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rudder to be applied than is safe for the structure.
Full rudder is not permitted above 160 kt.
RUDDER.................................................................................................MAINTAIN CENTRAL
Care must be taken to keep rudder steady and approximately centralized during slats
extension, until the TLU has released.
SEC 1................................................................................................................OFF THEN ON
SEC 2................................................................................................................OFF THEN ON
FOR LDG...................................................................................................... USE NORMAL CONF
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 130/142
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.
FOR LDG.......................................................................................................... USE NORMAL CONF
F/CTL PRIM 1(2)(3) (SEC 1)(2) PITCH FAULT
Applicable to: ,
L2 Failure of pitch channel in the associated computer.
Crew awareness
STATUS
• IF F/CTL PRIM1 PITCH FAULT
CAT 3 SINGLE ONLY
INOP SYS
CAT 3 DUAL (1)
(1) (IF F/CTL PRIM1 PITCH FAULT)
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 131/142
FCOM 19 AUG 10
F/CTL PRIM 1(2)(3) (SEC 1)(2) PITCH FAULT
Applicable to: MSN ,
,
L2 Failure of pitch channel in the associated computer.
Crew awareness
STATUS
• IF F/CTL PRIM1 PITCH FAULT
CAT 3 SINGLE ONLY
INOP SYS
CAT 3 DUAL (1)
(1) (IF F/CTL PRIM1 PITCH FAULT)
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 132/142
FCOM 19 AUG 10
F/CTL RUDDER JAM/RUDDER PEDAL JAM
Applicable to:
Rudder jamming may be detected by undue (and adverse) pedal movement during rolling
maneuvers.
This is because yaw damper orders can no longer be sent to the rudder, but are fed back to the
pedals.
Use the F/CTL SD page for a visual check of the rudder position.
This procedure also applies to RUDDER PEDAL JAM cases.
FOR APPROACH
AVOID LANDING WITH CROSSWIND from the side where the rudder is deflected.
FOR LANDING............................................................................................................ USE FLAP 2
GPWS FLAP MODE..................................................................................................................OFF
�� If all engines are operative:
APPR SPD................................................................................................................. VLS + 10
SPEED and TRAJECTORY.......................................................................... STABILIZE ASAP
LDG DIST PROC........................................................................................................... APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
�� In case of an Engine-Out:
APPR SPEED............................................................................................................ 160 knots
SPEED and TRAJECTORY.......................................................................... STABILIZE ASAP
　
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