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reduce differential pressure.
DIFF PRESS warning message persists:
Yes
(4) Descent ....................................................... Initiate to 10,000 feet or lowest safe
altitude, whichever is higher.
(5) AIR-CONDITIONING, L (R)
PACK switch/light ....................................Press out to shutdown one pack.
Check L (R) PACK OFF light
on.
DIFF PRESS warning message persists:
Yes
(6) AIR-CONDITIONING, L
and R PACK switch/lights ................Press out to shutdown both packs.
Check L and R PACK OFF
lights on.
(7) CABIN
PRESSURIZATION,
EMER DEPRESS
switch/light ......................................... Press in to depressurize the airplane.
Check the following:
• EMER DEPRESS ON light
on, and
• EMER DEPRESS caution
message on.
(8) Descent................................................ Initiate to the lowest possible altitude.
EMERGENCY PROCEDURES
Air−Conditioning and Pressurization
Vol. 1 03−05−4
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
1. AIR-CONDITIONING AND PRESSURIZATION (CONT'D)
C. High Rate of Cabin Pressurization or Over-Pressurization (Cont’d)
(9) Unpressurized Flight
Procedure .....................................Accomplish Refer to Chapter 5;
ABNORMAL PROCEDURES
– AIR-CONDITIONING AND
PRESSURIZATION –
Unpressurized Flight
Procedure.
− END −
No
(6) Cabin altitude..............................................Monitor
− END −
No
(4) Manual cabin pressurization
control procedure ............................................ Continue
(5) Cabin altitude .....................................................Monitor
END
EMERGENCY PROCEDURES
Air−Conditioning and Pressurization
Vol. 1 03−05−5
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
EMERGENCY PROCEDURES
Air−Conditioning and Pressurization
Vol. 1 03−05−6
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
THIS PAGE INTENTIONALLY LEFT BLANK
1. AUTOMATIC FLIGHT CONTROL SYSTEM
NOTE
After generator transfers, AFCS channel 2 will momentarily fail and
the following must be manually re-engaged:
• Yaw damper 2 (YD 2), and
• Autopilot (if it was coupled before the power interruption, and
operating on AFCS channel 2).
A. Autopilot Failure
Indication: Abnormal autopilot operation and/or “CAVALRY CHARGE” aural and/or
flashing AP (red) message on the primary flight displays.
(1) Autopilot ....................................................... Disconnect using AP/SP DISC switch on
the control wheel, or the AP
DISC switch on the FCP.
(2) AFCS SEL 1 (2) switch (centre
pedestal)...............................................................Select to operative AFCS channel.
Check AFCS 1 (2) INOP status
message on.
(3) Autopilot ....................................................... Re-engage
Autopilot warning persists:
Yes
(4) Autopilot................................................ Disconnect using AP/SP DISC switch on
the control wheel, or the AP
DISC switch on the FCP.
(5) Manual control .......................................... Resume
− END −
No
(4) No further action required.
END
EMERGENCY PROCEDURES
Automatic Flight Control System
Vol. 1 03−06−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. AUTOMATIC FLIGHT CONTROL SYSTEM (CONT'D)
B. AFCS Messages Failure
Indication: AFCS MSGS FAIL warning message and/or flashing AP (red) message on
the primary flight displays.
(1) Autopilot ....................................................... Disconnect using AP/SP DISC switch on
the control wheel, or the AP
DISC switch on the FCP.
NOTE
Do not use the autopilot when an AFCS MSGS FAIL warning message
is displayed.
(2) Manual control.................................................. Resume
END
EMERGENCY PROCEDURES
Automatic Flight Control System
Vol. 1 03−06−2
REV 69, Jun 04/07
CL−604 Operating Manual
PSP 604−6
1. AUXILIARY POWER PLANT
A. APU Fire
Indication: APU FIRE PUSH light on, APU FIRE warning message and fire bell on.
(1) APU FIRE PUSH switch/light ............................Press in Check the following:
• BOTTLE ARMED PUSH
TO DISCH light on, and
• APU SOV CLSD advisory
message on.
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庞巴迪挑战者604操作手册 Operating Manual 1(47)
