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Average rate of descent is approximately 1 300 ft/min.
CABIN AND COCKPIT........................................................................................................PREPARE
SEAT BELT/NO SMOKING............................................................................................................ ON
COMMERCIAL.............................................................................................................................OFF
USE RUDDER WITH CARE
�� WHEN BELOW FL 150:
RAM AIR.................................................................................................................................ON
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 146/196
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.
�� When L/G downlocked:
L/G lever...............................................................................................................DOWN
APPROACH SPEED............................................................................................170 KT
Adjust the speed to the above given Vapp. Nevertheless, to reach the landing
field/runway, the approach speed may be adjusted up to 240 kt (max speed with
landing gear extended).
GND SPLR.............................................................................................................. ARM
MAX BRK PR................................................................................................... 1000 PSI
AT 2 000 FT AGL
CABIN....................................................................................................NOTIFY FOR LANDING
AT 500 FT AGL
BRACE FOR IMPACT..................................................................................................... ORDER
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 147/196
FCOM 19 AUG 10
ENG ALL ENG FLAMEOUT - FUEL REMAINING
- ENGINE RELIGHT ATTEMPT (Cont'd)
AT TOUCHDOWN
ENG MASTERS.....................................................................................................................OFF
APU MASTER SW................................................................................................................ OFF
BRAKES ON ACCU ONLY
AFTER LANDING
�� When the aircraft has stopped:
PARKING BRK................................................................................................................. ON
ATC (VHF1).............................................................................................................. NOTIFY
FIRE pushbutton (ENG and APU)............................................................................... PUSH
AGENTS (ENG and APU).......................................................................................... DISCH
　
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