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(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
Vol. 1 05−12−25
REV 74, Nov 07/08
▼
CL−604 Operating Manual
PSP 604−6
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
Vol. 1 05−12−26
REV 74, Nov 07/08
▼
CL−604 Operating Manual
PSP 604−6
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:
Yes
(5) FUEL, L (R) TO AUX
XFLOW switch/light ........................... Press in to open affected crossflow
valve.
Check L (R) TO AUX XFLOW
ON light on.
NOTE
Anticipate increasing lateral trim and control forces.
When trim or control forces becomes excessive:
(6) FUEL, L (R) TO AUX
XFLOW switch/light .........................Press out to close affected crossflow
valve.
Check L (R) TO AUX XFLOW
ON light out.
ABNORMAL PROCEDURES
Fuel
Vol. 1 05−12−27
REV 74, Nov 07/08
▼
CL−604 Operating Manual
PSP 604−6
1. FUEL (CONT'D)
AC. Fuel Leak Procedure (Cont’d)
(7) Repeat steps (5) and (6), as necessary to conserve as much fuel as possible
from the leaking tank.
(8) Fuel tank quantity
readouts..............................................Monitor
NOTE
Consider use of asymmetric thrust to maintain fuel
imbalance within limits.
No
(5) Fuel tank quantity readouts ................................Monitor
NOTE
Consider use of asymmetric thrust to maintain fuel imbalance
within limits.
Landing with a FUEL IMBALANCE caution message:
Yes
NOTE
Select the longest runway available with minimum turbulence
and crosswind.
Prior to landing:
(6) GPWS/FLAP OVRD switch
(if installed) ...................................................Select to OVRD, to mute the flap
aural warning.
(7) FLAPS ..........................................................Select to 20° for landing.
　
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