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TRANSFER ON light on,
and
• SEC TAIL TANK
TRANSFER ON light on.
(3) Fuel tank quantity readouts ................................Monitor to ensure that auxiliary tank
quantity does not exceed
7,000 lb.
END
AB. Loss of Totalizer Fuel Quantity Indication
Indication: Totalizer fuel quantity indication dashed.
(1) Fuel tank quantity readouts ................................Monitor sum of each tank vs fuel burn.
END
ABNORMAL PROCEDURES
Fuel
05−12−24
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FUEL (CONT'D)
AC. Fuel Leak Procedure
Indication: 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 to determine location of leak.
Expedite landing if tank quantity gauge indications are amber.
NOTE
1. The minimum fuel quantity for go-around is 230 kg (500 lb) per wing
(with the airplane level), and assuming a maximum airplane climb
attitude of 10° nose up.
2. Do not action FUEL IMBALANCE , L (R) FUEL LO PRESS or L (R)
SCAV EJECTOR caution messages or L (R) MAIN EJECTOR FAIL
status messages. Disregard fuel imbalance limitations.
(3) Autopilot .............................................................Monitor operation.
NOTE
Anticipate out of trim situation when disconnecting autopilot.
Fuel leak from engine is suspected:
Yes
On low quantity side:
(4) Thrust lever................................ Confirm and IDLE
(5) Thrust lever......................................... Confirm and
SHUT OFF
(6) Affected ENG FIRE PUSH
switch/light .................................................Press in to close engine fuel feed SOV.
(7) Affected engine.......................................Shutdown Refer to POWER PLANT –
In-Flight Engine
Failure/Shutdown Procedure
in this chapter.
− END −
ABNORMAL PROCEDURES
Fuel
05−12−25
REV 74, Nov 07/08
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FUEL (CONT'D)
AC. Fuel Leak Procedure (Cont’d)
No
Fuel leak from wing tank is suspected:
(4) FUEL, GRAVITY/XFLOW
switch/light .......................................................Press out to close gravity crossflow
valve.
Check GRAVITY XFLOW
OPEN light out.
Range is a consideration:
Yes
NOTE
Consider use of asymmetric thrust to use as much fuel as
possible from the leaking tank.
Leak in auxiliary tank is confirmed:
Yes
(5) FUEL, TAIL TANK
TRANSFER, MANUAL
OVRD switch/light.............................. Press in to select manual transfer.
Check MANUAL light on.
(6) Auxiliary fuel tank
quantity readout ..................................Monitor
When auxiliary tank quantity has stabilized:
(7) FUEL, PRI TAIL TANK
TRANSFER switch/light.....................Press in to start primary pump.
Check PRI TAIL TANK
TRANSFER ON light on.
Ensure auxiliary and tail tank
quantities remain within limits.
Refer to Figure 02−05−3.
− END −
No
Leak in tail tank is confirmed:
Yes
(5) FUEL, TAIL TANK
TRANSFER, MANUAL
OVRD switch/light.............................. Press in to select manual transfer.
Check MANUAL light on.
ABNORMAL PROCEDURES
Fuel
05−12−26
REV 74, Nov 07/08
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. FUEL (CONT'D)
AC. Fuel Leak Procedure (Cont’d)
(6) FUEL, PRI and SEC TAIL
TANK TRANSFER
switch/lights ....................................... Press in to start both pumps.
Check the following:
• PRI TAIL TANK
TRANSFER ON light on,
and
• SEC TAIL TANK
TRANSFER ON light on.
Ensure auxiliary and tail tank
quantities remain within limits.
Refer to Figure 02−05−3.
When AUX TANK HEAVY caution message is displayed:
(7) FUEL, PRI and SEC TAIL
TANK TRANSFER
switch/lights .....................................Press out to stop both pumps.
Check the following:
• PRI TAIL TANK
TRANSFER ON light out,
and
• SEC TAIL TANK
TRANSFER ON light out.
− END −
No
Leak in wing tank is confirmed:
　
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