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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 100/142
FCOM 19 AUG 10
F/CTL L (R) ELEV FAULT (Cont'd)
L12
STATUS
SPD BRK.......................................................DO NOT USE
MAX SPEED............................................................ 330/.82
APPR PROC
�� If elevator oscillation detected:
AP......................................................................................OFF
GPWS FLAP MODE................................................................OFF
FOR LDG...................................................................USE FLAP 2
APPR SPD................................................................ VLS + 10 KT
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
ALTN LAW: PROT LOST
INOP SYS
F/CTL PROT
AP 1 + 2 (1)
L (R) ELEV
CAT 2 (1)
(1) (Not displayed, in case the elevator is frozen at zero, subsequent to elevator oscillation)
F/CTL ELEV SERVO FAULT
Applicable to: ,
L2 The remaining servojack controls the elevator
Crew awareness
STATUS
CAT 3 SINGLE ONLY INOP SYS
CAT 3 DUAL
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 101/142
FCOM 19 AUG 10
F/CTL ELEV SERVO FAULT
Applicable to: MSN ,
,
L2 The remaining servojack controls the elevator
Crew awareness
STATUS
CAT 3 SINGLE ONLY INOP SYS
CAT 3 DUAL
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 102/142
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
L2Note: Fuel consumption is increased by approximately 1 %.
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 103/142
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
　
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