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Crew awareness.
L/G LGCIU 1 FAULT
Applicable to:
GPWS..........................................................................................................................................OFF
L2GPWS receives “L/G in up position” information even if the landing gear is down.
Setting the GPWS SYS pb-sw to OFF will prevent untimely warnings during the approach.
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 22/76
FCOM 19 AUG 10
L/G LGCIU 1 FAULT (Cont'd)
L12
STATUS
ENG 1 APPR IDLE ONLY
See (1)
INOP SYS
LGCIU 1
REVERSER 1
GPWS
Note: 1. The partial
spoiler
extension ��
at landing when
only one main
landing gear is
compressed is
not available.
The spoilers
extend normally
on ground when
wheel speed
greater than
72 kt.
2. Depending
on the LGCIU
failure, only
a part of the
above systems
may be lost.
(1)WL2 hen idle is selected on the ground with slats extended, only approach idle is available.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
LANDING GEAR
A318/A319/A320/A321 FLEET PRO-ABN-32 P 23/76
FCOM 19 AUG 10
L/G LGCIU 1 FAULT
Applicable to: ,
GPWS..........................................................................................................................................OFF
L2GPWS receives “L/G in up position” information even if the landing gear is down.
Setting the GPWS SYS pb-sw to OFF will prevent untimely warnings during the approach.
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 24/76
FCOM 19 AUG 10
L/G LGCIU 1 FAULT (Cont'd)
L12
STATUS
ENG 1 APPR IDLE ONLY
See (1)
INOP SYS
LGCIU 1
REVERSER 1
GPWS
Note: 1. The partial
spoiler
extension ��
at landing when
only one main
landing gear is
compressed is
not available.
The spoilers
extend normally
on ground when
wheel speed
greater than
72 kt.
2. Depending
on the LGCIU
failure, only
a part of the
above systems
may be lost.
(1)WL2 hen idle is selected on the ground with slats extended, only approach idle is available.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
LANDING GEAR
A318/A319/A320/A321 FLEET PRO-ABN-32 P 25/76
FCOM 19 AUG 10
L/G LGCIU 1 FAULT
Applicable to: ,
MSN,,,,
GPWS..........................................................................................................................................OFF
L2GPWS receives “L/G in up position” information even if the landing gear is down.
Setting the GPWS SYS pb-sw to OFF will prevent untimely warnings during the approach.
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 26/76
FCOM 19 AUG 10
L/G LGCIU 1 FAULT (Cont'd)
L12
STATUS
ENG 1 APPR IDLE ONLY
See (1)
INOP SYS
LGCIU 1
REVERSER 1
GPWS
Note: 1. The partial
spoiler
extension ��
at landing when
only one main
landing gear is
compressed is
not available.
The spoilers
extend normally
on ground when
wheel speed
greater than
72 kt.
2. Depending
on the LGCIU
failure, only
a part of the
above systems
may be lost.
(1)WL2 hen idle is selected on the ground with slats extended, only approach idle is available.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
LANDING GEAR
A318/A319/A320/A321 FLEET PRO-ABN-32 P 27/76
FCOM 19 AUG 10
L/G LGCIU 2 FAULT
Applicable to:
L2Crew awareness
L12
STATUS
ENG 2 APPR IDLE ONLY
See (1)
INOP SYS
LGCIU 2
REVERSER 2
Note: 1. The partial
spoiler
extension ��
at landing when
only one main
landing gear is
compressed is
not available.
The spoilers
extend normally
on ground when
wheel speed
greater than
　
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