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A330/A340 FLEET DSC-70-92 P 12/16
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
N2 OVERLIMIT
N2 above 105 %
EGT OVERLIMIT
EGT above 915 °C (950 °C at TO
power)
SINGLE CHIME MASTER
CAUT
OIL LO PR
Oil pressure low CRC MASTER
WARN ENG 1, 10
MINOR FAULT
Engine short time limited dispatch NIL NIL 1 to 8
CTL SYS FAULT
VBV or VSV failure or loss of
parameters (PS 3, T25, T3, N1, N2)
or loss of FMV, VSV position or burn
staging valve failure or RAC system
failure.
4, 5, 7, 8
BLEED STATUS FAULT
Bleed status not received by active
FADEC channel
NIL
3, 4, 5, 7, 8
ENG FAIL
Eng core speed below idle with master
sw ON and fire pb is not pushed
ENG
ENG SHUT DOWN
Eng master at OFF in phases 3 to 8 or
eng fire pb pushed in phases 1, 2, 9 and
10
NIL
THR LEVERS NOT SET
Throttle set between MCLB and MCT
at TO Flex or derated takeoff mode not
selected by at least one FADEC
1, 4 to 8, 10
ENG T.O. THRUST DISAGREE
One FADEC at least selects a different
thrust takeoff mode on ground
NIL
1, 4 to 10
ENG STALL
Stall detected (not during start
sequence)
ENG 3, 4, 5, 7, 8
EIU FAULT
Data bus between EIU and FADEC
failed. Engine vib indication is lost.
SINGLE CHIME MASTER
CAUT
NIL 3, 4, 5, 8
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
A340 CONTROLS AND INDICATORS (CFM)
A330/A340 FLEET DSC-70-92 P 13/16
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
FADEC SYS FAULT
One NOGO failure affects one or both
channels.
Channel failure, or alternate fault, or
overspeed governor fault, or sensor
failure.
NIL 4, 5, 6, 7, 8
FADEC FAULT
Data bus between FADEC and ECAM
failed.
4, 5, 7, 8
FADEC OVHT
MASTER
CAUT
FUEL FILTER CLOG NIL NIL
ENG
IGN A + B FAULT
Both ignition circuits are failed. SINGLE CHIME MASTER
CAUT
IGN A(B) FAULT
Ignition circuit A or B is failed. NIL NIL
3, 4, 5, 7, 8
TYPE DISAGREE
Disagree between pin programming on
the FADEC and on the FWC (engine
rate).
3 to 10
REV FAULT
Loss of thrust reverser on one engine. 3, 4, 5
REV ISOL FAULT 3 to 8
REV PRESSURIZED
Reverser system is pressurized, while
rev doors are stowed and locked, with
no deploy order (on ground).
1, 8
REV UNLOCKED
One reverser door not the locked in the
stowed position, with no deploy order.
8
REV SET
Reverse thrust has been selected by
the crew in flight.
SINGLE CHIME MASTER
CAUT
1 to 4, 8 to 10
REV INHIBITED
Reverser is inhibited by maintenance
action.
NIL NIL 3 to 8
THR LEVER FAULT
Both resolvers on one thrust lever are
failed.
8
THR LEVER DISAGREE
Disagree between both resolvers of a
thrust lever.
SINGLE CHIME MASTER
CAUT
NIL
4, 5, 8
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
A340 CONTROLS AND INDICATORS (CFM)
A330/A340 FLEET DSC-70-92 P 14/16
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 < -10 °C (on ground
before takeoff).
3 to 9
OIL HI TEMP
Engine oil temp between 140 °C and
155 °C for more than 15 min, or above
155 °C.
ENG
4, 5, 7, 8
OIL FILTER CLOG
It can only be triggered when N1 is
less than 75 %and altitude is below
20 000 ft.
3, 4, 5, 7, 8
THRUST LOCKED
Thrust is frozen on one or more
engines, after an involuntary A/THR
disconnection.
This caution is recalled every 5 s, until
thrust levers are moved.
NIL
2, 3, 4, 8, 9
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
　
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