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calculated by the FCMC, based on the CG.
Crew awareness.
F/CTL PITCH TRIM/MCDU/CG DISAGREE
Applicable to: ,
MSN
L2 The system detects a disagreement between any of the following: The real pitch trim value, the
pitch trim value calculated by the FCMC, based on the CG and the pitch trim value entered in the
MCDU.
Crew awareness.
F/CTL SENSOR FAULT
Applicable to: ALL
L2 A failure affecting a sensor in the F/CTL system is detected.
Crew awareness
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 127/142
FCOM 19 AUG 10
F/CTL RUD TRV LIM FAULT
Applicable to:
RUD WITH CARE ABV 160 KT
L2 Depending on when the failure occurs, the rudder travel limiter system may not be in the correct
position for the flight speed. Therefore, to prevent damage to the aircraft structure, use the rudder
with care, when the speed is above 160 kt.
At slats’ extension, the low speed TLU authority may be recovered.
L1 If TLU (rudder or pedals) remains locked at high speed after slat extension:
MAX X WIND FOR LDG 15 KT
AT LDG ROLL:
DIFF BRAKING.......................................................................................................AS RQRD
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 128/142
FCOM 19 AUG 10
F/CTL RUD TRV LIM FAULT (Cont'd)
L12
STATUS
RUD WITH CARE ABV 160 KT
If TLU (rudder or pedals) remains locked at high speed
after slat extension:
MAX X WIND FOR LDG 15 KT
AT LDG ROLL:
DIFF BRAKING.................................................AS RQRD
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.
APPR SPD................................................................ VLS + 10 KT
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH or Refer to 99 Duref Cible FCOM.
APPR PROC (IF ONE ENGINE INOPERATIVE)
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.
APPR SPD..........................................................................160 KT
IN CASE OF GO AROUND:
SPD...............................................................SELECT 160 KT
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH or Refer to 99 Duref Cible FCOM.
INOP SYS
RUD TRV LIM
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 129/142
FCOM 19 AUG 10
F/CTL RUDDER TRIM RUNAWAY
Applicable to:
LATERAL CONTROL....................................................................................USE TO LEVEL WINGS
RUDDER........................................................................................................................ CENTRALIZE
Check the rudder position on the F/CTL SD page.
Note: This failure is seen mainly as uncommanded roll (induced by yaw). In most conditions, the
aircraft stabilizes in a steady heading sideslip.
For continued flight, either maintain rudder central or leave the aircraft in a steady
stabilized heading sideslip, but ensure that all changes between rudder centralized and
steady heading sideslip are made smoothly. As speed is reduced, the TLU may gradually
open to allow more rudder to be applied by the trim runaway.
Note: This failure is seen mainly as uncommanded roll (induced by yaw). In most conditions, the
aircraft stabilizes in a steady heading sideslip.
For continued flight, either maintain rudder central or leave the aircraft in a steady
stabilized heading sideslip, but ensure that all changes between rudder centralized and
steady heading sideslip are made smoothly. As speed is reduced, the TLU may gradually
open to allow more rudder to be applied by the trim runaway.
DURING APPROACH
BEFORE SLATS EXTENSION:
LOWEST SAFE SPEED.............................................................................................. SELECT
In the case of TLU failure, the TLU fully opens when slats are extended, and allow more
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 7(112)
