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A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 192/196
FCOM 19 AUG 10
ENG ALL ENG FLAMEOUT - NO FUEL
REMAINING - SECURE CABIN AND COCKPIT
Applicable to:
The flight crew must apply this paper procedure. Then, if time permits, clear ECAM warnings, and
check the ECAM STATUS page.
RAT...................................................................................................................................... MAN ON
THRUST LEVERS........................................................................................................................IDLE
OPTIMUM SPEED............................................................................................. 230 KT/GREEN DOT
GREEN DOT SPEED WITH ALL ENGINES INOPERATIVE (KNOTS)
Weight (1000 kg) At or below FL 200 FL 300 FL 400
200 217 227 237
180 205 215 225
160 193 203 213
140 181 191 201
120 169 179 189
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 1 300 ft/min.
LANDING STRATEGY.................................................................................................... DETERMINE
Determine if a runway can be reached, or determine the most appropriate place for a forced
landing/ditching.
EMER ELEC POWER (if not automatically coupled)............................................................ MAN ON
VHF1............................................................................................................................................USE
ATC........................................................................................................................................NOTIFY
CREW OXY MASKS (Above FL 100)............................................................................................ ON
CABIN AND COCKPIT........................................................................................................PREPARE
SIGNS............................................................................................................................................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 193/196
FCOM 19 AUG 10
ENG ALL ENG FLAMEOUT - NO FUEL REMAINING
- SECURE CABIN AND COCKPIT (Cont'd)
COMMON ACTIONS FOR THE APPROACH
APPROACH PREPARATION
Note: Final descent slope, when configured (CONF 1 ; L/G DOWN), will be approximately
650 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 194/196
FCOM 19 AUG 10
ENG ALL ENG FLAMEOUT - NO FUEL REMAINING
- SECURE CABIN AND COCKPIT (Cont'd)
IF FORCED LANDING ANTICIPATED:
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.
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.
�� When L/G downlocked:
L/G lever...............................................................................................................DOWN
APPROACH SPEED............................................................................................170 KT
　
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