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L2 Operation of engine and wing anti ice will increase the stall margin, but EGT will increase
accordingly.
L1 THR LEVER (AFFECTED ENGINE)......................................................SLOWLY ADVANCE
If stall recurs:
THR LEVER (AFFECTED ENGINE)................................................................. REDUCE
L2 Reduce thrust and operate below the stall threshold.
L1 If stall does not recur:
L2Continue engine operation.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 19/194
FCOM 19 AUG 10
ENG 1(2) STALL
Applicable to: MSN
4566,,,
L2 A stall may be indicated by varying degrees of abnormal engine noises, accompanied by
flame from the engine exhaust (and possibly from the engine inlet in severe case), fluctuating
performance parameters, sluggish or no throttle response, high EGT and/or a rapid EGT rise when
thrust lever is advanced.
L1 On the ground:
THR LEVER (AFFECTED ENGINE)..................................................................................... IDLE
ENG MASTER (AFFECTED ENGINE)...................................................................................OFF
In flight:
THR LEVER (AFFECTED ENGINE)..................................................................................... IDLE
ENG PARAMETERS (AFFECTED ENGINE)....................................................................CHECK
IF ABNORMAL:
ENG MASTER (AFFECTED ENGINE)............................................................................ OFF
L12
ASSOCIATED PROCEDURES
ENG 1(2) SHUT DOWN
Refer to PRO-ABN-70-I After ENG 1(2) SHUT DOWN
L2 Engine restart at crew discretion.
L1 Normal:
ENG A. ICE (AFFECTED ENGINE).................................................................................. ON
WING A. ICE......................................................................................................................ON
L2 Operation of engine and wing anti ice will increase the stall margin, but EGT will increase
accordingly.
L1 THR LEVER (AFFECTED ENGINE)......................................................SLOWLY ADVANCE
If a stall recurs:
THR LEVER (AFFECTED ENGINE)................................................................. REDUCE
L2 Reduce thrust and operate below the stall threshold.
L1 If a stall does not recur:
L2Continue engine operation.
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 20/194
FCOM 19 AUG 10
ENG 1(2) STALL (Cont'd)
ENG 1(2) EPR OR N1 OR N2 OR EGT OR FF DISCREPANCY
Applicable to: MSN
4566,,,
L2 Discrepancy between displayed value on ECAM and real value. On ECAM upper display a CHK
message is displayed besides affected indication.
If both thrust levers are at the same position, cross check with the opposite parameter.
Crew awareness.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 21/194
FCOM 19 AUG 10
ENG 1(2) START VALVE FAULT
Applicable to:
START VALVE NOT CLOSED:
L2 Remove all bleed sources supplying the faulty start valve.
L1 APU BLEED (IF ENG 1 AFFECTED).................................................................................... OFF
X BLEED............................................................................................................................ SHUT
In flight:
ENG BLEED (AFFECTED SIDE).....................................................................................OFF
On the ground:
MAN START (IF MAN START PERFORMED)................................................................OFF
ENG MASTER (AFFECTED SIDE)................................................................................. OFF
L2 On the ground, consider application of “START VALVE MANUAL OPERATION” procedure.
L1 START VALVE NOT OPEN:
If opposite engine running:
X BLEED..........................................................................................................................ON
If APU AVAIL below FL 200:
APU BLEED....................................................................................................................... ON
If UNSUCCESSFUL:
MAN START (IF MAN START PERFORMED)................................................................OFF
ENG MASTER (AFFECTED) (IF AUTO START PERFORMED).....................................OFF
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 10(125)
