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FCOM 19 AUG 10
F/CTL RUD PEDAL FAULT (Cont'd)
L12
STATUS
MAX X WIND FOR LDG: 15 KT
APPR PROC
BEFORE AUTOLAND:
RUD TRIM (AP OFF)...................................................RESET
Manual landing is preferred, however autoland can be
performed.
The autopilot normally adjusts the rudder trim by comparing
the rudder trim command with the feedback on the rudder
pedal. As the rudder pedal is faulty, the autopilot cannot
apply rudder trim on the rudder surface, but it still internally
computes rudder trim up to its maximum value. During the
flight, the AP maintains the correct flight path, necessary by
a permanent rudder deflection (as the AP’ trim order would
have done). However, just before landing, during the align
mode, the computed maximum rudder trim is added to the
rudder demand and could cause lateral deviation. To prevent
this, the rudder trim must be reset to its zero position, before
the align mode, at around 1 000 ft.
To perform this reset, the autopilot must be disconnected and
then reconnected to perform the autoland.
AT LDG ROLL:
DIFF BRAKING....................................................... AS RQRD
INOP SYS
RUD PEDAL
RUD TRIM
Loss of nosewheel steering
via the pedals ; however,
it remains available using
the handwheel. The rudder
may be deflected by the
yaw damper.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 141/142
FCOM 19 AUG 10
F/CTL RUD NORM CTL FAULT
Applicable to: ,
USE RUD FOR TURN COORD
RUD WITH CARE ABV 160 KT
L2 The backup control module takes over the rudder control but cannot ensure the rudder travel limit
function. Therefore, to prevent damage to the aircraft structure, use the rudder with care, when the
speed is above 160 kt. However, aerodynamic limitations ensure that excessive load cannot be
reached on the rudder.
L12
STATUS
RUD WITH CARE ABV 160 KT
USE RUD FOR TURN COORD
RUD BACKUP CTL
See (1)
(1) RL2udder via the rudder backup module.
F/CTL RUD PRIM (SEC) 1 FAULT
Applicable to: ,
L2Crew awareness.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
Intentionally left blank
A330/A340 FLEET PRO-ABN-27 P 142/142
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FUEL
A330/A340 FLEET PRO-ABN-28 P 1/98
FCOM 19 AUG 10
FUEL PUMP 1(2)(3)(4) LO PR
Applicable to:
L2 The corresponding standby pump automatically replaces the faulty main pump
L1 PUMP (AFFECTED)......................................................................................................................OFF
STATUS
INOP SYS
FUEL PUMP (affected)
FUEL LEFT (RIGHT) PUMP 1(2) LO PR
Applicable to: ,
L2 The corresponding standby pump automatically replaces the faulty main pump.
L1 PUMP (AFFECTED)......................................................................................................................OFF
STATUS
INOP SYS
FUEL AFT XFR
L (R) FUEL PUMP 1(2)
FUEL PUMPS 1(2)(3)(4) + STBY LO PR
Applicable to:
X FEED (AFFECTED SIDE)...........................................................................................................ON
PUMP (AFFECTED)......................................................................................................................OFF
PUMP (AFFECTED) STBY........................................................................................................... OFF
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FUEL
A330/A340 FLEET PRO-ABN-28 P 2/98
FCOM 19 AUG 10
FUEL PUMPS 1(2)(3)(4) + STBY LO PR (Cont'd)
STATUS
FUEL CELL 1 BY GRVTY ONLY (2)(3)(4) INOP SYS
FUEL AFT XFR (1)
F. PUMP 1+STBY (2)(3)(4)
(1) (Only if CTR TK empty)
FUEL L(R) STBY PUMP LO PR
Applicable to: ,
STBY PUMP (AFFECTED)........................................................................................................... OFF
STATUS
INOP SYS
FUEL AFT XFR
L (R) FUEL STBY
FUEL L(R) CTR PUMP LO PR
Applicable to: ,
CTR PUMP (AFFECTED)............................................................................................................. OFF
STATUS
INOP SYS
L(R) CTR PUMP
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 7(116)
