

ALT P/B on FCU………………………………….PRESS

At EO ACC ALT

CLEAN UP THE A/CAt GREEN DOT

1. ALT SELECTOR knob……..…………………..…PULL

2. THR LEVERS……..……………...………..…..…….MCT

THR LEVERS……..….MCT

For T/O in FLEX : FLEX

CLB

MCT

FMA

ORDER…………….………………………..……”STOP ECAM” ECAM ACTIONS………………….…………………....STOP

Before EO ACC ALT

FMA

PF PNF

CONTINUE ECAM

RETURN TO NORMAL TASK SHARING

SITUATION ASSESSMENTDECISION

ECAM ACTIONSECAM PROCEDURE

SYSTEM DISPLAY

STATUS

ORDER…………….………..…..…”CONTINUE ECAM” ECAM ACTIONS……………………..……CONTINUE

PERFAfter a succesful engine relight :

If EO CLR is still displayed, press on the prompt ⇒

Pressing EO CLR prompt restores predictions and performances for ALL ENGINES OPERATIVE. Once pressed : Reverting to ONE ENGINE OUT conditions is not possible.

PF PNF

APPROACH PREPARATION

FMS PREPARATION :

STANDARD

APPR BRIEFING :

STANDARD

+

STATUS

+

CONSIDER OVERWEIGHT LANDING

FMS………………………….…………………PREPARE

APPR BRIEFING .........……….……………PERFORM

ANNOUNCE………………..”YOU HAVE CONTROL ?” ANNOUNCE………………………...”I HAVE CONTROL”

QRH

PF PNF

………………

THE END...

ENG FAIL

DETECTION

Above 400 ft and established on appropriate flight path :

ECAM ACTIONSECAM PROCEDURE

ECAM actions can be stopped at any time on PF request for trajectory, configuration, etc...

DAMAGE ?

FLY THE AIRCRAFT

CONSIDER AUTOMATION USE

NAVIGATE ⇒ LAND ASAP

PFCOMMUNICATE

400 ft AGLNO ACTION until

NO DAMAGE ?

ANNOUNCE .………………………..……”ENGINE FAILURE”The first who detects :

PF PNF

- Gear Up

- Consider TOGA

- Pitch adjust 12.5º

- Beta target Conditions

- Consider A/P

FLY THE AIRCRAFT

ENG FAIL

DETECTION

Above 400 ft and established on appropriate flight path :

ECAM ACTIONSECAM PROCEDURE

ECAM actions can be stopped at any time on PF request for trajectory, configuration, etc...

DAMAGE ?

FLY THE AIRCRAFT

CONSIDER AUTOMATION USE

NAVIGATE ⇒ LAND ASAP

PFCOMMUNICATE

400 ft AGLNO ACTION until

NO DAMAGE ?

ANNOUNCE .………………………..……”ENGINE FAILURE”The first who detects :

PF PNF

In such situation, stabilizing the flight path is number one priority. Performing ECAM actions before stabilization reduces efficiency

due to PF high workload.

ENG FAIL

DETECTION

Above 400 ft and established on appropriate flight path :

ECAM ACTIONSECAM PROCEDURE

ECAM actions can be stopped at any time on PF request for trajectory, configuration, etc...

DAMAGE ?

FLY THE AIRCRAFT

CONSIDER AUTOMATION USE

NAVIGATE ⇒ LAND ASAP

PFCOMMUNICATE

400 ft AGLNO ACTION until

NO DAMAGE ?

ANNOUNCE .………………………..……”ENGINE FAILURE”The first who detects :

PF PNF

If applicable, consider EOSID for TAKEOFF RWY.

NAVIGATE ⇒ LAND ASAP

DETECTION

Above 400 ft and established on appropriate flight path :

ECAM ACTIONSECAM PROCEDURE

ECAM actions can be stopped at any time on PF request for trajectory, configuration, etc...

DAMAGE ?

PFCOMMUNICATE

400 ft AGLNO ACTION until

NO DAMAGE ?

PF PNF

FLY THE AIRCRAFT

CONSIDER AUTOMATION USE

NAVIGATE ⇒ LAND ASAP

NO DAMAGE ?

According to the situation, the crew may decide to attempt an engine relight in flight at

this step, but it is recommended:

- to perform all ECAM actions and

- to consider engine relight when reaching the STATUS page

PF PNFENG FAIL

DETECTION

Above 400 ft and established on appropriate flight path :

ECAM ACTIONSECAM PROCEDURE

ECAM actions can be stopped at any time on PF request for trajectory, configuration, etc...

DAMAGE ?

PFCOMMUNICATE

400 ft AGLNO ACTION until

NO DAMAGE ?

FLY THE AIRCRAFTCONSIDER AUTOMATION USENAVIGATE ⇒ LAND ASAP

DAMAGE ?

