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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
AT SLAT EXTENSION (if a FUEL 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
CONSIDER APU GEN USE
MCDU BACK UP NAV AVAIL
INOP SYS
See below
INOP SYS
F/CTL PROT STABILIZER B+Y HYD
PACK 1+2 PRIM 2+3 ADR 2+3
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 46/196
FCOM 19 AUG 10
ENG ALL ENG FLAME OUT (Cont'd)
RA 1+2 A/CALL OUT ANTI SKID
RUD TRIM WING A.ICE AP 1+2
MOST SPLRS REVERSERS CAT 2
HF 1+2 N/W STRG AUTO BRK
ALTN BRK MOST F. PUMPS GPS 2
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 47/196
FCOM 19 AUG 10
ENG ALL ENG FLAME OUT
Applicable to:
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
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 8(139)
