曝光台 注意防骗
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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.
ABN-80
13/32
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET ,
WINDSHEAR AHEAD
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 kts 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......................................................................................................................P
ERFORM
This includes the use of full backstick, if required.
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 TBD by AIRBUS.
WINDSHIELD/WINDOW ARCING
Affected WINDOW/WINDSHIELD ANTI ICE
C/B................................................................................... PULL
In case of electrical arcing, pull the circuit breaker of the affected window/windshield
heating system:
‐ ANTI ICE L WSHLD C/B AF10
‐ ANTI ICE/WINDOWS L C/B X14
‐ ANTI ICE R WSHLD C/B AF03
‐ ANTI ICE/WINDOWS R C/B W14
ABN-80
14/32
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET ,
WINDSHIELD/WINDOW CRACKED
MAX
FL....................................................................................................................................
.................230
CAB PRESS MODE
SEL.........................................................................................................................MAN
MAN V/S
CTL................................................................................................................................
AS RQRD
Set the cabin altitude, according to the table below.
ΔP = 5 PSI CABIN AFLLTITUDE 1000 31 05000 62 00000 82 03000
When starting the final descent:
CAB PRESS MODE
SEL................................................................................................................ AUTO
Note: If sufficient visibility is not granted for approach, 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............................................................................................................................FU
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空客320快速检查单QRH QUICK REFERENCE HAND BOOK5(113)
