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NIL
THR LEVERS NOT SET
Throttle set between CLB and MCT at T.O.
Flex take off mode not selected by at least one
FADEC.
ENG T.O. THRUST DISAGREE
One FADEC, at least, selects a different thrust at
T.O.
SINGLE
CHIMIE
MASTER
CAUT
NIL
NIL
1, 4, 5, 6,
7, 8, 10
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
A330 CONTROLS AND INDICATORS (RR, PW)
A330/A340 FLEET DSC-70-91 P 17/18
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 STALL
Stall detected. ENG 4, 5, 7, 8
EIU FAULT
Data bus between EIU and FADEC failed. Engine
vib indication is lost.
3, 4, 5, 8
FADEC SYS FAULT
One NOGO failure affects one or both channels.
Channel failure, or alternate fault, or overspeed
governor fault, or sensor failure.
NIL
NIL
4, 5, 6, 7, 8
FADEC FAULT
Data bus between FADEC and ECAM failed 4 to 8
FADEC OVHT
FUEL FILTER CLOG
ENG
IGN A+ B FAULT
Both ignition circuits are failed.
MASTER
CAUT
IGN A(B) FAULT
Ignition circuit A or B failed. NIL NIL
3, 4, 5, 7, 8
TYPE DISAGREE
Disagree between pin programming on FADEC
and on FWC (engine rate).
3 to 10
REV FAULT
Loss of thrust reverser on one engine. 3, 4, 5
REV SET
Reverse thrust has been selected in flight
1 to 4,
8 to 10
REV PRESSURIZED
Reverser system is pressurized, while rev cowls
are stowed and locked, with no deploy order (on
ground).
1, 8
REV UNLOCKED
One reverser cowl not locked in stowed position,
with no deploy order.
SINGLE
CHIMIE
MASTER
CAUT
8
REV INHIBITED
Reverser is inhibited by maintenance action. NIL NIL 3 to 8
THR LEVER FAULT
Both resolvers on one thrust lever failed. 8
THR LEVER DISAGREE
Disagree between both resolvers of a thrust lever.
SINGLE
CHIMIE
MASTER
CAUT
NIL
4, 5, 8
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
A330 CONTROLS AND INDICATORS (RR, PW)
A330/A340 FLEET DSC-70-91 P 18/18
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
OIL LO TEMP
Engine oil temp < 50 °C
(on ground before takeoff)
3 to 9
OIL HI TEMP
Engine oil temp between 163 °C and 177 °C
more than 20 min or above 177 °C.
ENG
4, 5, 7, 8
OIL FILTER CLOG 3, 4, 5, 7, 8
THRUST LOCKED
The thrust is frozen on one or both engines,
after an involuntary A/THR disconnection. This
caution is recalled every 5 s, until thrust levers are
moved.
2, 3, 4, 8, 9
ENG THRUST LOSS
The actual bleed configuration is not in
accordance with the bleed configuration
requested by the crew.
NIL
1, 4 to 10
START VALVE FAULT
The start valve is either stuck closed, or stuck
open, or no starter air pressure is available (valve
disagree).
START FAULT
Start fault due to :
• Starter time exceeded, or
• EGT overlimit, or
• No light up, or
• Low N1, or
• Starter failure, or
• Hung start, or
• THR levers not at idle.
HP FUEL VALVE
Fuel valve failed closed, or open.
ENG
Associated
FAULT lt on
ENG panel
on pedestal
(except in case
of starter time
exceeded)
3, 4, 5, 7, 8
REV MINOR FAULT
At least a failure needing repair before 150 h , is
detected by the FADEC.
INCREASED FUEL BURN
Fuel burn deviates from more than 1 % of the
calculated valve.
NIL NIL NIL NIL 3 to 8
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
A340 CONTROLS AND INDICATORS (CFM)
A330/A340 FLEET DSC-70-92 P 1/16
FCOM 19 AUG 10
PEDESTAL
Applicable to:
(1) Thrust levers
Refer to DSC-70-35-30 THRUST LEVERS
(2) Reverse control levers
When the thrust levers are not at idle, the reverse control levers are mechanically locked in the
stowed position.
When the thrust levers are at idle, thrust reverser operation can be controlled by pulling
backward the reverse control levers.
　
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