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L (R) PITOT TUBE HEAT
L (R) PITOT BASE HEAT
Do not rely on associated instruments:
• ATC transponder,
• Air Data Computer, and
• Inertial Reference System.
(2) Select ADC source to operative side.
L (R) STATIC HEAT
Do not rely on associated instruments:
• Standby altimeter and indicated airspeed indicator,
and
• Cabin Pressure Acquisition Module.
(2) No further action required.
STBY PITOT HEAT Do not rely on standby indicated airspeed indicator.
(2) No further action required.
TAT PROBE HEAT Do not rely on air temperature indications.
(2) No further action required.
L (R) PROBE HEAT OFF During flight – No further action required.
Both L and R AOA HEAT messages persist:
Yes
(2) Avoid icing conditions.
(3) Stall Protection System
Failure procedure..........................Accomplish Refer to FLIGHT CONTROLS
– Stall Protection System
Failure in this Chapter.
− END −
ABNORMAL PROCEDURES
Ice and Rain Protection
Vol. 1 05−14−10
REV 68, Apr 16/07
▼
CL−604 Operating Manual
PSP 604−6
1. ICE AND RAIN PROTECTION (CONT'D)
I. Probe Heater Failures (Cont’d)
No
(2) No further action required.
END
J. Windshield/Window Heat Failure
Indication: L (R) WINDOW HEAT caution message,
L (R) WSHLD HEAT caution message.
(1) Affected ANTI-ICE,
WSHLD/WIND switch...........................................Select to RESET, then LO or HI as
applicable.
Caution message persists:
Yes
(2) CKPT HEAT switch ......................................Select to ON.
(3) AIR (cockpit heat diverter
valve) ..........................................................Pull out
− END −
No
(2) No further action required.
END
K. Windshield Outer Face Ply Failure
(1) Affected ANTI-ICE,
WSHLD/WIND switch...........................................Select to OFF.
(2) CKPT HEAT switch ..............................................Select to ON.
(3) AIR (cockpit heat diverter valve) ........................Pull out
END
ABNORMAL PROCEDURES
Ice and Rain Protection
Vol. 1 05−14−11
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
ABNORMAL PROCEDURES
Ice and Rain Protection
Vol. 1 05−14−12
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
THIS PAGE INTENTIONALLY LEFT BLANK
1. INSTRUMENTS SYSTEM
A. Primary Flight Display Failure
Indication: PFD goes blank.
(1) Reversionary panel, applicable
MFD L (R) switch..................................................Select to PFD.
Check applicable MFD reverts
to primary flight display.
END
B. Display Control Panel Failure
Indication: Display control panel is inoperative, course and HDG knob is inoperative.
(1) Reversionary panel, DCP switch..........................Select operative side.
(2) Autopilot XFR switch ............................................Select side corresponding to
operative display control
panel.
NOTE
HDG knob remains inoperative until operable display control panel is
selected.
END
C. EFIS Comparator Failure
Indication: EFIS COMP INOP caution message.
(1) Affected flight instruments ..................................Monitor
(2) Standby instruments................................................ Use to cross-check.
END
D. EFIS Comparator Monitor Failures
Indication: EFIS COMP MON caution message on, and one of the following comparator
warning annunciators shown on the primary flight display.
• ALT • IAS • ROL • LOC
• HDG • PIT • RA • GS
PFD ACTION
ALT and/or IAS
(1) Flight instruments and
standby flight instruments............Cross
check
(2) Centre pedestal, AIR
DATA source selector
switch.......................................... Select to reliable side
Refer to Airplane Flight Manual, Chapter 6; PERFORMANCE, for
alternate static system position error correction charts.
ABNORMAL PROCEDURES
Instruments System
Vol. 1 05−15−1
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
1. INSTRUMENTS SYSTEM (CONT'D)
D. EFIS Comparator Monitor Failures (Cont’d)
PFD ACTION
ROL or PIT
(1) Flight instruments and
standby flight instruments............Cross
check
(2) Reversionary panel, IRS
switch.......................................... Select to reliable alternate
source.
　
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