ENG MASTERS........................................................................................................OFF 30S/ON
Unassisted start attempts can be repeated until successful, or until APU BLEED is available.
IF UNSUCCESSFUL:
CREW OXY MASKS (Above FL 100)......................................................................................ON
WHEN BELOW FL 250:
APU (if operative)........................................................................................................ START
WHEN BELOW FL 200:
WING ANTI ICE............................................................................................................... OFF
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 138/196
FCOM 19 AUG 10
ENG ALL ENG FLAMEOUT - FUEL REMAINING
- ENGINE RELIGHT ATTEMPT (Cont'd)
APU BLEED....................................................................................................................... ON
IN SEQUENCE:
ENG MASTER (one at a time).................................................................... OFF 30S/ON
LAND ASAP
When APU bleed is available or if engine restart is considered definitively impossible:
OPTIMUM SPEED............................................................................REFER TO TABLE BELOW
GREEN DOT SPEED WITH ALL ENGINES INOPERATIVE (KNOTS)
Weight (1000 kg) At or below FL 200 FL 300 FL 400
280 273 283 293
260 261 271 281
240 249 259 269
220 237 247 257
200 225 235 245
180 213 223 233
160 201 211 221
140 189 199 209
120 177 187 197
At green dot speed, the aircraft can fly up to approximately 3 nm per 1 000 ft (with no wind).
Average rate of descent is approximately 1 500 ft/min.
CABIN AND COCKPIT........................................................................................................PREPARE
SEAT BELT/NO SMOKING............................................................................................................ ON
COMMERCIAL.............................................................................................................................OFF
USE RUDDER WITH CARE
WHEN BELOW FL 150:
RAM AIR.................................................................................................................................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 139/196
FCOM 19 AUG 10
ENG ALL ENG FLAMEOUT - FUEL REMAINING
- ENGINE RELIGHT ATTEMPT (Cont'd)
COMMON ACTIONS FOR THE APPROACH
APPROACH PREPARATION
Note: Final descent slope, when configured (CONF 1 ; L/G DOWN), will be approximately
700 ft/nm (with no wind).
BARO................................................................................................................................... SET
CREW MASKS/OXY SUPPLY (below FL 100).....................................................................OFF
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 140/196
FCOM 19 AUG 10
ENG ALL ENG FLAMEOUT - FUEL REMAINING
- ENGINE RELIGHT ATTEMPT (Cont'd)
IF FORCED LANDING ANTICIPATED:
LAND ASAP
APPROACH
MIN RAT SPEED..............................................................................................................140 KT
At a suitable altitude (not below 3 000 ft AGL), configure the aircraft for landing
(CONF 1 ; L/G DOWN):
LAND RECOVERY........................................................................................................... ON
FLAP 1..................................................................................................................... SELECT
EMER GEN is lost at slats’ extension. The aircraft is supplied by batteries only.
At slat extension, if FUEL MAN FWD XFR has been selected:
T TANK MODE......................................................................................................AUTO
T TANK FEED....................................................................................................... AUTO
MAX SPEED for GRAVITY EXTENSION.................................................................. 200 KT
L/G GRVTY EXTN......................................................................................................DOWN
Disregard “USE MAN PITCH TRIM” on the PFD, because the stabilizer is frozen in the
position it was at, when the windmilling was insufficient to provide hydraulic power.
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