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Increase thrust to a setting compatible with the flight phase. VIB level will come back to normal
after ice shed despite a slight increase during acceleration.
Resume normal operation.
Note: If possible, shut the engine down after landing for taxiing, when vibrations above the
advisory level have been experienced during the flight.
ENG 1(2) FADEC PLUG FAULT
Applicable to: MSN
4566,,,
L2Maintenance action is due.
Crew awareness.
ENG 1(2) AIRCRAFT FADEC SUPPLY
Applicable to: MSN
4566,,,
L2 On ground, loss of aircraft 28 V supply of either EEC channel, or, in flight, loss of aircraft 28 V
supply of:
‐ Both EEC channels, or
‐ One EEC channel without switching to the other channel.
Crew awareness.
L12
STATUS
The ECAM only displays these inoperative systems, if there is:
‐ A loss of aircraft 28 V supply of both EEC channels, or
A loss of aircraft 28 ‐ V supply of one EEC channel without
switching to the other channel.
INOP SYS
REVERSER 1(2)
ENG 1(2) START
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 180/194
FCOM 19 AUG 10
ENG 1(2) BEARING 4 OIL SYS
Applicable to: MSN
4566,,,
L2 One of the two following messages is displayed:
L1 SCAVENGE VALVE FAULT
L2N° 4 bearing scavenge valve stuck open.
L1 HI PRESS
L2N° 4 bearing carbon seal is failed or due to scavenge valve stuck closed or due to a clogged
scavenge valve restrictor.
Maintenance action is due.
ENG 1(2) BLEED STATUS FAULT
(ON GROUND)
Applicable to:
L2 Status of bleed valves, pack valves, wing and engine anti ice valves, X bleed valve is not received
by the FADEC active channel.
L12 HI GND IDLE
FADEC increases minimum idle as if valves were opened.
L1�� If ENG ANTI ICE on:
ENG MODE SEL..................................................................................................................... IGN
L2When ENG anti ice is on, there is no automatic selection of continuous relight since FADEC
does not know position of engine anti ice valves position.
L1�� BEFORE T.O.:
PACK (ASSOCIATED SIDE)..................................................................................................OFF
L2 Associated pack must be closed to reduce risk of excessive EGT.
STATUS
ENG 1(2) HI GND IDLE
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 181/194
FCOM 19 AUG 10
ENG 1(2) BLEED STATUS FAULT
(ON GROUND)
Applicable to: ,
L2 Status of bleed valves, pack valves, wing and engine anti ice valves, X bleed valve is not received
by the FADEC active channel.
L12 HI GND IDLE
FADEC increases minimum idle as if valves were opened.
L1�� If ENG ANTI ICE on:
ENG MODE SEL..................................................................................................................... IGN
L2When ENG anti ice is on, there is no automatic selection of continuous relight since FADEC
does not know position of engine anti ice valves position.
L1�� BEFORE T.O.:
PACK (ASSOCIATED SIDE)..................................................................................................OFF
L2 Associated pack must be closed to reduce risk of excessive EGT.
STATUS
ENG 1(2) HI GND IDLE
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 182/194
FCOM 19 AUG 10
ENG 1(2) BLEED STATUS FAULT
(ON GROUND)
Applicable to: ,
MSN
L2 Status of bleed valves, pack valves, wing and engine anti ice valves, X bleed valve is not received
by the FADEC active channel.
L12 HI GND IDLE
FADEC increases minimum idle as if valves were opened.
L1�� If ENG ANTI ICE on:
ENG MODE SEL..................................................................................................................... IGN
L2When ENG anti ice is on, there is no automatic selection of continuous relight since FADEC
does not know position of engine anti ice valves position.
L1�� BEFORE T.O.:
PACK (ASSOCIATED SIDE)..................................................................................................OFF
L2 Associated pack must be closed to reduce risk of excessive EGT.
STATUS
ENG 1(2) HI GND IDLE
ENG 1(2) BLEED STATUS FAULT
(IN FLIGHT)
Applicable to:
L2 Status of bleed valves, pack valves, wing and engine anti ice valves, X bleed valves is not received
　
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