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REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 FUEL MALFUNCTIONS
DUMP VALVE OPEN
DUMP VALVE OPEN
(1) Tank quantities ............................................................MONITOR
(2) FUEL, DUMP.......................................................AS REQUIRED
NOTE
Tail tank contents will deplete from full to empty in
approximately 30 minutes.
END
TAIL DUMP SOV
TAIL DUMP SOV
........SOV not in commanded position
FUEL DUMP selected:
Yes
(1) Tank quantities ....................................................MONITOR
Check that tail tank quantity is depleting.
If tail tank quantity is not depleting:
(2) Land at the nearest suitable airport.
− END −
No
(1) Tank quantities ............................................................MONITOR
Check that tail tank is not leaking.
END
Loss of Tail Tank Fuel Quantity Indication
........Tail tank fuel quantity indication dashed.
(1) TAIL TANK TRANSFER,
MANUAL OVRD............................................................MANUAL
(2) PRI and SEC TAIL TANK
TRANSFER............................................................................ ON
(3) Tank quantities ............................................................MONITOR
Check that aux tank quantity does not exceed 7,000 lb.
END
ABNORM 9-19
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 FUEL MALFUNCTIONS
Loss of Auxiliary Tank Fuel Quantity Indication
........Auxiliary tank fuel quantity indication dashed.
(1) TAIL TANK TRANSFER,
MANUAL OVRD............................................................MANUAL
(2) PRI or SEC TAIL TANK
TRANSFER............................................................................ ON
to start applicable pump.
(3) Tank quantities ............................................................MONITOR
Check that tail tank fuel quantity is depleting.
Tail tank quantity is not depleting:
Yes
(4) FUEL, DUMP............................................................. OPEN
NOTE
1. Fuel jettison must only be carried out with
flaps set to 0°.
2. Jettisoning of fuel in known lightning
conditions is prohibited.
3. Tail tank contents will deplete from full to
empty, in approximately 30 minutes.
− END −
No
(4) No further action required.
END
ABNORM 9-20
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 FUEL MALFUNCTIONS
Loss of Wing Tank Fuel Quantity Indication
........Wing tank fuel quantity indication dashed.
(1) Both ENG SPEED .................................................................. ON
(2) Airplane attitude .........................................STRAIGHT & LEVEL
(3) Engine fuel flow indications .............................................MATCH
(4) APU........................................................................ SHUTDOWN
if not required.
NOTE
APU operation will increase fuel burn from right wing tank,
by a rate of 100 to 300 lb/hr.
(5) Airplane trim ...................................................................ADJUST
(6) Missing fuel tank quantity ....................................... CALCULATE
using FMS fuel used page and displayed indications.
(7) Fuel distribution ...........................................................MONITOR
for imbalance.
Excessive imbalance exists (more than 25% of available trim
required):
Yes
Affected high tank:
(8) L (R) TO AUX XFLOW .............................................. OPEN
NOTE
Cross flow transfers fuel at a rate of approximately
15 lb/min or higher.
When excessive imbalance has been corrected:
(9) Affected L (R) TO AUX
XFLOW.................................................................... CLOSE
NOTE
Increase fuel reserves by 5%.
− END −
No
(8) No further action required.
END
Loss of Totalizer Fuel Quantity Indication
........Totalizer fuel quantity indication dashed.
(1) Tank quantities ............................................................MONITOR
Compare fuel burn to sum of tank quantities.
END
ABNORM 9-21
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 FUEL MALFUNCTIONS
Fuel Leak
........Fuel leak is evident, suspected or confirmed.
(1) Diversion may be required.
NOTE
If visibility permits, a visual check from the cabin may
enable identification of the leak source.
Leak is confirmed or suspected:
(2) Land immediately at the nearest suitable airport.
CAUTION
Do not delay landing while attempting
　
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