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CABIN CREW..........................................................................................................................NOTIFY
PASSENGER OXYGEN...................................................................................................... AS RQRD
Depending on contamination.
ENG ANTI ICE..............................................................................................................................ON
WING ANTI ICE............................................................................................................................ON
ECON FLOW...............................................................................................................................OFF
APU.........................................................................................................................................START
If possible, start the APU and have it ready for an assisted engine relight in the event of an engine
flame-out. (Refer to LIM-49-10-A GENERAL - APU STARTER).
ENGINE PARAMETERS..................................................................................................... MONITOR
Monitor particularly EGT. If EGT exceeds limits, it may become necessary to consider a
precautionary engine shutdown and engine restart in flight.
AIRSPEED INDICATIONS...................................................................................................MONITOR
If airspeed is unreliable or lost, Refer to PRO-ABN-34 UNRELIABLE SPEED INDICATION/ADR
CHECK PROC - GENERAL.
If both engines flame out and speed indications are lost, Refer to PRO-ABN-70-S ENG DUAL
FAILURE to get the required pitch attitude for the optimum relight speed. In case of engine failure,
switch off the wing anti ice before engine restart.
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 66/182
FCOM 19 AUG 10
VOLCANIC ASH ENCOUNTER (Cont'd)
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.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
MISCELLANEOUS
A318/A319/A320/A321 FLEET PRO-ABN-80 P 67/182
FCOM 19 AUG 10
COCKPIT WINDSHIELD/WINDOW CRACKED
Applicable to: ALL
In case of a one ply crack, whichever one it may be, the windshield/windows are still able to sustain
the maximum differential pressure. However, because the pilot is unable to accurately determine
how many plies have failed, the differential pressure must be reduced to 5 PSI by applying the
following procedure:
MAX FL.........................................................................................................................................230
The maximum flight level is restricted to FL 230 to obtain ΔO4ORH+vhsgntsqdrtkshmfhmm
excessive cabin altitude and corresponding EXCESS CAB ALT warning.
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CAB PRESS MODE SEL.............................................................................................................MAN
MAN V/S CTL...................................................................................................................... AS RQRD
Set the cabin altitude, according to the table below:
ΔO< FL 100 150 200 230
5 PSI CABIN ALTITUDE 0 3 000 6 000 8 000
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.................................................................................................. FULL UP
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 11(50)
