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− END −
No
(1) Engine instruments.......................................CONFIRM ENGINE
FAILURE
using N1, fuel flow, ITT & N2
Engine failure is confirmed:
Yes
(2) In-Flight Engine
Failure/Shutdown..........................................ACCOMPLISH
(See Page ABNORM 1–2)
− END −
No
(2) No further action required.
END
ABNORM 9-3
REV 74, Nov 07/08
QUICK REFERENCE HANDBOOK
PSP 604-15 FUEL MALFUNCTIONS
L (R) FUEL FILTER
L FUEL FILTER or R FUEL FILTER
........Impending fuel filter bypass
(1) Affected engine ...........................................................MONITOR
engine indication and performance.
END
L (R) FUEL LO PRESS
L FUEL LO PRESS or R FUEL LO PRESS
Associated L (R) MAIN EJECTOR FAIL status message and/or
L (R) SCAV EJECTOR caution message on:
Yes
(1) Affected engine fuel flow
indication .................................................................CHECK
(2) Affected wing tank fuel
quantity ....................................................................CHECK
Affected fuel tank quantity is depleting abnormally:
Yes
(3) Affected BOOST PUMP ........................................OFF
Fuel quantity continues to deplete abnormally:
Yes
(4) Fuel Leak Procedure .................... ACCOMPLISH
(See Page ABNORM 9–22)
− END −
No
(1) Affected engine instruments........................................MONITOR
END
ABNORM 9-4
REV 74, Nov 07/08
QUICK REFERENCE HANDBOOK
PSP 604-15 FUEL MALFUNCTIONS
L (R) FUEL LO TEMP
L FUEL LO TEMP or R FUEL LO TEMP
........Fuel temperature readout indicates caution range (amber)
On ground:
Yes
(1) Do not attempt take-off.
− END −
No
In flight:
(1) Affected engine instruments.............................................Monitor
NOTE
The engine fuel system will not be heated. L (R) FUEL
FILTER caution message may come on, indicating an
impending bypass.
END
BULK FUEL TEMP
BULK FUEL TEMP
On ground:
Yes
(1) APU/Engines .............................................DO NOT START
if fuel temperature is below the specified limits for
fuel type.
(2) Airplane ............................................... DO NOT TAKE OFF
if anticipated air mass temperature is below the
specified limit for fuel type.
− END −
No
During flight:
(1) Airplane ............................................... DESCEND OR DEVIATE
to warmer air mass, and/or
(2) Airspeed .................................................................... INCREASE
as required.
END
ABNORM 9-5
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 FUEL MALFUNCTIONS
L (R) FUEL PUMP
L FUEL PUMP
or
R FUEL PUMP
(1) Affected BOOST PUMP ....................................................... OFF
then ON.
L (R) FUEL PUMP caution message and L (R) BOOST PUMP
INOP light persists:
Yes
(2) Affected engine instruments ................................MONITOR
− END −
No
(2) No further action required.
END
ABNORM 9-6
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 FUEL MALFUNCTIONS
Motive Flow Failure
L SCAV EJECTOR or R SCAV EJECTOR
(1) Both BOOST PUMPs ................................................CHECK ON
Engine thrust is inadequate:
Yes
(2) Unaffected engine ..................................ADJUST THRUST
to maintain flight path.
No
(2) Tank quantities ............................................................MONITOR
Total fuel quantity is depleting abnormally:
Yes
(3) Affected BOOST PUMP ............................................... OFF
Fuel quantity continues to deplete abnormally:
Yes
(4) Fuel Leak Procedure ............................ ACCOMPLISH
(See Page ABNORM 9–22)
− END −
No
(3) No further action required.
END
ABNORM 9-7
REV 74, Nov 07/08
QUICK REFERENCE HANDBOOK
PSP 604-15 FUEL MALFUNCTIONS
L (R) SCAV EJECTOR
L SCAV EJECTOR or R SCAV EJECTOR
Fuel quantity in either wing tank is less than 230 kg (500 lb):
Yes
(1) Airplane attitude............................................... 5° NOSE UP
maximum.
(2) Tank quantities ....................................................MONITOR
Total fuel quantity is depleting abnormally:
Yes
(3) Affected BOOST PUMP ........................................OFF
Fuel quantity continues to deplete abnormally:
　
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