Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 221

PILOT'S OPERATING HANDBOOK
SUPPLEMENT
PROPELLER ANTI-ICE
SYSTEM
(MODEL T210)
SUPPLEMENT
PROPELLER ANTI-ICE SYSTEM
(MODEL T210)
SECTION 1
GENERAL
The propeller anti-ice system provides a measure of protection if
unexpected icing conditions are encountered. The system is operated by a
rocker-type switch located on the left switch and control panel. When the
switch is placed in the ON position, current flows to an anti-ice timer
which supplies electric power in cycles every 20 seconds to elements in the
,,,---.-,, anti-icing boots located on the propeller blades. Operation of the anti-ice
system can be checked by monitoring a propeller anti-ice ammeter near
the upper left corner of the instrument panel. The system is protected by a
circuit breaker, labeled PROP A/ICE, located on the left sidewall circuit
breaker panel.
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SECTION 2
LIMITATIONS
There is no change to the airplane limitations when the propeller anti-
ice system is installed; intentional flight into known icing conditions is
prohibited, regardless of installed ice protection equipment.
SECTION 3
EMERGENCY PROCEDURES
There is no change to the airplane emergency procedures when the
propeller anti-ice system is installed.
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