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pressure warning and caution messages are also not available.
(1) Standby cabin altimeter......................................Monitor
END
ABNORMAL PROCEDURES
Air-Conditioning and Pressurization
Vol. 1 05−05−9
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
ABNORMAL PROCEDURES
Air-Conditioning and Pressurization
Vol. 1 05−05−10
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
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.
Retrim as required.
NOTE
Anticipate out of trim situation when disconnecting or changing
autopilot.
Caution message persists:
Yes
(2) Autopilot................................................ Disconnect
(3) AFCS SEL 1(2) switch
(centre pedestal)...........................................Select to operative AFCS channel.
Check AFCS 1 (2) INOP status
message on.
(4) Autopilot..................................................... Engage and monitor operation.
Retrim as required.
Caution message persists:
Yes
(5) Autopilot........................................ Disconnect and assume manual control.
− END −
No
(2) No further action required.
END
ABNORMAL PROCEDURES
Automatic Flight Control System
Vol. 1 05−06−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. AUTOMATIC FLIGHT CONTROL SYSTEM (CONT'D)
B. Autopilot Pitch Trim Failure
Indication: AP PITCH TRIM caution message on.
NOTE
Failure is resultant of autopilot pitch trim not being able to keep up with
the pitch change.
Anticipate elevator out of trim situation when disconnecting the
autopilot.
(1) Autopilot ....................................................... Disconnect Retrim as required.
(2) AFCS SEL 1(2) switch
(centre pedestal) ..................................................Select to operative AFCS channel.
Check AFCS 1 (2) INOP status
message on.
(3) FDs and autopilot .............................................. Engage and monitor operation.
Retrim as required.
AP PITCH TRIM caution message persists:
Yes
(4) Autopilot................................................ Disconnect and assume manual control.
− END −
No
(4) No further action required.
END
ABNORMAL PROCEDURES
Automatic Flight Control System
Vol. 1 05−06−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. AUTOMATIC FLIGHT CONTROL SYSTEM (CONT'D)
C. Double Yaw Damper Failure
Indication: YAW DAMPER caution message on. Autopilot will disengage if it was
coupled.
(1) YAW DAMPER, YD1 and YD2
switches.............................................................Press in to engage both yaw dampers.
YAW DAMPER caution message persists:
Yes
(2) YAW DAMPER, DISC button ....................Press in to disconnect both yaw
dampers.
(3) FLAPS ..........................................................Select as required. Land with flaps at
20°, commensurate with the
controllability of the airplane.
No
Landing with FLAPS at 20 degrees:
Yes
Prior to landing:
(2) GPWS/FLAP OVRD switch
(if installed) ...................................................Select to OVRD, to mute the flap
aural warning.
(3) Approach speed ...........................VREF (Flaps 45°)
+ 14 KIAS minimum.
(4) Actual landing distance............................. Increase as applicable by factor given
below:
WITHOUT THRUST REVERSERS WITH THRUST REVERSERS
1.55 (55%) 1.50 (50%)
NOTE
Select the runway available with minimum crosswind.
− END −
No
(2) No further action required.
END
ABNORMAL PROCEDURES
Automatic Flight Control System
Vol. 1 05−06−3
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. AUTOMATIC FLIGHT CONTROL SYSTEM (CONT'D)
D. Single Flight Director Failed
Indication: FD 1 (2) FAIL status message on, FD annunciator flag displayed on affected
PFD, loss of flight director guidance cue on affected PFD, and autopilot may
　
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