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both channels failed ENG 1, 3, 4, 5,
7, 8, 10
ENG 1(2) FADEC OVHT 3, 4, 5, 7, 8
ENG 1(2) FAIL
ENG core speed below idle with master sw ON
and fire pb not pushed.
NIL 1, 10
ENG 1(2) SHUT DOWN
ENG master sw at off in phases 3 to 8 or ENG
fire pb pushed in phases 1, 2, 9 and 10
NIL
ENG 1(2) REVERSE UNLOCKED
one reverser not locked in stowed position in
flight or on ground with no deploy order
8
ENG 1(2) REV PRESSURIZED
reverser system is pressurized while rev are
stowed and locked with no deploy order
NIL
4, 5, 8
ENG 1(2) REV SWITCH FAULT
failure of reverser permission switch ENG 3, 4, 5, 6, 7, 8
ENG 1(2) N1 or N2 or EGT OVER LIMIT
N1 above 100 %
N2 above 100 %
EGT above 650 °C
4, 8
ENG 1(2) IGN A + B FAULT
both ignition circuits are failed 3, 4, 5, 7, 8
ENG 1(2) COMPRESSOR VANE
low pressure compressor bleed valve sys
failure or stator vane angle disagree
ENG 1(2) EPR MODE FAULT
FADEC has reverted to back up control mode
(N1 mode)
4, 5
ENG 1(2) CTL VALVE FAULT
burn stag valve failure or HPTC or RAC system
failure
ENG 1(2) FUEL CTL FAULT
Fuel Metering Valve position disagree or,
failure of FMV command or of FMV position
feedback
NIL
NIL
4, 5, 7, 8
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
CONTROLS AND INDICATORS (IAE)
A318/A319/A320/A321 FLEET DSC-70-95 P 27/28
FCOM 19 AUG 10
Continued from previous page
E/WD : FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNING
FLT PHASE
INHIB
ENG 1(2) HOT FUEL
FADEC fuel overheat ENG 3, 4, 5, 7, 8
ENG 1(2) SENSOR FAULT
Engine monitoring parameters sensor failed 4, 5, 7, 8
ENG 1(2) EPR (N1, N2, EGT, FF)
DISCREPANCY
Discrepancy between real and displayed
values
3, 4, 5, 8
ENG 1(2) EGT EXCEEDED DURING AIR
START 3, 4, 5, 6, 7, 8
ENG 1(2) SYSTEM FAULT
failure of internal engine bleed or failure of
engine probe heat
NIL
3, 4, 5, 7, 8
ENG 1(2) EIU FAULT
Data bus between EIU and FADEC failed
1, 3, 4, 5,
7, 8, 10
ENG 1(2) FUEL FILTER CLOG NIL NIL
ENG
3, 4, 5, 7, 8
ENG 1(2) FUEL HEAT SYS
failure of fuel diverter valve or fuel or oil temp
sensors, or fuel return valve in open position.
3, 4, 5, 6, 7, 8
ENG COMPRESSOR VANE
ENG 1 and 2 bleed valve or stator vane angle
fault
NIL
ENG 1(2) OIL FILTER CLOG ENG
ENG 1(2) BEARING 4 OIL SYS
scavenge valve position disagree or high
pressure detection
3, 4, 5, 7, 8
ENG VIB SYS FAULT
failure of vibration detection system
3, 4, 5,
6, 7, 8, 9
ENG 1(2) OVSPD PROT FAULT
loss of overspeed protection 4, 5, 6, 7, 8
ENG 1(2) IGN A(B) FAULT
ignition circuit A or B failed 3, 4, 5, 7, 8
ENG 1(2) FADEC A(B) FAULT
one FADEC channel failed 3, 4, 5, 7, 8
ENG 1(2) FADEC ALTERNATOR
loss of electrical auto supply of FADEC
ENG 1(2) FADEC PLUG FAULT
ENG 1(2) A/C FADEC SUPPLY
3, 4, 5, 7, 8
ENG 1(2) REVERSER FAULT
loss of thrust reverser on one engine due to
system components, sensors or FADEC fault
NIL NIL
NIL
NIL
3, 4, 5
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
CONTROLS AND INDICATORS (IAE)
A318/A319/A320/A321 FLEET DSC-70-95 P 28/28
FCOM 19 AUG 10
Continued from previous page
E/WD : FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNING
FLT PHASE
INHIB
ENG 1(2) REV ISOL FAULT SINGLE
CHIME CAUTION 3 to 7
ENG REV SET
Reverse thrust has been selected in flight.
1 to 4
8 to 10
ENG 1(2) AIR EXCHANGR FAULT
failure of air/oil heat exchanger valve on
ground
ENG 1(2) ONE TLA FAULT
NIL NIL 3, 4, 5, 6, 7, 8
ENG 1(2) THR LEVER ABV IDLE
One thrust lever is at or above idle while the
other thrust lever is in the reverse detent.
SINGLE
CHIME
MASTER
CAUTION
1, 2, 3, 4,
5, 6, 7, 10
MEMO DISPLAY
IGNITION appears in green when the continuous ignition is activated on either engine.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
ELECTRICAL SUPPLY
A318/A319/A320/A321 FLEET DSC-70-98 P 1/2
FCOM 19 AUG 10
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 4(123)
