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7. Refer to the Operating Manual, Volume 1, Chapter 6;
SUPPLEMENTARY PROCEDURES – COLD WEATHER
OPERATION – PHASE OF FLIGHT PROCEDURES.
AR Certified Airplanes
WARNING
When the OAT is 5°C (41°F) or below use deicing/anti-icing
treatment before take-off.
When the OAT is 5°C (41°F) or below the wing anti-ice system must
be selected ON for take-off, just prior to thrust increase for take-off.
NOTE
When Type II, III or IV anti-icing fluids have been applied, the wing
anti-ice system must only be selected ON, if required, just prior to
thrust increase for take-off.
NORMAL PROCEDURES
Ice and Rain Protection
04−14−4
REV 77, Oct 20/09
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. ICE AND RAIN PROTECTION (CONT'D)
G. Cowl Anti-Ice – Before Flight (Engines Running)
(1) ANTI-ICE, COWL L and R
switch/lights ..........................................................Select as required (See Note).
NOTE
1. The engine cowl anti-ice system must be on when the OAT is 10°C
(50°F) or below, and visible moisture in any form is present (such as
fog with visibility of one mile or less, rain, snow, sleet and ice
crystals).
2. The engine cowl anti-ice system must also be on when the OAT is
10°C (50°F) or below when operating on runways, ramps, or
taxiways where surface snow, ice, standing water or slush is
present.
H. Icing Conditions During Flight
NOTE
Icing conditions exist in flight at a TAT of 10°C (50°F) or below, and
visible moisture in any form is encountered (such as clouds, rain, snow,
sleet or ice crystals), except when the SAT is –40°C (–40°F) or below.
WARNING
Delaying the use of cowl anti-ice may result in engine ice ingestion,
resulting in possible severe engine damage and/or flameout.
Delaying the use of wing anti-ice may result in small amounts of ice
accumulation on the wing leading edge.
Small accumulations of ice on the wing leading edge can change the
stall characteristics, the stall speed and the stall margin provided by the
stall protection system.
At or above 22,000 feet, when ice is indicated by the ice detection system,
OR
Below 22,000 feet, when in icing conditions or when ice is indicated by the ice
detection system,
Accomplish the following:
(1) Thrust ...................................................................Check N2 RPM 78% minimum.
(2) ANTI-ICE, COWL L and R
switch/lights .......................................................Press in to select cowl anti-ice on.
Check COWL A/ICE ON
advisory message on.
NORMAL PROCEDURES
Ice and Rain Protection
04−14−5
REV 77, Oct 20/09
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. ICE AND RAIN PROTECTION (CONT'D)
H. Icing Conditions During Flight (Cont’d)
(3) ANTI-ICE, WING switch .......................................Select to NORM.
Check the following:
• L and R WING A/ICE
caution messages may
come on briefly, then out.
• N2 gauges change colour to
indicate wing anti-ice on.
• WING/COWL A/ICE ON
advisory message on.
• WING L HEAT and R HEAT
lights on.
If WING/COWL A/ICE ON advisory message is out
OR
If WING L HEAT or R HEAT light is out:
(4) Thrust ............................................................... Increase until the following come on:
• WING/COWL A/ICE ON
advisory message
• WING L HEAT and R HEAT
lights
If WING/COWL A/ICE ON advisory message remains out
OR
If WING L HEAT or R HEAT light remains out:
(5) Leave icing conditions.
NORMAL PROCEDURES
Ice and Rain Protection
04−14−6
REV 77, Oct 20/09
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. ICE AND RAIN PROTECTION (CONT'D)
H. Icing Conditions During Flight (Cont’d)
If required:
(6) ANTI-ICE, WSHLD/WIND L and R
switches................................................................Select to HI.
NOTE
1. Flaps should not be extended in icing conditions except as required
for take-off, approach and landing. However, if flaps are deployed in
icing conditions for extended periods or in severe icing, light to
moderate buffet may be encountered. No handling difficulties will
result, and normal landing flaps can be used. If the buffet is
alleviated by reducing the flap setting, a landing in this configuration
may be made at the discretion of the pilot. Refer to Chapter 5;
　
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