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Check the following:
• 10TH ISOL OPEN light out.
• APU LCV OPEN light on.
(c) BLEED AIR, 10TH
STAGE L switch/light .........................Press in to open left valve and close
APU load control valve.
Check the following:
• L 10TH CLOSED light out.
• APU LCV OPEN light out.
(d) BLEED AIR, APU LCV
switch/light .......................................Press out to match APU load control
valve closed position.
No
(1) APU, PWR FUEL switch/light..........................Press out
(2) Land at the nearest suitable airport.
END
E. APU Fuel Shut-Off Valve not in the Selected Position
Indication: APU SOV caution message on.
(1) No further action required. The APU is not available.
END
ABNORMAL PROCEDURES
Auxiliary Power Unit
05−07−4
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. AUXILIARY POWER UNIT (CONT'D)
F. APU Negative-G Shut-Off Valve Failed to Close After APU Shutdown Due to Fire
Indication: APU NEG-G SOV caution message on.
(1) FUEL, L BOOST PUMP
switch/light .......................................................Press out to disarm affected boost
pump.
Check the following:
• L FUEL PUMP ON advisory
message out, and
• L FUEL PUMP INOP light
on.
(2) Left engine......................................................Shutdown Refer to POWER PLANT −
In-Flight Engine
Failure/Shutdown procedure in
this chapter.
END
G. APU Pump Failure
Indication: APU PUMP caution message on.
On ground:
Yes
(1) APU ........................................................Shutdown
− END −
No
In flight:
APU generator is essential (both main generators failed):
Yes
(1) APU indications ..........................................Monitor
(2) Land at the nearest suitable airport.
CAUTION
APU adapter oil will no longer be cooled. Adapter oil will
overheat causing APU to auto-shutdown.
− END −
No
(1) APU................................................................Shutdown
END
ABNORMAL PROCEDURES
Auxiliary Power Unit
05−07−5
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
ABNORMAL PROCEDURES
Auxiliary Power Unit
05−07−6
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. DOORS
A. Passenger Door – Outer Handle not Stowed
Indication: PAX DOOR OUT HNDL caution message on.
(1) PASS SIGNS, SEAT BLTS switch .......................Select to ON.
(2) Cabin pressure .....................................................Check normal.
Cabin pressure is normal:
Yes
(3) Passenger door ............................................Check visually, and ensure that four
roll-over catch green witness
marks are correctly aligned.
All 4 witness marks are aligned:
Yes
(4) Passenger door, inner
T-handle.................................................... Pull to stow outer handle. Green
LOCKED flag-indicator visible.
When the handle is locked:
(5) Passenger door, inner
T-handle..............................................Push in to stow inner T-handle, and
then close inner T-handle
access cover.
Check PAX DOOR STOW
caution message out.
PAX DOOR OUT HNDL caution message persists:
Yes
(6) Land at the nearest suitable airport.
− END −
No
(6) No further action required.
− END −
No
Switch to manual pressurization control:
(3) CABIN PRESSURIZATION, MAN
ALT selector .........................................................Check set to mid position/centre.
(4) CABIN PRESSURIZATION,
PRESS CONT switch/light ...................................Select to manual mode.
Check PRESS CONT
MANUAL light on.
ABNORMAL PROCEDURES
Doors
05−08−1
REV 68, Apr 16/07
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. DOORS (CONT'D)
A. Passenger Door – Outer Handle not Stowed (Cont’d)
(5) CABIN PRESSURIZATION, MAN
ALT selector ................................................ As required to maintain cabin altitude at
8,000 feet, to minimize the
pressure differential across
the affected door.
NOTE
Set the selector to “UP” to increase cabin altitude; “DN” to
reduce cabin altitude.
(6) CABIN PRESSURIZATION, MAN
　
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