曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
NIL NIL
NIL NIL
3, 4, 5,
6, 7, 8
MEMO DISPLAY
IGNITION appears in green, when continuous ignition is activated on either engine.
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 21/24
FCOM 19 AUG 10
WARNINGS AND CAUTIONS
Applicable to:
E / WD : FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNING
FLT
PHASE
INHIB
ENG DUAL FAILURE
Associated
with GEN
FAULT lts
and PACK
FAULT lt
NIL
ENG 1(2) OIL LO PR
Oil low pressure triggered at 13 PSI by the oil
pressure switch.
CRC MASTER
WARN
1, 10
ENG STALL
NIL
ENG 1(2) HP FUEL VALVE
HP fuel valve failed closed.
3, 4, 5, 7, 8
ENG 1(2) START FAULT
Start fault due to :
• No light up, or
• Eng stall or overtemp (above 725 °C), or
• Starter time exceeded
• Thrust lever not at idle
• Low start air press
3, 4, 5,
6, 7, 8
ENG 1(2) START VALVE FAULT
Position disagree.
Associated
FAULT lt on
ENG panel
on pedestal
(exception
case of
starter time
exceeded)
3, 4, 5, 7, 8
ENG 1(2) THR LEVER DISAGREE
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.
SINGLE
CHIME
MASTER
CAUT
ENG
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 (CFM)
A318/A319/A320/A321 FLEET DSC-70-90 P 22/24
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) LOW N1
No N1 rotation during start.
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 THR LEVERS NOT SET
The levers position does not correspond to T.O
power mode.
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
3 to 10
ENG 1(2) THR LEVER FAULT
Both resolvers on one thrust lever have failed. 5
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.
SINGLE
CHIME
MASTER
CAUT
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 (CFM)
A318/A319/A320/A321 FLEET DSC-70-90 P 23/24
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) 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.
ENG 1(2) N1 (N2, EGT, FF) DISCREPANCY
Discrepancy between real and displayed values. 3, 4, 5, 8
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
A320机组操作手册FLIGHT CREW OPERATING MANUAL 4(115)
