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A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
LANDING GEAR
A330/A340 FLEET PRO-ABN-32 P 16/64
FCOM 19 AUG 10
L/G RETRACTION FAULT (Cont'd)
STATUS
MAX SPEED............................................................ 250/.55
L/G LEVER.....................................................KEEP DOWN
INCREASED FUEL CONSUMP
INOP SYS
L/G RETRACT
L/G L (R) LENGTHENING FAULT
Applicable to: ,
MAX SPEED...........................................................................................................................250/.55
L/G LEVER.....................................................................................................................KEEP DOWN
L2Note: The shock absorber performance of the affected gear is degraded. Touchdown as
smoothly as possible.
STATUS
MAX SPEED............................................................ 250/.55
L/G LEVER.....................................................KEEP DOWN
INCREASED FUEL CONSUMP
INOP SYS
L/G RETRACT
L/G L (R) LENGTHENING FAULT
Applicable to: MSN ,
,
MAX SPEED...........................................................................................................................250/.55
L/G LEVER.....................................................................................................................KEEP DOWN
L2Note: The shock absorber performance of the affected gear is degraded. Touchdown as
smoothly as possible.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
LANDING GEAR
A330/A340 FLEET PRO-ABN-32 P 17/64
FCOM 19 AUG 10
L/G L (R) LENGTHENING FAULT (Cont'd)
STATUS
MAX SPEED............................................................ 250/.55
L/G LEVER.....................................................KEEP DOWN
INCREASED FUEL CONSUMP
INOP SYS
L/G RETRACT
L/G SYS DISAGREE
Applicable to: ALL
L2 Disagreement between the landing gear positions detected by LGCIU 1 and by LGCIU 2.
Provided there is no other landing gear ECAM warning, the landing gear position is in agreement
with the L/G lever position.
Crew awareness
L/G DOORS NOT CLOSED
Applicable to: ,
L2 This warning appears, if the landing gear sequence is not completed after 30 s.
L1MAX SPEED...........................................................................................................................250/.55
If L/G lever is UP :
WHEN SPD < 250/.55 :
L/G LEVER............................................................................................................. RECYCLE
L2 Recycling the landing gear switches landing gear control to the other LGCIU.
STATUS
MAX SPEED............................................................ 250/.55
INCREASED FUEL CONSUMP
INOP SYS
L/G DOOR
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
LANDING GEAR
A330/A340 FLEET PRO-ABN-32 P 18/64
FCOM 19 AUG 10
L/G DOORS NOT CLOSED
Applicable to: MSN ,
,
L2 This warning appears, if the landing gear sequence is not completed after 30 s.
L1MAX SPEED...........................................................................................................................250/.55
If L/G lever is UP :
WHEN SPD < 250/.55 :
L/G LEVER............................................................................................................. RECYCLE
L2 Recycling the landing gear switches landing gear control to the other LGCIU.
STATUS
MAX SPEED............................................................ 250/.55
INCREASED FUEL CONSUMP
INOP SYS
L/G DOOR
L/G LGCIU 1 (2) FAULT
Applicable to: ,
GPWS (IF LGCIU 1 AFFECTED)................................................................................................. OFF
L2 As LGCIU 1 is lost, GPWS receives "landing gear in up position" information even if landing gear is
down. Setting GPWS SYS pb-sw to OFF, will prevent untimely warnings in approach.
STATUS
INOP SYS
LGCIU 1(2)
GPWS (1)
(1) (If LGCIU 1 failed)
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
LANDING GEAR
A330/A340 FLEET PRO-ABN-32 P 19/64
FCOM 19 AUG 10
L/G LGCIU 1 (2) FAULT
Applicable to:
GPWS SYS (IF LGCIU 1 AFFECTED).........................................................................................OFF
L2 As LGCIU 1 is lost, GPWS receives "landing gear in up position" information even if landing gear is
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 8(50)
