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ATC.................................................................................................................................
...................NOTIFY
A/THR.............................................................................................................................
.........................OFF
THRUST (conditions
permitting)...................................................................................................DECREASE
CREW OXYGEN
MASKS...............................................................................................................
ON/100 %
CABIN
CREW.............................................................................................................................
...... NOTIFY
ENG ANTI
ICE..................................................................................................................................
........ON
WING ANTI
ICE..................................................................................................................................
......ON
PACK
FLOW..............................................................................................................................
.................HI
APU.................................................................................................................................
....................START
ENGINE
PARAMETERS...............................................................................................................
..MONITOR
AIRSPEED
INDICATIONS..............................................................................................................
MONITOR
If airspeed is unreliable or lost, Refer to ABN-34-C UNRELIABLE SPEED
INDICATION/ADR CHECK
PROC - Memory Items If both engines flame out and speed indications are lost, Refer
to ABN-70-A ENG
ALL ENG FLAME OUT - FUEL REMAINING - ENGINE RELIGHT ATTEMPT to
get the required pitch
altitude for optimum relight speed.
In case of engine failure, switch off the wiring anti-ice before engine start.
Note: If sufficient visibility is not granted for approach due to windshield/window
damage, consider
AUTOLAND. If AUTOLAND is not available, consider opening the sliding window
on the PF's
side, after cabin depressurization.
�� To manually depressurize the cabin:
CAB PRESS MODE
SEL................................................................................................... MAN
MAN V/S
CTL..............................................................................................................FULL UP
Due to the increased noise level, pay particular attention to visual warnings.
ABN-80
12/32
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET
WINDSHEAR
A red flag “WINDSHEAR” is displayed on each PFD associated with an aural
synthetic voice
“WINDSHEAR” repeated three times.
If windshear is detected by pilot observation, apply the following recovery technique:
�� At takeoff
�� If before V1
The takeoff should be rejected only if significant airspeed variations occur below
indicated V1 and
the pilot decides that there is sufficient runway remaining to stop the airplane.
�� If after V1
THR
LEVERS.........................................................................................................................
TOGA
REACHING
VR....................................................................................................................ROTATE
SRS
ORDERS....................................................................................................................
FOLLOW
�� Airborne, initial climb or landing
THR LEVERS AT TOGA..........................................................................................
SET OR CONFIRM
AP (if
engaged)..........................................................................................................................
...KEEP
SRS
ORDERS.........................................................................................................................
FOLLOW
This includes the use of full back stick, if demanded.
Note: 1. If engaged, the autopilot disengages when α is greater than α prot.
2. If the FD bars are not available, use an initial pitch attitude up to 17.5 ° with full
backstick,
if necessary.If needed, to minimize the loss of height, increase this pitch attitude.
DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL OUT OF
SHEAR.
CLOSELY MONITOR FLIGHT PATH AND SPEED.
　
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