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The minimum ambient temperature approved for take-off is
–40°C (–40°F).
− END −
No
During flight:
(1) Airplane .............................................................Operate as follows:
• Descend or deviate to
warmer air mass, or
• Increase airspeed.
END
ABNORMAL PROCEDURES
Fuel
05−12−5
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FUEL (CONT'D)
G. Fuel Temperature Less than 5°C
Indication: L (R) FUEL LO TEMP caution message on. 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
H. Fuel Boost Pump Failure
Indication: L (R) FUEL PUMP caution message and L (R) BOOST PUMP INOP light
on.
(1) FUEL, L (R) BOOST PUMP
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
05−12−6
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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
05−12−7
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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
05−12−8
REV 74, Nov 07/08
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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.
　
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