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STATUS
MAX SPEED............................................................ 305/.82
APPR PROC
FOR LDG...................................................................USE FLAP 3
This line is replaced by “FOR LDG: USE FLAP 3” when CONF 3
is selected, as a reminder.
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH or Refer to 99 Duref Cible FCOM.
USE RUD FOR TURN COORD
ALTN LAW: PROT LOST
INOP SYS
F/CTL PROT
YAW DAMPER
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 122/142
FCOM 19 AUG 10
F/CTL YAW DAMPER FAULT
Applicable to:
L2 Loss of yaw damper 1 + 2.
L1 USE RUD FOR TURN COORD
ASSOCIATED PROCEDURES
F/CTL ALTN LAW (PROT LOST)
MAX SPEED...........................................................................................................................305/.82
STATUS
MAX SPEED............................................................ 305/.82
APPR PROC
FOR LDG...................................................................USE FLAP 3
USE RUD FOR TURN COORD
ALTN LAW: PROT LOST
INOP SYS
F/CTL PROT
YAW DAMPER
AP 1 + 2
CAT 2
L12
STATUS
MAX SPEED............................................................ 305/.82
APPR PROC
FOR LDG...................................................................USE FLAP 3
This line is replaced by “FOR LDG: USE FLAP 3” when CONF 3
is selected, as a reminder.
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH or Refer to 99 Duref Cible FCOM.
USE RUD FOR TURN COORD
ALTN LAW: PROT LOST
INOP SYS
F/CTL PROT
YAW DAMPER
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 123/142
FCOM 19 AUG 10
F/CTL YAW DAMPER FAULT - FWSPAGE
Applicable to:
STATUS
MAX SPEED............................................................ 305/.82
APPR PROC
FOR LDG...................................................................USE FLAP 3
USE RUD FOR TURN COORD
ALTN LAW: PROT LOST
INOP SYS
F/CTL PROT
YAW DAMPER
AP 1 + 2
CAT 2
CONFIG RUD TRIM NOT IN T.O RANGE
Applicable to: ALL
L2Crew awareness
F/CTL RUD TRIM 1(2) FAULT
Applicable to: ,
L2Crew awareness
STATUS
CAT 3 SINGLE ONLY INOP SYS
RUD TRIM 1(2)
CAT 3 DUAL
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 124/142
FCOM 19 AUG 10
F/CTL RUD TRIM 1(2) FAULT
Applicable to: MSN ,
,
L2Crew awareness
STATUS
CAT 3 SINGLE ONLY INOP SYS
RUD TRIM 1(2)
CAT 3 DUAL
F/CTL RUD TRIM FAULT
Applicable to: ,
L2Crew awareness
STATUS
INOP SYS
RUD TRIM
AP 1 + 2
CAT 2
F/CTL RUD TRIM FAULT
Applicable to: MSN ,
,
L2Crew awareness
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 125/142
FCOM 19 AUG 10
F/CTL RUD TRIM FAULT (Cont'd)
STATUS
INOP SYS
RUD TRIM
AP 1 + 2
CAT 2
F/CTL RUD TRV LIM 1(2) FAULT
Applicable to:
L2Crew awareness
STATUS
INOP SYS
RUD TRV LIM 1(2)
F/CTL RUD G (Y)(B) SERVO JAM
Applicable to:
L2Crew awareness
Note: If the F/CTL RUD G(Y)(B) SERVO JAM warning occurs at engine start:
‐ Reset FCDC 1 and 2
‐ Select the non affected LEAK MEASUREMENT valves OFF
‐ Perform a rapid and full deflection of the rudder.
If no new warning is triggered, disregard the previous one, and reselect the LEAK
MEASUREMENT valves ON.
Note: If the G and Y LEAK MEASUREMENT valves have been selected OFF, at the
end of the above test the rudder will be deflected 1.5 ° to the right.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 126/142
FCOM 19 AUG 10
F/CTL PEDAL SENSOR FAULT
Applicable to: ,
L2 A failure affecting a pedal sensor is detected.
Crew awareness.
F/CTL PITCH TRIM/MCDU/CG DISAGREE
Applicable to:
L2 The system detects a disagreement between: The real pitch trim value and the pitch trim value
　
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