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REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
6. AIRFRAME DEICING, ANTI-ICING, AND INSPECTION (CONT'D)
C. Removal of Loose Contamination
If significant amounts of loose snow are on the airplane:
(1) Flaps............................................................ As required Flaps 45° recommended.
(2) Snow ................................................................ Remove from the following areas, and
inspect for presence of
adhering ice, frost or snow:
• Wings – leading edges,
upper and lower surfaces;
• Upper fuselage;
• Vertical and horizontal
stabilizers – leading edges,
upper/lower surfaces and
side panels;
• Flaps, flap tracks and flap
drives;
• Ailerons, elevators, rudder
and spoilers;
• Air data probes/sensors,
AOA vanes;
• Antennas;
• Fuel drains and NACA vent
scoops;
• Engine and APU intakes;
APU exhaust;
• Landing gear and landing
gear bays;
• Windshield, windows; door
sills and surrounds.
CAUTION
Excessive temperatures in the windshield may result in permanent
damage.
NOTE
A light accumulation of snow may be cleared from the windshield, by setting
the WSHLD/WIND heat switches on the overhead panel to LOW.
(3) Tactile check ............................................... Accomplish
If deicing/anti-icing is not planned:
(4) Limitations .......................................................... Review Refer to Chapter 2;
LIMITATIONS.
SUPPLEMENTARY PROCEDURES
Cold Weather Operations
Vol. 1 06−12−19
REV 74, Nov 07/08
▼
CL−604 Operating Manual
PSP 604−6
6. AIRFRAME DEICING, ANTI-ICING, AND INSPECTION (CONT'D)
C. Removal of Loose Contamination (Cont’d)
If frozen contamination is found adhering to critical surfaces:
(5) Deicing/anti-icing ......................................... Accomplish
D. Preparation for Deicing/Anti-Icing
Before fluid is applied:
NOTE
It is recommended that the application of deicing/anti-icing fluid be carried
out with the engines and APU off. If this is not possible, steps (2) to (7),
following, must be observed.
If engines/APU are off:
(1) Proceed to step (8).
If engines/APU are operating:
(2) Thrust levers...........................................................IDLE for the duration of the
operation.
NOTE
If the APU is running, ensure that personnel carrying out the fluid
application are aware of the location of the APU air intake, and have
been instructed to avoid fluid spray that can be ingested by the APU.
(3) AIR-CONDITIONING, L and R
PACK switch/lights ..........................................Press out Check L and R PACK OFF
lights on.
(4) BLEED AIR, 10TH STAGE L and
R switch/lights .................................................Press out Check L and R 10TH STAGE
CLOSED lights on.
(5) ANTI-ICE, WING switch ..........................................OFF
(6) ANTI-ICE, COWL L and R
switch/lights .....................................................Press out Check L and R COWL ON
lights out.
(7) BLEED AIR, 14TH STAGE L and
R switch/lights .................................................Press out Check L and R 14TH STAGE
CLOSED lights on.
(8) Stabilizer trim............................................... As required In most cases, it is advisable
to set the stabilizer trim to
nose up, in order for the
deicing fluid and contaminants
to run off more easily. Set
stabilizer trim for take-off after
completion of the deicing
procedure.
SUPPLEMENTARY PROCEDURES
Cold Weather Operations
Vol. 1 06−12−20
REV 74, Nov 07/08
▼
CL−604 Operating Manual
PSP 604−6
6. AIRFRAME DEICING, ANTI-ICING, AND INSPECTION (CONT'D)
D. Preparation for Deicing/Anti-Icing (Cont’d)
(9) Flaps............................................................ As required If the flaps require deicing,
extend to (or leave at) 45°
during the deicing procedure.
Upon completion, retract to 0°
or set for take-off, as
applicable. Otherwise, leave
flaps retracted or in their
present position, as
applicable.
(10) Deicing operator .................................................. Advise to avoid direct spraying of the
anti-icing fluid jet, to prevent
damage on:
• Windshields, side windows
and cabin windows;
• Pitot/static and TAT probes;
• AOA vanes;
• Static pressure ports;
　
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