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1, 3, 4, 5,
7, 8, 10
TRIM TK PUMP LO PR
SINGLE
CHIME
MASTER
CAUT
NIL
NIL
3, 4, 5, 7, 8
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
WARNINGS AND CAUTIONS
A330/A340 FLEET DSC-28-30 P 3/10
FCOM 19 AUG 10
Continued from previous page
E/WD : FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNINGS
FLT PHASE
INHIB
NO WEIGHT/CG DATA
No data inserted on INIT B page at engine
start.
1, 3, 4, 5,
7, 8, 10
CELL NOT FULL
On one wing side, the forward collector cell’s
fuel quantity is less than 500 kg and the split
valve is closed ; or, on both wing sides, both
forward collector cells’ fuel quantities are less
than 600 kg, and the split valves are closed.
FUEL 1 to 5
7 to 10
WARNINGS AND CAUTIONS
Applicable to:
E/WD : FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNINGS
FLT PHASE
INHIB
EXCESS AFT CG CRC MASTER
WARN NIL 2 to 5,
7 to 10
L(R) WING PUMPS LO PR
All pumps of the same wing low pressure.
associated
PUMP
FAULT lts
1, 3, 4 5,
7, 8, 10
ENG 1(2) LP VALVE FAULT
Valve disagree. 4, 5, 7, 8
ZFWZFCG DISAGREE
Disagree between the pilot entered values
and the FCMC values.
3 to 8
L(R) WING TK LO LVL
Both level sensors of one inner tank have
been dry for more than 60 s.
Depending on the pitch attitude, the caution
may be triggered between 1 640 kg /3 616 lb,
and 2 700 kg /5 960 lb of fuel in either inner
tank.
SINGLE
CHIME
MASTER
CAUT
FUEL
NIL
3, 4, 5, 7, 8, 9
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
WARNINGS AND CAUTIONS
A330/A340 FLEET DSC-28-30 P 4/10
FCOM 19 AUG 10
Continued from previous page
E/WD : FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNINGS
FLT PHASE
INHIB
L + R WING TK LO LVL
All of the four level sensors in the inner tanks
have been dry for more than 60 s.
WING TK OVERFLOW
One of the wing surge-tank overflow sensors
has been wet for more than 25 s.
OUTR TO INR FAULT OUTR
TK XFR lt
TRIM TK PUMP LO PR NIL
T TANK XFR FAULT TRIM TK
FAULT lt
3, 4, 5, 7, 8
TRIM LINE FAULT
Trim tank isolation failure. 4, 5, 8
APU LP VALVE FAULT
Valve disagree. 3, 4, 5 7, 8
FCMC 1 + 2 FAULT
Loss of automatic XFR control.
NIL
4, 5 , 7, 8
FUEL LO TEMP
Inner fuel temp < -35 °C
Outer fuel temp < -40 °C
Trim fuel temp < -40 °C
OUTR TK XFR
lt and TRIM
TK FAULT lt
3, 4, 5, 7, 8
L(R) INR TK HI TEMP
Inner fuel temp > 49 °C in flight
Inner fuel temp > 45 °C on ground
3, 4, 5, 7, 8
ABNORM MAN FWD XFR
Trim TK pump failed and pitch attitude is
greater than 3.4 ° for more than 30 s and
T TANK MODE pb sw selected FWD or
TRIM TANK FEED sel selected OPEN.
1, 10
NO WEIGHT/CG DATA
No data inserted on INIT B page at engine
start.
NIL
NIL
1, 3, 4, 5,
7, 8, 10
L(R) PUMP 1(2) LO PR
L(R) STBY PUMP LO PR
associated
PUMP FAULT lt
APU AFT PUMP FAULT
WING X FEED FAULT
Valve disagree.
FCMC 1(2) FAULT
NIL NIL FUEL
NIL
1, 3, 4, 5, 7, 8
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
WARNINGS AND CAUTIONS
A330/A340 FLEET DSC-28-30 P 5/10
FCOM 19 AUG 10
WARNINGS AND CAUTIONS
Applicable to:
E/WD : FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNINGS
FLT PHASE
INHIB
EXCESS AFT CG CRC MASTER
WARN NIL 2 to 5,
7 to 10
L(R) WING PUMPS LO PR
All pumps of the same wing low pressure.
associated
PUMP
FAULT lts
1, 3, 4 5,
7, 8, 10
ENG 1(2) LP VALVE FAULT
Valve disagree. 4, 5, 7, 8
ZFWZFCG DISAGREE
Disagree between the pilot-entered values
and the FCMC values.
3 to 8
L(R) WING TK LO LVL
Both level sensors of one inner tank have
been dry for more than 60 s.
Depending on the pitch attitude, the caution
may be triggered between 1 640 kg /3 616 lb,
　
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