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Disagree between both resolvers of a thrust lever. 4, 5, 8
ENG 1(2) OIL HI TEMP
Oil temp between 140 and 155 °C for more than
15 min, or oil temp above 155 °C.
ENG 1(2) FADEC FAULT
Both channels failed.
4, 5, 7, 8
ENG 1(2) LOW N1
No N1 rotation during start.
SINGLE
CHIME
MASTER
CAUT
ENG
4, 5, 6, 7,
8, 9, 10
ENG THRUST LOCKED
Thrust levers are not moved within 5 s, following
an unvoluntary disconnection of the A/THR (or
disconnection through the FCU pb).
SINGLE
CHIME
every 5 s
MASTER
CAUT
every 5 s
1, 2, 3, 4,
8, 9, 10
ENG FLEX TEMP NOT SET
Flex temp has not been entered on the MCDU.
1, 4, 5, 6,
7, 8, 10
ENG 1(2) FADEC HI TEMP 3, 4, 5, 7, 8
ENG TYPE DISAGREE
Rating discrepancy between the two engines.
NIL
NIL
3 to 10
ENG 1(2) THR LEVER FAULT
Both resolvers on one thrust lever have failed.
SINGLE
CHIME
MASTER
CAUT
NIL NIL 5
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
CONTROLS AND INDICATORS (CFM)
A318/A319/A320/A321 FLEET DSC-70-90 P 19/24
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) FAIL
Eng core speed below idle, with master sw ON and
fire pb not pushed.
ENG 1(2) SHUT DOWN
Eng master at off in phases 3 to 8, or eng fire pb
pushed in phases 1, 2, 9 and 10.
1, 10
ENG 1(2) REVERSE UNLOCKED
One or more reverser doors 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 doors
are stowed and locked with no deploy order.
4, 5, 8
ENG 1(2) COMPRESSOR VANE
Variable bleed valve sys or variable stator vane sys
fault.
4, 5, 7, 8
ENG 1(2) N1 or N2 or EGT OVER LIMIT
N1 above 104 %
N2 above 105.0 %
EGT above 950 °C
4, 8
ENG 1(2) IGN A + B FAULT
Both ignition circuits are failed.
3, 4, 5, 7, 8
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.
ENG 1(2) SENSOR FAULT
PS 3 or T 25 or T3 or N1 or N2 data unavailable on
both channels.
ENG 1(2) PROBES FAULT
T 12 or PO PT 2 data unavailable on both
channels.
4, 5, 7, 8
ENG 1(2) N1 (N2, EGT, FF) DISCREPANCY
Discrepancy between real and displayed values. 3, 4, 5, 8
ENG 1(2) BLEED STATUS FAULT
Bleed, X Bleed, pack, anti-ice valve position status
not received by FADEC active channel.
3, 4, 5, 7, 8
ENG 1(2) FUEL FILTER CLOG
ENG 1(2) OIL FILTER CLOG NIL NIL ENG 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 (CFM)
A318/A319/A320/A321 FLEET DSC-70-90 P 20/24
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 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, 7, 8
ENG 1(2) IGN A(B) FAULT
Ignition circuit A or B failed.
ENG 1(2) FADEC ALTERNATOR
Electrical auto supply loss of either FADEC
channel.
ENG COMPRESSOR VANE
Engine 1 and 2 VBV or VSV fault.
ENG 1(2) FUEL RETURN VALVE
Fuel return valve is failed in the not open, or not
closed position.
3, 4, 5, 7, 8
ENG 1(2) FADEC A(B) FAULT
One FADEC channel failed.
NIL
4, 5, 7, 8
ENG 1(2) EIU FAULT
Databus between EIU and ECU failed.
1, 3, 4, 5,
7, 8, 10
ENG 1(2) REVERSER FAULT
Loss of thrust reverser on one engine, due to
system components or input faults.
NIL NIL
3, 4, 5
ENG 1(2) REV ISOL FAULT SC CAUT 3 to 7
ENG 1(2) REV SWITCH FAULT
Failure of reverser permission switch.
3, 4, 5,
6, 7, 8
ENG REV SET Reverse thrust has been selected
in flight.
1 to 4
8 to 10
ENG 1(2) FUEL RETURN VALVE
Failure of the fuel return valve in the open or closed
position
3, 4, 5, 7, 8
ENG 1(2) ONE TLA FAULT
　
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