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disregarded, as the MCDU BACK UP NAV is not available when the CSM/G is powered
by the RAT.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 27/196
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
flight crew to apply the applicable QRH procedure, depending on if there is fuel or not.
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
EMER ELEC PWR (IF NOT AUTOMATICALLY COUPLED)................................................MAN ON
THR LEVERS............................................................................................................................. IDLE
�� IF FUEL REMAINS:
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.
L1OPT RELIGHT SPD...........................................................................................................300 KT
L2 If there is fuel remaining , the optimum speed is the optimum relight speed.
The ECAM provides reference to an envelope speed. In case of speed indication failure
(volcanic ash), pitch altitude for optimum relight is provided in the paper procedure.
L1 ENG/FUEL PROC.............................................................................................................. APPLY
L2 Refer to the ENG ALL ENG FLAME OUT – FUEL REMAINING paper procedure in the Refer
to PRO-ABN-70-AF ENG ALL ENG FLAMEOUT - FUEL REMAINING - ENGINE RELIGHT
ATTEMPT or in the Refer to 99 Duref Cible QRH
L1�� IF NO FUEL:
OPT SPD.....................................................................................................250 KT/GREEN DOT
L2 If there is no fuel remaining, the optimum speed is the green dot speed.
Initially fly 250 kt then refer to the paper procedure to get the accurate green dot speed.
L1 ENG/ NO FUEL PROC...................................................................................................... APPLY
L2 Refer to the ENG ALL ENG FLAME OUT – FUEL REMAINING paper procedure in the Refer
to PRO-ABN-70-AG ENG ALL ENG FLAMEOUT - NO FUEL REMAINING - SECURE CABIN
AND COCKPIT or in the Refer to 99 Duref Cible QRH
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 28/196
FCOM 19 AUG 10
ENG ALL ENG FLAME OUT (Cont'd)
L12
STATUS
SPD BRK.......................................................DO NOT USE
MAX SPEED.......................................................... 305/0.82
MIN RAT SPEED..................................................... 140 KT
MANEUVER WITH CARE
AVOID ICING CONDITIONS
MAX BRK PR........................................................1000 PSI
APPR PROC
LAND ASAP
�� FOR SLATS EXTENSION:
LAND RECOVERY............................................................. ON
FOR LDG............................................................ USE FLAP 1
This line is replaced by "FOR LDG : USE FLAP 1" when
CONF 1 is selected, as a remainder.
�� AT SLAT EXTENSION (if a FUEL MAN FWD XFR has been
selected):
T TK MODE................................................................... AUTO
T TK FEED.................................................................... AUTO
�� FOR L/G GRVTY EXTN:
MAX SPEED................................................................ 200 KT
L/G GRVTY EXTN........................................................DOWN
�� WHEN L/G DOWNLOCKED:
L/G................................................................................ DOWN
PITCH AUTHORITY REDUCED
TARGET SPD.............................................................. 170 KT
ALTN LAW: PROT LOST
See (1)
INOP SYS
See below
INOP SYS
To be continued on next page
A330/A340 FLIGHT CREW
　
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