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L1�� If the trim tank pump is inoperative or not installed:
�� IF CG AFT 32 % AND WHEN SPEED > 270 KT AND NOT IN CLIMB:
T TANK MODE................................................................................................................FWD
L2Note: Fuel consumption is increased by approximately 1 %.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 107/142
FCOM 19 AUG 10
F/CTL L + R ELEV FAULT (Cont'd)
L12
STATUS
SPD BRK.......................................................DO NOT USE
MAX SPEED............................................................ 305/.80
MANEUVER WITH CARE
APPR PROC
FOR LDG...................................................................USE FLAP 2
This line is replaced by “FOR LDG: USE FLAP 2” when CONF 2
is selected, as a reminder.
Do not select CONF FULL so as not to degrade handling
qualities.
GPWS FLAP MODE................................................................OFF
APPR SPD................................................................ VLS + 10 KT
MAN PITCH TRIM...................................................................USE
�� If the trim tank pump is operative:
�� IF CG AFT 32 %:
T TANK MODE..........................................................FWD
Note: Fuel consumption is increased by
approximately 1 %.
�� If the trim tank pump is inoperative or not installed:
�� IF CG AFT 32 % AND WHEN SPEED > 270 KT AND
NOT IN CLIMB:
T TANK MODE..........................................................FWD
Note: Fuel consumption is increased by
approximately 1 %.
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
PITCH MECH BACK UP
ROLL DIRECT LAW
INOP SYS
L + R ELEV
F/CTL PROT
AP 1 + 2
CAT 2
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 108/142
FCOM 19 AUG 10
F/CTL L + R ELEV FAULT (Cont'd)
L12
STATUS
SPD BRK.......................................................DO NOT USE
MAX SPEED............................................................ 305/.80
MANEUVER WITH CARE
APPR PROC
GPWS FLAP MODE................................................................OFF
FOR LDG...................................................................USE FLAP 2
This line is replaced by “FOR LDG: USE FLAP 2” when CONF 2
is selected, as a reminder.
Do not select CONF FULL so as not to degrade handling
qualities.
APPR SPD................................................................ VLS + 10 KT
MAN PITCH TRIM...................................................................USE
�� If the trim tank pump is operative:
�� IF CG AFT 32 %:
T TANK MODE..........................................................FWD
�� If the trim tank pump is inoperative or not installed:
�� IF CG AFT 32 % AND WHEN SPEED > 270 KT AND
NOT IN CLIMB:
T TANK MODE..........................................................FWD
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
PITCH MECH BACK UP
ROLL DIRECT LAW
INOP SYS
L + R ELEV
F/CTL PROT
AP 1 + 2
CAT 2
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 109/142
FCOM 19 AUG 10
F/CTL L + R ELEV FAULT
Applicable to:
PITCH MECH BACK UP
SPD BRK.......................................................................................................................DO NOT USE
L2 Do not use speed brakes, because it is difficult to control the induced pitch moment with manual
pitch trim only.
L1MAX SPEED...........................................................................................................................305/.80
L2 Due to loss of high speed protections.
L1MAN PITCH TRIM........................................................................................................................ USE
L2 Only manual trim is available for pitch control. To improve the longitudinal control of the aircraft it is
recommended to disconnect the autothrust.
L1MANEUVER WITH CARE
�� If the trim tank pump is operative:
�� IF CG AFT 32 %:
T TANK MODE................................................................................................................FWD
　
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