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− END −
No
(3) No further action required.
END
ABNORMAL PROCEDURES
Ice and Rain Protection
05−14−8
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. ICE AND RAIN PROTECTION (CONT'D)
H. Insufficient Heat for Wing Anti-Icing
Indication: Wing anti ice selected ON and WING L HEAT or R HEAT light goes out or
WING A/ICE ON or WING/COWL A/ICE ON advisory message goes out.
(1) Thrust ............................................................... Increase until the following come on:
• WING A/ICE ON or
WING/COWL A/ICE ON
advisory message.
• WING L HEAT and R HEAT
lights.
WING A/ICE ON or WING/COWL A/ICE ON advisory message remains out or
WING L HEAT or R HEAT light remains out:
Yes
(2) Leave icing conditions.
− END −
No
(2) No further action required.
END
ABNORMAL PROCEDURES
Ice and Rain Protection
05−14−9
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. ICE AND RAIN PROTECTION (CONT'D)
I. Probe Heater Failures
Indication: • L (R) AOA HEAT caution message,
• AUX AOA CASE (VANE) HEAT caution message,
• L (R) PITOT BASE (TUBE) HEAT caution message,
• L (R) STATIC HEAT caution message,
• STBY PITOT HEAT caution message,
• TAT PROBE HEAT caution message,
• L (R) PROBE HEAT OFF caution message.
(1) ANTI-ICE, PROBES L and R
switches................................................................Select OFF and then ON.
Applicable caution message still on:
Yes
MESSAGE ACTION
L (R) AOA HEAT Do not rely on stall protection system.
(2) No further action required.
AUX AOA CASE HEAT
AUX AOA VANE HEAT
Do not rely on low speed cue displayed on both PFDs.
(2) No further action required.
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
05−14−10
REV 68, Apr 16/07
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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
05−14−11
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
ABNORMAL PROCEDURES
Ice and Rain Protection
05−14−12
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. INSTRUMENTS SYSTEM
A. Primary Flight Display Failure
Indication: PFD goes blank.
(1) Reversionary panel, applicable
　
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