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A330/A340 FLEET DSC-28-20 P 37/38
FCOM 19 AUG 10
Green : Normal aft ( ) or forward ( ) transfer (auto).
Amber : Abnormal aft ( ) or forward ( ) transfer.
(12) Jettison indication
No display : No jettison.
JETTISON (Green) : Jettison normally active.
JETTISON (Amber) : Abnormal jettison (valve abnormally open).
JETTISON (Amber) : Valve abnormally closed.
ECAM UPPER DISPLAY
Applicable to:
(1) FOB - Fuel on Board indication
‐ It is normally green.
‐ An amber half box appears around FOB, when the indicated quantity is not fully usable.
‐ When the fuel quantity indication is inaccurate, two amber lines appear across the last two
digits.
‐ Units may be indicated in kg or lbs.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
CONTROLS AND INDICATORS
A330/A340 FLEET DSC-28-20 P 38/38
FCOM 19 AUG 10
ECAM UPPER DISPLAY
Applicable to: ,
(1) FOB - Fuel on Board indication
‐ It is normally green.
‐ An amber half box appears around FOB, when the indicated quantity is not fully usable.
‐ When the fuel quantity indication is inaccurate, two amber lines appear across the last two
digits.
‐ Units may be indicated in kg or lbs.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FUEL
WARNINGS AND CAUTIONS
A330/A340 FLEET DSC-28-30 P 1/10
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
T TK XFR
FAULT lt
2 to 5,
7 to 10
PUMPS 1(2)(3)(4) + STBY LO PR
Dual pump failure in one collector cell.
PUMP and
STBY PUMP
FAULT lts
L(R) WING PUMPS LO PR
All pumps of the same wing low pressure.
1, 3, 4, 5,
7, 8, 10
L + R CTR PUMPS LO PR
associated
PUMP
FAULT lts 4, 5, 7, 8
ENG 1(2)(3)(4) LP VALVE FAULT
Valve disagree. 4, 5, 7, 8
ZFWZFCG DISAGREE
Disagree between the pilot entered values
and the FCMC values.
3 to 8
JETTISON NOT CLOSED
Valve disagree in open position.
SINGLE
CHIME
MASTER
CAUT
4, 5, 7, 8
JETTISON FAULT
One wing tank low level sensor is failed. NIL NIL 3, 4, 5, 7, 8, 9
L(R) WING TK LO LVL
Both level sensors of one inner tank have
been dry for more than 60 s (Fuel quantity
below 2 700 kg /5 952 lb).
L + R WING TK LO LVL
All of the four level sensors in the inner
tanks have been dry for more than 60 s
(Fuel quantity in each tank below 2 700 kg
/5 952 lb).
NIL
3, 4, 5, 7, 8, 9
WING TK OVERFLOW
One of the wing surge-tank overflow sensors
has been wet for more than 25 s.
SINGLE
CHIME
MASTER
CAUT
FUEL
CTR XFR +
PUMP FAULT lt 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 2/10
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
CTR TO INNER FAULT
In case an anomaly is detected during CTR to
INR XFR or an inlet valve of INR, OUTR tank
is failed open.
4, 5, 7, 8
OUTR TO INR FAULT OUTR
TK XFR lt
T TANK XFR FAULT TRIM TK
FAULT lt
APU LP VALVE FAULT
Valve disagree.
3, 4, 5, 7, 8
FCMC 1 + 2 FAULT
Loss of automatic XFR control.
TRIM LINE FAULT
Damage on the trim line, or in case of trim
tank isolation failure.
NIL
4, 5 , 8
FUEL LO TEMP
Inner fuel temp < -35 °C
Outer fuel temp < -40 °C
Trim fuel temp < -40 °C
OUTR and
TRIM TK
FAULT lt
L(R) INR TK HI TEMP
Inner fuel temp > 49 °C in flight
Inner fuel temp > 45 °C on ground
NIL
PUMP 1(2)(3)(4) LO PR
L(R) CTR PUMP LO PR
associated
PUMP FAULT lt
APU AFT PUMP FAULT
X FEED 1 (2)(3)(4) FAULT
Valve disagree.
FCMC 1(2) FAULT
NIL NIL
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 selected FWD, or
TRIM TANK FEED sel selected OPEN.
1, 2, 3, 9, 10
MAN XFR COMPLETED
Manual XFR selected ON, and center or outer
tank emptied.
　
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