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passengers within cabin.
END
ABNORMAL PROCEDURES
Air-Conditioning and Pressurization
05−05−6
REV 69, Jun 04/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. AIR-CONDITIONING AND PRESSURIZATION (CONT'D)
H. Manual Cabin Pressurization Control Procedure
NOTE
The MAN ALT selector is a three (3) position switch. The switch is
spring-loaded to mid position/centre.
(1) CABIN PRESSURIZATION,
MAN ALT selector ................................................Check set to mid position/centre.
(2) CABIN PRESSURIZATION,
PRESS CONT switch/light ................................Press in to select manual mode.
Check PRESS CONT
MANUAL light on.
Operate CABIN PRESS, MAN
ALT and MAN RATE switches
as required.
To increase cabin altitude:
(3) CABIN PRESSURIZATION, MAN
ALT selector .......................................... Select and hold to UP.
(4) CABIN PRESSURIZATION, MAN
RATE switch................................................ As required
To decrease cabin altitude:
(5) CABIN PRESSURIZATION, MAN
ALT selector .......................................... Select and hold to DN.
(6) CABIN PRESSURIZATION,
MAN RATE switch....................................... As required
To maintain cabin altitude:
When reaching target cabin altitude as per the chart below:
(7) CABIN PRESSURIZATION, MAN
ALT selector .....................................Mid position/centre
Cruise Flight Level 180 200 220 240 260 280 290 310 330
Target Cabin Altitude 1700 2000 2400 2800 3200 3700 4100 4600 5300
Cruise Flight Level 350 370 390 410
Target Cabin Altitude 6000 6700 7400 8000
Before landing:
NOTE
Do not set cabin altitude below destination field elevation.
ABNORMAL PROCEDURES
Air-Conditioning and Pressurization
05−05−7
REV 68, Apr 16/07
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. AIR-CONDITIONING AND PRESSURIZATION (CONT'D)
H. Manual Cabin Pressurization Control Procedure (Cont’d)
Differential pressure exists after landing:
Yes
(8) CABIN PRESSURIZATION,
MAN ALT selector ......................... Select and hold to UP.
(9) CABIN PRESSURIZATION,
MAN RATE switch ............................................ Set to maximum INCR.
− END −
No
(8) No further action required.
END
I. Display Overtemperature
Indication: DISPLAY TEMP annunciation on affected CRT. Raster image is removed
from affected CRT.
EICAS display is affected:
Yes
(1) EICAS Primary Display or
Secondary Display Failure
procedure ............................................ Accomplish Refer to AURAL/VISUAL
WARNING SYSTEM in this
chapter.
− END −
No
Primary flight display (PFD) is affected:
Yes
(1) Primary Flight Display Failure
procedure ............................................ Accomplish Refer to INSTRUMENTS
SYSTEM in this chapter.
− END −
No
Multifunction display (MFD) is affected:
(1) No further action required.
END
ABNORMAL PROCEDURES
Air-Conditioning and Pressurization
05−05−8
REV 68, Apr 16/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. AIR-CONDITIONING AND PRESSURIZATION (CONT'D)
J. Cabin Pressure Acquisition Module Failure
Indication: CPAM FAIL caution message on.
NOTE
EICAS pressurization system readouts (e.g., cabin altitude, rate of
change, and differential pressure) are not available. EICAS cabin
pressure warning and caution messages are also not available.
(1) Standby cabin altimeter......................................Monitor
END
ABNORMAL PROCEDURES
Air-Conditioning and Pressurization
05−05−9
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
ABNORMAL PROCEDURES
Air-Conditioning and Pressurization
05−05−10
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. AUTOMATIC FLIGHT CONTROL SYSTEM
NOTE
Autopilot disconnect warnings are indicated by “Cavalry Charge”
aural and flashing red AP message on primary flight display.
A. Autopilot Mistrim
Indication: AP TRIM IS LWD (RWD) (ND) (NU) caution messages on.
Aileron (A) or elevator (E) flags displayed on the primary flight displays.
(1) Autopilot .............................................................Monitor operation.
　
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