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APPROACH
GPWS
SYS..................................................................................................................................
....... OFF
L/G
lever............................................................................................................................C
HECK DOWN
GRVTY GEAR EXTN handcrank......................................................................TURN
BACK TO NORMAL
AUTOBRAKE.................................................................................................................
...... DO NOT ARM
EMER EXIT
LT.....................................................................................................................................
ON
CABIN
REPORT...........................................................................................................................
OBTAIN
A/SKID & N/W
STRG...........................................................................................................................OF
F
MAX BRAKE
PR........................................................................................................................... 1000
PSI
�� If one or both MAIN L/G abnormal:
GROUND
SPOILERS.....................................................................................................DO NOT
ARM
BEFORE LANDING
RAM
AIR..................................................................................................................................
............. ON
BRACE FOR
IMPACT.....................................................................................................................OR
DER
�� If the external light condition is poor at landing:
DOME
LT....................................................................................................................................
.. DIM
FLARE, TOUCH DOWN AND ROLL OUT
Engines should be shut down sufficiently early to ensure fuel is shut off before the
nacelles impact, but
sufficiently late to ensure adequate hydraulic supplies for the flight controls.
Engine pumps continue to supply adequate hydraulic pressure for 30 s after engine
shutdown.
REVERSE........................................................................................................................
.....DO NOT USE
�� If NOSE L/G abnormal:
NOSE............................................................................................................................
MAINTAIN UP
After touchdown, keep the nose off the runway by use of the elevator. Then, lower the
nose on to
the runway before elevator control is lost.
BRAKES (compatible with elevator
efficiency).......................................................................... APPLY
ENG
MASTERS.......................................................................................................................
......OFF
Shutdown the engines before nose impact.
To be continued on next page
ABN-32
4/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , ,
LDG WITH ABNORMAL L/G (Cont'd)
�� If one MAIN L/G abnormal:
ENG
MASTERS.......................................................................................................................
......OFF
At touchdown, shut down both engines.
FAILURE SIDE
WING....................................................................................................MAINTAIN UP
Use roll control, as necessary, to maintain the unsupported wing up as long as
possible.
DIRECTIONAL
CONTROL...................................................................................................
MAINTAIN
Use rudder and brakes (maximum 1 000 PSI) to maintain the runway axis as long as
possible.
�� If both MAIN L/G abnormal:
ENG
MASTERS.......................................................................................................................
......OFF
Shut down the engines in the flare, before touchdown.
PITCH ATTITUDE (at touchdown).......................................................................NOT
LESS THAN 6°
WHEN A/C STOPPED
ENG (all) and APU FIRE
pushbutton................................................................................................ PUSH
Pressing the ENG FIRE pb shuts off the related hydraulic pressure within a short
time.
ENG (all) and APU
AGENT..............................................................................................................DISCH
　
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