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the EVAC
COMMAND pushbutton �� .
�� If Evacuation not required:
CABIN CREW and PASSENGERS
(PA)................................................................................. NOTIFY
Ensure that all the landing gears are secured before initiating the disembarkation
(before switching
OFF the seat belts signs).
ABN-32
1/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , MSN,,,
LOSS OF BRAKING
�� IF AUTOBRAKE IS SELECTED:
BRAKE
PEDALS.........................................................................................................................
PRESS
�� IF NO BRAKING AVAILABLE:
REV.................................................................................................................................
................. MAX
BRAKE
PEDALS.......................................................................................................................R
ELEASE
A/SKID & N/W
STRG.........................................................................................................................OF
F
BRAKE
PEDALS.........................................................................................................................
PRESS
MAX BRK
PR.............................................................................................................................
1000 PSI
�� If STILL NO BRAKING:
PARKING BRAKE...................................................... SHORT AND SUCCESSIVE
APPLICATIONS
RESIDUAL BRAKING PROC
�� IN FLIGHT:
BRAKE PEDALS..............................................................................................APPLY
SEVERAL TIMES
Press the brake pedals several times. This could zero a residual pressure on the
alternate system.
�� IF RESIDUAL PRESSURE REMAINS:
A/SKID & N/W STRG
selector............................................................................................KEEP ON
�� IF AUTOBRAKE IS AVAILABLE:
FOR
LANDING..................................................................................................AUTO/BRK
MED
Using MED mode gives immediate priority to normal braking upon landing gear
touchdown,
which cancels residual alternate pressure.
�� IF AUTOBRAKE IS NOT AVAILABLE:
JUST AFTER TOUCHDOWN..........................................................................APPLY
BRAKING
Pressing the brake pedals gives immediate priority to normal braking, which cancels
residual
alternate pressure.
Beware of possible braking asymmetry after touchdown, which can be controlled by
using the
pedals.
Note: In case of taxi with deflated or damaged tires, Refer to FCOM/LIM-32 TAXI
WITH DEFLATED
TIRES.
ABN-32
2/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , MSN,,,
L/G GRAVITY EXTENSION
GRAVITY GEAR EXTN
handcrank.....................................................................................PULL AND TURN
Rotate the handle clockwise 3 turns until reaching the mechanical stop, even if
resistance is felt.
L/G
lever.................................................................................................................................
.............DOWN
GEAR DOWN indications (if
available)............................................................................................... CHECK
Note: 1. Depending on aircraft speed, the display may show the landing gear doors in
the amber transit
position.
2. In the event of gravity extension, caused by the failure of both LGCIUs, landing
gear position
indication on ECAM are lost. LDG GEAR light on LDG GEAR control panel remain
available, if
LGCIU 1 is electrically supplied.
3. The L/G LGCIU 2 FAULT or BRAKES SYS 1(2) FAULT cautions may be
spuriously triggered
after a gravity extension.
4. If the three green downlock arrows are not on, it is possible that the handcrank is
not at the
mechanical stop. Check that the handcrank is firmly against the mechanical stop.
�� If successful:
Do not reset the free-fall system. This will avoid such undesirable effects as further
loss of fluid, in the
event of a leak, or possible landing gear unlocking, in the event of a gear selector
valve jamming in the
UP position.
Note: The free-fall system may be reset in flights used for training. If the green
hydraulic system is
available, resetting the free-fall system allows the landing gear doors to be closed.
　
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