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FOR LDG ................................................................. USE FLAP 3
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
CONSIDER APU GEN USE
• If ENG 1 shutdown:
SLATS SLOW
• if ENG 2 shutdown:
FLAPS SLOW
CAT 3 SINGLE ONLY
See (2)
INOP SYS
BLUE HYD (YELLOW HYD)
PART SPLRS
REV 1(2)
CAT 3 DUAL
ENG 1 (2) BLEED
PACK 1(2)
G ENG 1(2) PUMP
B ENG 1 PUMP
(Y ENG 2 PUMP)
GEN 1 (2)
ALTN BRK (1)
PART GALLEY
(1) (If ENG 1 shutdown)
(2)
NL2ote: If one ENG FIRE pb has been pressed, the A/THR may be inoperative for RR and PW
engines. Therefore, landing capability is degraded to CAT 2.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 21/196
FCOM 19 AUG 10
ENG 1(2) AFTER SHUT DOWN
Applicable to:
LAND ASAP
ENG START SEL...........................................................................................................................IGN
L2Continuous ignition is selected to protect the remaining engine.
Note: If the Y ELEC PUMP is running after ENG 2 failure (engine failure before flaps retraction),
SWITCH OFF the pump when in clean configuration.
L1 L/G (DISPLAYED DURING THE TAKEOFF PHASE).....................................................................UP
FUEL IMBALANCE..............................................................................................................MONITOR
L2 The FUEL IMBALANCE ...... MONITOR action line is not displayed in the case of an engine feed
line burst.
Note: If engine windmilling induces transient HYD SYS LO PR warnings, it is recommended that
flight crew switch OFF the hydraulic pumps associated with the failed engine. Procedure
only applicable when engine will not be restarted.
L1 TCAS MODE SEL �� ....................................................................................................................TA
L12
SECONDARY FAILURES
* ELEC
* HYD
* F/CTL
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 22/196
FCOM 19 AUG 10
ENG 1(2) AFTER SHUT DOWN (Cont'd)
NL2ote: In some conditions,
with full asymmetric
power, the aircraft
may be control-limited
before reaching
the limits of the
protection system.
Therefore, in extreme
conditions, where
low speed may be
advantageous (GPWS,
WINDSHEAR, etc),
reduce speed with
care below VLS and
respect the minimum
control speed.
L12
ASSOCIATED PROCEDURES
AIR ABNORM BLEED CONFIG
Refer to PRO-ABN-36-C AIR ABNORM BLEED CONFIG
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 23/196
FCOM 19 AUG 10
ENG 1(2) AFTER SHUT DOWN (Cont'd)
L12
STATUS
FUEL IMBALANCE........................................................MONITOR
APPR PROC
�� BEFORE S/F EXTENSION:
�� If ENG 1 S/D and green hyd lost:
BLUE ELEC PUMP.................................................... OFF
�� If ENG 2 S/D and green hyd lost:
YELLOW ELEC PUMP...............................................OFF
FOR LDG ................................................................. USE FLAP 3
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
CONSIDER APU GEN USE
• If ENG 1 shutdown:
SLATS SLOW
• if ENG 2 shutdown:
FLAPS SLOW
CAT 3 SINGLE ONLY
See (2)
INOP SYS
BLUE HYD (YELLOW HYD)
PART SPLRS
REV 1(2)
CAT 3 DUAL
ENG 1 (2) BLEED
PACK 1(2)
G ENG 1(2) PUMP
B ENG 1 PUMP
(Y ENG 2 PUMP)
GEN 1 (2)
ALTN BRK (1)
PART GALLEY
(1) (If ENG 1 shutdown)
(2)
NL2ote: If one ENG FIRE pb has been pressed, the A/THR may be inoperative for RR and PW
engines. Therefore, landing capability is degraded to CAT 2.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 24/196
FCOM 19 AUG 10
ENG ALL ENG FLAME OUT
Applicable to:
L2 This warning inhibits the ELEC EMER CONFIG warning, and provides the flight crew with the
immediate actions to take in the case of a failure of all engines. This procedure then directs the
　
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