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recovery of LGCIU1, BSCU1, SFCC1 and WHC1.
GPWS FLAP MODE.........................................................OFF
�� FOR L/G GRVTY EXTN:
MAX SPEED................................................................ 200 KT
L/G GRVTY EXTN........................................................DOWN
�� WHEN L/G DOWNLOCKED:
L/G ........................................................................ DOWN
INCREASE FUEL CONSUP
SLATS/FLAPS SLOW
See (1)
INOP SYS
FUEL AFT XFR
BSCU CH 1
L WSHLD HEAT
LGCIU 1
R FUEL PUMP 2
L WINDOW HEAT
(1)
NL2ote: If only one engine is recovered, the ECAM displays additional procedures due to the fact
that one engine remains inoperative.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 63/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) CTL SYS FAULT
Applicable to:
�� On ground:
THR LEVER 1(2)(3)(4)...........................................................................................................IDLE
ENG MASTER 1(2)(3)(4)........................................................................................................OFF
�� In flight:
L2 Depending on the type of failure, one of the following three messages is displayed:
L1 AVOID RAPID THR CHANGES
ENG (AFFECTED) SLOW RESPONSE
MAX N2: 95 %
�� In flight:
AVOID RAPID THR CHANGES
ENG (AFFECTED) SLOW RESPONSE, OR
MAX ENG 1 (2)(3)(4) N2: 95 %
ENG 1(2) CTL SYS FAULT
Applicable to: ,
�� On ground:
THR LEVER 1(2)................................................................................................................... IDLE
ENG MASTER 1(2).................................................................................................................OFF
�� In flight:
�� In case of a P30 failure:
AVOID RAPID THR CHANGES
�� In case of an FMV or FSV position failure:
ENG 1(2) SLOW RESPONSE.
�� In case of an N1, N2 SENSOR failure:
ENG 1(2) AT IDLE
�� In case of a BLEED VALVE failure:
THR LEVER 1(2).............................................................................................................IDLE
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 64/196
FCOM 19 AUG 10
ENG 1(2) CTL SYS FAULT (Cont'd)
STATUS
• IN CASE OF P 30 failure:
AVOID RAPID THR CHANGES
• IN CASE OF FMV or FSV position failure:
ENG 1(2) SLOW RESPONSE
• IN CASE OF N1, N2 SENSOR failure:
ENG 1(2) AT IDLE
ENG 1(2)(3)(4) BLEED STATUS FAULT
Applicable to:
L2 Bleed valve, pack valve, wing and engine anti-ice valve, crossbleed valve position status is not
received by the FADEC’s active channel.
L1 HI IDLE
L2 The FADEC increases minimum idle on the related engine as if bleed, pack, wing and engine anti–
ice valves were opened.
L1�� BEFORE T.O:
PACK 1+2.............................................................................................................................. OFF
WING ANTI ICE (IF ENG ANTI ICE ON)................................................................................ ON
BOTH PACKS AVAIL IN FLT (DISPLAYED ON GROUND)
STATUS
BOTH PACKS AVAIL IN FLT (on ground)
ENG (affected) HI IDLE
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 65/196
FCOM 19 AUG 10
ENG 1(2) BLEED STATUS FAULT
Applicable to: ,
L2 Bleed valves, pack valves, wing and engine anti-ice valves, crossbleed valve position status is not
received by the active FADEC channel.
L1 HI IDLE
L2 FADEC increases minimum idle on the related engine, as if bleed and pack valves were open.
L1�� BEFORE T.O:
PACK 1+2.............................................................................................................................. OFF
WING ANTI ICE (IF ENG ANTI ICE ON)................................................................................ ON
BOTH PACKS AVAIL IN FLT (DISPLAYED ON GROUND)
STATUS
BOTH PACKS AVAIL IN FLT (displayed on ground)
ENG (affected) HI IDLE
ENG 1(2) LP SHAFT PROT LOSS
Applicable to: ,
L2 LP shaft sensor is failed.
Crew awareness
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 66/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) FADEC FAULT OR OVHT
　
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