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third failure occurs, the ELEV REDUND LOST PROC and associated FL and speed limitations no
longer apply. In this case, if the MAN PITCH TRIM ONLY message is displayed, it is recommended
that the autothrust be disconnected to improve longitudinal control of the aircraft.
L1 The autopilot is not available.
SPD BRK.......................................................................................................................DO NOT USE
MAX FL.........................................................................................................................................300
MAX SPEED.............................................................................................................................M0.75
�� WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE...................................................................................................................... FWD
L2 Fuel consumption is increased by approximately 1 %.
Displayed, if the trim tank pump is failed.
L12
STATUS
SPD BRK.......................................................DO NOT USE
MAX FL.......................................................................... 300
MAX SPEED.............................................................. M0.75
�� WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE................................................................ FWD
Displayed, if the trim tank pump is failed.
APPR PROC
�� AT SLATS EXTENSION:
T TANK XFR..................................................................AUTO
INOP SYS
CAT 3 DUAL
Note: The STATUS and
the INOP SYS
list is completed
according to the
failures, which led
to the elevator
redundancy loss
(green system,
PRIM 2 or SEC 2).
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 74/142
FCOM 19 AUG 10
F/CTL ELEV REDUND LOST
(AILERONS ARE NOT PRESET)
Applicable to: MSN ,
,
L2 This caution is triggered, in case of dual failure, when a subsequent third failure affecting the
F/CTL system may lead to degraded pitch control or pitch mechanical backup. Certain failure
combinations lead to an aileron preset to limit the pitch up effect in case of this third failure. If this
third failure occurs, the ELEV REDUND LOST PROC and associated FL and speed limitations no
longer apply. In this case, if the MAN PITCH TRIM ONLY message is displayed, it is recommended
that the autothrust be disconnected to improve longitudinal control of the aircraft.
L1 The autopilot is not available.
SPD BRK.......................................................................................................................DO NOT USE
MAX FL.........................................................................................................................................300
MAX SPEED.............................................................................................................................M0.75
�� WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE...................................................................................................................... FWD
L2 Fuel consumption is increased by approximately 1 %.
Displayed, if the trim tank pump is failed.
L12
STATUS
SPD BRK.......................................................DO NOT USE
MAX FL.......................................................................... 300
MAX SPEED.............................................................. M0.75
�� WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE................................................................ FWD
Displayed, if the trim tank pump is failed.
APPR PROC
�� AT SLATS EXTENSION:
T TANK XFR..................................................................AUTO
INOP SYS
CAT 3 DUAL
Note: The STATUS and
the INOP SYS
list is completed
according to the
failures, which led
to the elevator
redundancy loss
(green system,
PRIM 2 or SEC 2).
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 75/142
FCOM 19 AUG 10
F/CTL STAB CTL FAULT
Applicable to:
MAN PITCH TRIM................................................................................................................... CHECK
L2 The force needed on the pitch trim wheel may be higher than usual (pre-takeoff manual setting).
L1�� IF MAN TRIM AVAIL:
TRIM FOR NEUTRAL ELEV
L2 If man pitch trim is available, trim to maintain elevator at zero position (indications on F/CTL SD
　
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