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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 28/76
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
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 29/76
FCOM 19 AUG 10
L/G LGCIU 2 FAULT
Applicable to: ,
MSN,,,,
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
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 30/76
FCOM 19 AUG 10
L/G LGCIU 1(2) FAULT
(TWO LGCIUS FAULTY)
Applicable to:
L2Normal landing gear control and position indications are lost. LDG GEAR lights on LDG GEAR
control panel remain available if LGCIU 1 is electrically supplied.
L1 L/G...............................................................................................................................GRVTY EXTN
L2 Refer to PRO-ABN-32 L/G GRAVITY EXTENSION.
L1GPWS..........................................................................................................................................OFF
L2 As LGCIU 1 is lost, GPWS 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 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 31/76
FCOM 19 AUG 10
L/G LGCIU 1(2) FAULT (Cont'd)
(TWO LGCIUS FAULTY)
L12
STATUS
L/G...........................................................................GRVTY EXTN
L/G CONTROL NOT AVAIL
ENG 1 APPR IDLE ONLY
ENG 2 APPR IDLE ONLY
CAT 1 ONLY
INOP SYS
REVERSER 1 + 2
AP 1 + 2 (1)
A/THR
N.W STEER
LGCIU 1
LGCIU 2
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) (except in LAND mode)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
LANDING GEAR
A318/A319/A320/A321 FLEET PRO-ABN-32 P 32/76
FCOM 19 AUG 10
L/G LGCIU 1(2) FAULT
(TWO LGCIUS FAULTY)
Applicable to:
L2Normal landing gear control and position indications are lost. LDG GEAR lights on LDG GEAR
control panel remain available if LGCIU 1 is electrically supplied.
L1 L/G...............................................................................................................................GRVTY EXTN
L2 Refer to PRO-ABN-32 L/G GRAVITY EXTENSION.
L1GPWS..........................................................................................................................................OFF
L2 As LGCIU 1 is lost, GPWS receives “L/G in up position” information even if the landing gear is
　
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