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L2 Operation of engine and wing anti ice increase the stall margin but EGT increases
accordingly.
L1 THR LEVER (AFFECTED ENGINE)......................................................SLOWLY ADVANCE
If stall recurs:
THR LEVER (AFFECTED ENGINE)................................................................. REDUCE
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 78/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) STALL (Cont'd)
L2 Reduce thrust and operate below the stall threshold.
L1 If stall does not recur:
Continue engine operation.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 79/196
FCOM 19 AUG 10
ENG 1(2) STALL
Applicable to: ,
L2 A stall may be indicated by varying degrees of abnormal engine noises, accompanied by flame
from the engine exhaust and (possibly from engine inlet in severe cases), fluctuating parameters,
sluggish or no thrust lever response, high EGT and/or a rapid EGT rise when thrust lever is
advanced. Engine stalls must be reported for maintenance action.
L1 Stall is detected by the FADEC:
In flight:
FUEL ADJUSTED
L2 Fuel/Air ratio is automatically decreased until the stall disappears.
L1 THR LEVER 1(2).............................................................................................................IDLE
ENG 1(2) PARAMETERS...........................................................................................CHECK
IF ABNORMAL:
ENG MASTER 1(2)................................................................................................... OFF
On ground:
THR LEVERS 1 (2).........................................................................................................IDLE
ENG MASTER 1 (2).........................................................................................................OFF
If the crew detects a stall before the ECAM activation:
L2 The following non ECAM procedure may be applied:
L1 THR LEVER 1 (2)..................................................................................................................IDLE
ENG PARAMETERS 1 (2)................................................................................................ CHECK
If abnormal parameters:
ENG MASTER 1 (2).........................................................................................................OFF
L12
ASSOCIATED PROCEDURES
ENG 1(2) SHUT DOWN
L2 Refer to PRO-ABN-70-B After ENG 1(2) SHUT DOWN
Engine restart at crew discretion.
L1 If normal parameters:
ENG A ICE 1 (2)................................................................................................................ON
WING A ICE.......................................................................................................................ON
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 80/196
FCOM 19 AUG 10
ENG 1(2) STALL (Cont'd)
L2 Operation of engine and wing anti ice increase the stall margin but EGT increases
accordingly.
L1 THR LEVER 1 (2)..................................................................................SLOWLY ADVANCE
If stall does not recur:
Continue engine operation.
ENG 1(2) IGN SUPPLY FAULT
Applicable to: ,
L2 The emergency power supply of the ignition system is lost.
Crew awareness
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 81/196
FCOM 19 AUG 10
ENG 1(2) N1/N2/N3 OVERLIMIT
Applicable to: ,
Maximum pointer indications:
L2N1 above 99 %
N2 above 103.3 %
N3 above 100 %
L1 THR LEVER (AFFECTED ENGINE)...................................................................... BELOW LIMIT
L2Normal operation may be resumed and maintained until the next landing.
Report in the maintenance logbook.
L1 If THR LEVER at idle for more than 3 s:
ENG MASTER (AFFECTED ENGINE)...................................................................................OFF
L2 If conditions do not permit engine shutdown, land as soon as possible using the minimum thrust
required to sustain a safe flight.
L1
ASSOCIATED PROCEDURES
ENG 1(2) SHUT DOWN
Refer to PRO-ABN-70-B After ENG 1(2) SHUT DOWN
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 8(148)