CONSIDER ENGINE DAMAGE IF YOU NOTICE :

High vibration prior to flame out

Loud noise, explosion

Repeated and uncontrollable engine stalls

Abnormal engine indications on ECAM (such as N1 or N2 ~ 0)

No attempt of RELIGHT

ALT P/B on FCU………………………………….PRESS

At EO ACC ALT

At GREEN DOT

1. ALT SELECTOR knob……..…………………..…PULL

2. THR LEVERS……..……………...………..…..…….MCT

THR LEVERS……..….MCT

For T/O in FLEX : FLEX

CLB

MCT

FMA

ORDER…………….………………………..……”STOP ECAM” ECAM ACTIONS………………….…………………....STOP

FMA

EO ACC ALT

CLEAN UP THE A/C

You should delay the acceleration for SECURING the engine.

An engine is considered SECURED when:ENG MASTER…OFF for an engine failure without damageAGENT 1…DISH for an engine failure with damageFire extinguished or AGENT 2…DISH for an engine fire.

CAUTION: DO NOT EXCEED THE MAXIMUM EO ACC ALT

MCT

MAX EO ACC ALT:

-S-F Flaps 1 Flaps 0

LEVEL OFF

PRESS ALT P/B to…

OP CLB

400 ft mini

ENGINE FAILURE

V1

Green dot-°

ECAM ACTIONS

CHRONO 10 MINMAX

Refer to LPC NG…

… or RTOW charts

Before EO ACC ALT

PF PNF

PF PNFFLY THE AIRCRAFT

- “Engine failure”

- Reset MASTER CAUTION

- Gear Up

- Consider TOGA

- Pitch adjust 12.5º

- Beta target

- Consider A/P

- “Engine failure”

- Cancel warning

- Gear Up

- Consider TOGA

- Pitch adjust 12.5º

- Beta target

- Consider A/P

Beta target and rudder trim

Beta target

Once centered :Appropriate sideslip

for optimumaircraft performance

Moves at 1 deg/s, and, after 1.5 seconds,

at 3 deg/s

ENG FAIL

DETECTION

Above 400 ft and established on appropriate flight path :

ECAM ACTIONSECAM PROCEDURE

ECAM actions can be stopped at any time on PF request for trajectory, configuration, etc...

DAMAGE ?

FLY THE AIRCRAFT

CONSIDER AUTOMATION USE

NAVIGATE ⇒ LAND ASAP

PFCOMMUNICATE

400 ft AGLNO ACTION until

NO DAMAGE ?

ANNOUNCE .………………………..……”ENGINE FAILURE”The first who detects :

PF PNF

- Gear Up

- Consider TOGA

- Pitch adjust 12.5º

- Beta target Conditions

- Consider A/P

FLY THE AIRCRAFT

T/O thrust (FLEX or TOGA) must be kept until GREEN DOT speed is reached, limited to 10 min

(5 min under FAA rules)

TOGA thrust requires more rudder input

Setting TOGA when out of SRS mode with slats extended, triggers GO AROUND mode

On DERATED takeoff (option), DO NOT USE TOGA thrust if speed is below F in CONF 2 or 3

- Consider TOGA

ENG FAIL

DETECTION

Above 400 ft and established on appropriate flight path :

ECAM ACTIONSECAM PROCEDURE

ECAM actions can be stopped at any time on PF request for trajectory, configuration, etc...

DAMAGE ?

FLY THE AIRCRAFT

CONSIDER AUTOMATION USE

NAVIGATE ⇒ LAND ASAP

PFCOMMUNICATE

400 ft AGLNO ACTION until

NO DAMAGE ?

ANNOUNCE .………………………..……”ENGINE FAILURE”The first who detects :

PF PNF

- Gear Up

- Consider TOGA

- Pitch adjust 12.5º

- Beta target Conditions

- Consider A/P

FLY THE AIRCRAFT

Beta target conditions

A330

- Slats/Flaps in CONF 1, 1+F, 2, 3 or FULL, and- one thrust lever > MCT ( > or = FLX, if FLX or DRT TO), and- at least one ENG > 1.3 EPR (or 80% N1), and- thrust asymmetry > 0.25 EPR (or 30% N1).

A340-300

- Slats/Flaps in CONF 1, 2, or 3, and- any ENG N1 > 80%, and- the difference between the ENG N1’s exceeds 30%.

A340-600

- Slats/Flaps in CONF 1, 1+F, 2, 3 or FULL, and- one thrsut lever > MCT ( > or = FLX, if FLX or DRT TO), and- thrust asymmetry > 30% N1, between ENG 2 and 3, or ENG 1 and 4.

STOP ECAM

Before reading STATUS page :

NORMAL C/L

Computer reset

ENG RELIGHT (in flight)

QRH

LAST CHANGE

REV09

JUNE 2011 MERGING BG AND PDPENG SECURED ADDED