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ENG
3, 4, 5, 7, 8
ENG THR LEVERS NOT SET
The levers position does not correspond to T.O
power mode.
SINGLE
CHIME
MASTER
CAUT NIL
NIL
1, 4, 5, 6,
7, 8, 10
ENG THRUST LOCKED
Thrust levers are not moved for 5 sfollowing
an involuntary 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 1(2) FUEL VALVE FAULT
HP fuel valve failed closed, or failed open.
ENG 1 (2) START FAULT
start fault due to :
• No light up, or
• ENG stall or overtemp, or
• Hung start, or
• EEC not capable to open start valve.
SINGLE
CHIME
MASTER
CAUT ENG
Associated
FAULT lt on
ENG panel
on pedestal
3, 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 22/28
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) START FAULT
• Start fault due to no N1 rotation.
1, 4, 5, 7,
8, 9, 10
ENG 1(2) START VALVE FAULT
Position disagree. 3, 4, 5, 7, 8
ENG 1 (2) THR LEVER DISAGREE
Disagree between both resolvers of a thrust
lever.
4, 5
ENG 1 (2) THR LEVER FAULT
Both resolvers on one thrust lever failed. NIL 5
ENG 1(2) OIL HI TEMP
Oil temp between 155 and 165 °C for more
than 15 min, or oil temp above 165 °C.
ENG 4, 5, 7, 8
ENG TYPE DISAGREE
Rating discrepancy between the two engines. NIL
NIL
3 to 10
ENG 1(2) OIL LO TEMP
oil temp low NIL 1, 4, 5, 6,
7, 8, 9, 10
ENG 1(2) FADEC FAULT
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
NIL
NIL
3, 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 23/28
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) 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
4, 5, 7, 8
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
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 4(121)
