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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 40/196
FCOM 19 AUG 10
ENG ALL ENG FLAME OUT (Cont'd)
L2 The ENG ALL ENG FLAME OUT warning inhibits the ELEC EMER CONFIG warning. The FCOM
Volume 3 includes all step of the ENG ALL ENG FLAME OUT procedure. However, to facilitate
handling of all the ECAM procedure associated with an engine flameout, it is recommended using
the QRH ENG ALL ENG FLAME OUT paper procedure that also includes the DITCHING and
FORCED LANDING procedure.
When applying the QRH ENG ALL ENG FLAME OUT paper procedure:
If one or more engines are recovered, applying the corresponding ‐ ECAM procedure instead.
‐ If no engines are recovered, continue to apply the QRH ENG ALL ENG FLAME OUT paper
procedure. If time permits, clear the ECAM alerts, and check the STATUS SD page.
L1 LAND ASAP
RAT...................................................................................................................................... MAN ON
ENG START SEL...........................................................................................................................IGN
L2 If at any time all engines recover, refer to the end of this ENG ALL ENG FLAME OUT procedure for
the applicable ECAM procedure and status.
L1 THR LEVERS............................................................................................................................. IDLE
OPTIMUM RELIGHT SPD......................................................................................................300/0.82
L2 Increase speed during descent toward 300 kt. Do not exceed MMO.
300 kt/M 0.82 is the optimum airspeed for windmilling start.One fuel pump remains supplied down
to 260 kt. At 300 kt/M 0.82 with all engines stopped, it takes about 15 min to descend from FL 400
to the ground. Distance is about 100 nm. In case of a speed indication failure (volcanic ash), the
pitch altitude for optimum relight speed is 2 ° down. For weight above 150 000 kg/330 000 lb raise
the nose by 0.5 ° for every additional 20 000 kg /44 000 lb (e.g. if weight is 170 000 kg /374 000 lb
pitch is 1.5 ° down).
L1 EMER ELEC PWR (IF NOT AUTOMATICALLY COUPLED)................................................MAN ON
VHF1............................................................................................................................................USE
L2 Only VHF 1 is always supplied. Notify ATC of the nature of emergency and state intentions. If there
is no contact with air traffic control, transmit a distress message on VHF frequency 121.5 MHz .
L1�� IF NO RELIGHT AFTER 30 SEC:
ENG MASTERS........................................................................................................OFF 30S/ON
L2Must be OFF for 30 s to allow ventilation of combustion chamber. Unassisted start attempts
can be repeated until successful, or until APU BLEED available
L1�� IF UNSUCCESSFUL:
CREW OXY MASK (ABOVE FL100)....................................................................................... ON
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 41/196
FCOM 19 AUG 10
ENG ALL ENG FLAME OUT (Cont'd)
�� WHEN BELOW FL 250:
APU (IF OPERATIVE).................................................................................................START
�� WHEN BELOW FL 200:
WING ANTI ICE............................................................................................................... OFF
APU BLEED....................................................................................................................... ON
�� IN SEQUENCE:
ENG MASTERS (ONE AT A TIME)........................................................... OFF 30 S/ON
OPTIMUM SPEED (WHEN APU BLEED AVAIL)....................................................... 250 KT
L2 Green dot speed is not displayed on the captain's PFD. Initially use 250 kt before checking
the QRH.
L1 USE RUD WITH CARE
L2 If forced landing or ditching is expected, use the QRH's Forced Landing or Ditching
procedure.
L1�� EARLY IN APPROACH:
CAB SECURE............................................................................................................ ORDER
�� FOR SLATS EXTENSION:
LAND RECOVERY.............................................................................................................ON
FOR LDG............................................................................................................USE FLAP 1
L2 At FLAP 1 selection, the emergency generator stops.
　
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