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L/G..................................................................KEEP DOWN
INCREASED FUEL CONSUMP
INOP SYS
L/G RETRACT
Flight with the landing gear
extended has a significant
effect on fuel consumption
and climb gradient (Refer
to PRO-SPO-25-10
GENERAL). Multiply
fuel consumption by
approximately 2.8.
L/G GEAR UPLOCK FAULT
Applicable to: ,
MSN,,,,
L/G................................................................................................................................KEEP DOWN
L2 The landing gear must be left down to avoid structural damage, because the uplock device will stay
in the locked position.
L1MAX SPEED...........................................................................................................................280/.67
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
LANDING GEAR
A318/A319/A320/A321 FLEET PRO-ABN-32 P 19/76
FCOM 19 AUG 10
L/G GEAR UPLOCK FAULT (Cont'd)
L12
STATUS
MAX SPEED............................................................ 280/.67
L/G..................................................................KEEP DOWN
INCREASED FUEL CONSUMP
INOP SYS
L/G RETRACT
Flight with the landing gear
extended has a significant
effect on fuel consumption
and climb gradient (Refer
to PRO-SPO-25-10
GENERAL). Multiply
fuel consumption by
approximately 2.8.
L/G BOGIE ALIGN FAULT
Applicable to:
L2 A bogie is not correctly aligned after liftoff, or becomes incorrectly aligned during flight. The landing
gear retraction is inhibited.
L1MAX SPEED...........................................................................................................................280/.67
L2 Speed must be limited to VLE, as the landing gear must be kept down.
L1 L/G................................................................................................................................KEEP DOWN
STATUS
MAX SPEED............................................................ 280/.67
L/G..................................................................KEEP DOWN
INOP SYS
L/G RETRACT
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
LANDING GEAR
A318/A319/A320/A321 FLEET PRO-ABN-32 P 20/76
FCOM 19 AUG 10
L/G BOGIE ALIGN FAULT
Applicable to: ,
L2 A bogie is not correctly aligned after liftoff, or becomes incorrectly aligned during flight. The landing
gear retraction is inhibited.
L1MAX SPEED...........................................................................................................................280/.67
L2 Speed must be limited to VLE, as the landing gear must be kept down.
L1 L/G................................................................................................................................KEEP DOWN
STATUS
MAX SPEED............................................................ 280/.67
L/G..................................................................KEEP DOWN
INOP SYS
L/G RETRACT
L/G BOGIE ALIGN FAULT
Applicable to: ,
MSN,,,,
L2 A bogie is not correctly aligned after liftoff, or becomes incorrectly aligned during flight. The landing
gear retraction is inhibited.
L1MAX SPEED...........................................................................................................................280/.67
L2 Speed must be limited to VLE, as the landing gear must be kept down.
L1 L/G................................................................................................................................KEEP DOWN
STATUS
MAX SPEED............................................................ 280/.67
L/G..................................................................KEEP DOWN
INOP SYS
L/G RETRACT
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
LANDING GEAR
A318/A319/A320/A321 FLEET PRO-ABN-32 P 21/76
FCOM 19 AUG 10
L/G SYS DISAGREE
Applicable to: ALL
L2 Disagreement between the landing gear positions are detected by LGCIU 1 and LGCIU 2. Provided
there is no other L/G ECAM warning, the landing gear position is in agreement with the landing
gear lever position.
Crew awareness.
L/G GEAR NOT DOWN
Applicable to: ALL
L2 This warning appears in approach at 750 ft RA, if the landing gear is not set to DOWN, and the
system has not failed. When this warning appears, the red arrow on the instrument panel comes
on.
　
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