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switch/light .......................................................Press out then press in.
Check the following:
• L (R) BOOST PUMP INOP
light out.
• L (R) FUEL PUMP caution
message out.
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
ABNORMAL PROCEDURES
Fuel
Vol. 1 05−12−6
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. FUEL (CONT'D)
I. Motive Flow Failure
Indication: L (R) SCAV EJECTOR caution message accompanied by L (R) MAIN
EJECTOR FAIL status message.
(1) FUEL, L and R BOOST PUMP
switch/lights ..........................................................Check pressed in.
Check the following:
• L and R BOOST PUMP ON
lights on,
• L and R FUEL PUMP ON
advisory messages on, and
• L and R FUEL PUMP caution
messages out.
Engine thrust is inadequate:
Yes
(2) Unaffected engine ........................................Adjust thrust to maintain flight path.
No
(2) Fuel quantity indicators ......................................Monitor for abnormal fuel depletion.
Total fuel quantity is depleting abnormally:
Yes
(3) Affected Fuel, BOOST
PUMP switch/light....................................Press out to disable boost pump.
Check the following:
• L (R) BOOST PUMP ON
light out.
• L (R) FUEL PUMP ON
advisory message out.
• L (R) BOOST PUMP INOP
light on, and
• L (R) FUEL PUMP caution
message on.
Fuel quantity continues to deplete abnormally:
Yes
(4) Fuel Leak Procedure ....................Accomplish Refer to Fuel Leak Procedure
in this section.
− END −
No
(3) No further action required.
END
ABNORMAL PROCEDURES
Fuel
Vol. 1 05−12−7
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
1. FUEL (CONT'D)
J. Scavenge Ejector Failure
Indication: L (R) SCAV EJECTOR caution message on.
Fuel quantity in either wing tank is less than 230 kg (500 lb):
Yes
(1) Airplane attitude............................... Not more than
5° nose up
(2) Fuel quantity indicators...............................Monitor for abnormal fuel depletion.
Total fuel quantity is depleting abnormally:
Yes
(3) Affected Fuel, BOOST
PUMP switch/light............................Press out to disable boost pump.
Check the following:
• L (R) BOOST PUMP ON
light out.
• L (R) FUEL PUMP ON
advisory message out.
• L (R) BOOST PUMP INOP
light on, and
• L (R) FUEL PUMP caution
message on.
Fuel quantity continues to deplete abnormally:
Yes
(4) Fuel Leak Procedure ............Accomplish Refer to Fuel Leak
Procedure in this section.
− END −
No
(1) No further action required.
END
ABNORMAL PROCEDURES
Fuel
Vol. 1 05−12−8
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
1. FUEL (CONT'D)
K. Primary Tail Tank Pump Failure (Manual Mode)
Indication: PRI TAIL XFER PUMP caution message on and PRI TAIL TANK TRANSFER
FAIL light on.
(1) FUEL, SEC TAIL TANK
TRANSFER switch/light ....................................Press in to start secondary pump.
Check the following:
• SEC TAIL TANK
TRANSFER ON light on,
and
• MANUAL OVRD, MANUAL
light on.
(2) FUEL, PRI TAIL TANK
TRANSFER switch/light ..................................Press out
(3) Fuel tank quantity readouts ................................Monitor that secondary transfer pump
maintains tail and auxiliary
tank quantities normal (i.e., tail
tank is depleting).
Transfer is inoperative:
Yes
(4) Airplane attitude.....................................Level flight if practical.
(5) FUEL, DUMP switch/light ..........................Press in to jettison fuel.
Check DUMP OPEN light on.
Continue to dump fuel until
level flight is achieved.
In level flight, continue to
dump fuel until tail tank
quantity is 1,400 lb.
If auxiliary tank quantity is
below 3,000 lb, dump fuel until
tail tank is empty.
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.
　
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