Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 223

PILOT'S OPERATING HANDBOOK
SUPPLEMENT
SUPPLEMENT
WINDSHIELD
ANTI-ICE SYSTEM
(MODEL T210)
WINDSHIELD ANTI-ICE SYSTEM
(MODEL T210}
SECTION 1
GENERAL
The windshield anti-ice system assures adequate visibility for a
landing during flight conditions where ice may form on the windshield.
A
detachable electrically-heated glass panel,
11.0
inches high by
5.5
inches
wide, mounts to the base of the windshield in front of the pilot. Quick
disconnects are provided to facilitate ease of installation and removal.
,~ , When not in use, a padded cover i s provided for protection against
scratches, breakage, and wiring damage, and the panel may be stowed in
the seat pocket on the aft side of the pilot's or co-pilot's seat back.
Windshield anti-icing is controlled by a rocker-type switch, labeled W /S
A/ICE, on the left switch and control panel.
The heated glass panel should be installed whenever icing conditions
are a possibility on a proposed flight, especially if the freezing level is near
or at the surface.
SECTION 2
LIMITATIONS
,,.J
This is no change to the airplane limitations when the windshield anti-
ice system is installed; intentional flight into known icing conditions is
prohibited regardless of installed ice protection equipment. Prolonged
operation of the system without the engine running should be avoided.
SECTION 3
EMERGENCY PROCEDURES
There is no change to the airplane emergency procedures when the
windshield anti-ice system is installed.
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