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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.
RECOVER SMOOTHLY TO NORMAL CLIMB OUT OF SHEAR.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A318/A319/A320/A321 FLEET PRO-ABN-80 P 180/182
FCOM 19 AUG 10
WINDSHEAR AHEAD
Applicable to: ALL
The “W/S AHEAD” message is displayed on each PFD. The color of the message depends on the
severity and location of the windshear
Note: When a predictive windshear alert (“WINDSHEAR AHEAD”) is triggered, if the flight crew
makes a positive verification that no hazard exists, then the alert may be disregarded, as
long as:
There are no other signs of possible ‐ windshear conditions, and
‐ The reactive windshear system is operational.
Known cases of spurious predictive windshear alerts have been reported at some airports,
during either takeoff or landing, due to the specific obstacle environment.
However, always rely on any reactive windshear (“WINDSHEAR”).
W/S AHEAD RED
�� Takeoff
Associated with an aural synthetic voice “WINDSHEAR AHEAD, WINDSHEAR AHEAD”.
�� Before takeoff:
Delay takeoff, or select the most favorable runway.
�� During the takeoff run:
Reject takeoff.
Note: Predictive windshear alerts are inhibited above 100 kt until 50 ft.
�� When airborne:
THR LEVERS...........................................................................................................TOGA
As usual, the slat/flap configuration can be changed, provided the windshear is not
entered.
SRS ORDERS.................................................................................................... FOLLOW
Note: If engaged, the autopilot disengages when α is greater than α prot.
�� Landing:
Associated with an aural synthetic voice “GO AROUND, WINDSHEAR AHEAD”.
GO-AROUND..........................................................................................................PERFORM
This includes the use of full backstick, if required.
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A318/A319/A320/A321 FLEET PRO-ABN-80 P 181/182
FCOM 19 AUG 10
WINDSHEAR AHEAD (Cont'd)
Note: 1. If engaged, the autopilot disengages when α is greater than α prot.
2. If the FD is not available, use a pitch initial attitude up to 17.5 °. If necessary to
minimize the loss of height, increase this pitch attitude.
W/S AHEAD AMBER
Apply precautionary measures, as indicated in the SUPPLEMENTARY TECHNIQUES Refer to
PRO-SUP-91-10 GENERAL.
TAILSTRIKE
Applicable to: ALL
In the event of a tailstrike, apply the following procedure:
LAND ASAP
MAX FL.............................................................................................................................100 or MSA
500 ft/min should be targeted for the climb, to minimize pressure changes, and for passenger and
crew comfort. Similarly, the rate of descent must be limited to about 1 000 ft/min, except for the final
approach that must be performed normally.
Notify the ATC of the aircraft’s rate of climb.
RAM AIR....................................................................................................................................... ON
　
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