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�� If L/G lever still down :
L/G.....................................................................................................................KEEP DOWN
�� If L/G lever selected up :
L/G..............................................................................................................................DOWN
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 4/76
FCOM 19 AUG 10
L/G SHOCK ABSORBER FAULT (Cont'd)
(SHOCK ABSORBER NOT EXTENDED AFTER LIFTOFF)
L12
STATUS
MAX SPEED............................................................ 280/.67
L/G..................................................................KEEP DOWN
INCREASED FUEL CONSUMP
See (1)
INOP SYS
L/G RETRACT
(1) FL2light with landing gear extended has a significant effect on fuel consumption and climb gradient
(Refer to1997 **Not found**).
Note: If WHEEL N.W. STEER FAULT is also displayed, then the nose wheels may be at
maximum deflection. (Turned 90 ° from center). During landing, delay nose wheel
touchdown for as long as possible
L12
STATUS
• If L/G not uplocked:
MAX SPEED......................................................280/.67
L/G...........................................................KEEP DOWN
INCREASED FUEL CONSUMP
See (1)
INOP SYS
L/G RETRACT
(1) FL2light with landing gear extended has a significant effect on fuel consumption and climb gradient
(Refer to1997 **Not found**).
Note: If WHEEL N.W. STEER FAULT is also displayed, then the nose wheels may be at
maximum deflection. (Turned 90 ° from center). During landing, delay nose wheel
touchdown for as long as possible
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
LANDING GEAR
A318/A319/A320/A321 FLEET PRO-ABN-32 P 5/76
FCOM 19 AUG 10
L/G SHOCK ABSORBER FAULT
(SHOCK ABSORBER NOT EXTENDED AFTER LIFTOFF)
Applicable to: , , MSN,,,,
�� Shock absorber not extended after liftoff and L/G uplocked :
Crew awareness
�� Shock absorber not extended after liftoff and L/G not uplocked :
MAX SPEED...................................................................................................................... 280/.67
�� If L/G lever still down :
L/G.....................................................................................................................KEEP DOWN
�� If L/G lever selected up :
L/G..............................................................................................................................DOWN
L12
STATUS
• If L/G not uplocked:
MAX SPEED......................................................280/.67
L/G...........................................................KEEP DOWN
INCREASED FUEL CONSUMP
See (1)
INOP SYS
L/G RETRACT
(1) FL2light with landing gear extended has a significant effect on fuel consumption and climb gradient
(Refer to1997 **Not found**).
Note: If WHEEL N.W. STEER FAULT is also displayed, then the nose wheels may be at
maximum deflection. (Turned 90 ° from center). During landing, delay nose wheel
touchdown for as long as possible
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
LANDING GEAR
A318/A319/A320/A321 FLEET PRO-ABN-32 P 6/76
FCOM 19 AUG 10
L/G GEAR NOT UPLOCKED
Applicable to:
L2 This warning appears if the landing gear sequence is not completed after 30 s.
L1�� L/G doors closed:
AVOID EXCESS G FACTOR
L2 Because the gear rests on the doors, avoid excessive load factors in order not to damage door
structure.
L1�� L/G doors not closed:
MAX SPEED...................................................................................................................... 220/.54
L/G...............................................................................................................................RECYCLE
�� IF UNSUCCESSFUL:
L/G..............................................................................................................................DOWN
MAX SPEED................................................................................................................280/.67
L12
STATUS
MAX SPEED............................................................ 280/.67
INCREASED FUEL CONSUMP
See (1)
INOP SYS
L/G RETRACT
(1)
NL2ote: Flight with landing gear extended has a significant ‐ effect on fuel consumption and
　
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