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OVERFLOW ON THE STATUS Page:
PRESS AND MAINTAIN the STS KEY ON the ECP
The first page of STATUS appears.
RELEASE IT, THEN PRESS AGAIN WITHIN 2 s
The second page of STATUS appears.
CONTINUE UNTIL THE OVERFLOW ARROW DISAPPEARS.
When the STS key is released for more than 2 s, the EWD reappears.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
LANDING GEAR
A318/A319/A320/A321 FLEET PRO-ABN-32 P 1/76
FCOM 19 AUG 10
L/G SHOCK ABSORBER FAULT
(SHOCK ABSORBER EXTENDED ON THE GROUND)
Applicable to: ALL
L2Crew awareness
L/G SHOCK ABSORBER FAULT
(SHOCK ABSORBER NOT EXTENDED AFTER LIFTOFF)
Applicable to:
MAX SPEED...........................................................................................................................280/.67
L/G................................................................................................................................KEEP DOWN
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
L/G SHOCK ABSORBER FAULT
(SHOCK ABSORBER NOT EXTENDED AFTER LIFTOFF)
Applicable to:
MAX SPEED...........................................................................................................................280/.67
L/G................................................................................................................................KEEP 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 2/76
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
L/G SHOCK ABSORBER FAULT
(SHOCK ABSORBER NOT EXTENDED AFTER LIFTOFF)
Applicable to:
MAX SPEED...........................................................................................................................280/.67
L/G................................................................................................................................KEEP 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 3/76
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
L/G SHOCK ABSORBER FAULT
(SHOCK ABSORBER NOT EXTENDED AFTER LIFTOFF)
Applicable to:
MAX SPEED...........................................................................................................................280/.67
L/G................................................................................................................................KEEP DOWN
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
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 10(28)
