SOLOY TURBINE PAC
SECTION 3
POHS CESSNA T206H/206H
EMERGENCY PROCEDURES
3-10
F.A.A. Approved
May 23, 2003
These systems must be operated in the
above mentioned conditions even if there is
no visible sign of airframe ice and/or snow
accumulation.
Deactivation of the systems shall not be
made until the above mentioned conditions
no longer exist and the engine alternate air
must be used until all accumulated airframe
ice and/or snow has dissipated.
1. Engine Inlet Anti-Ice – UNLOCK, PULL ON, LOCK
NOTE
To verify proper functioning of the engine
anti-ice system, confirm a drop in torque
and a rise in TOT.
2. Turn pitot heat switch ON
3. Turn back or change altitude to obtain an OAT that is less
conducive to icing.
4. Pull cabin heat and defrost controls to full out to obtain maximum
windshield defroster airflow.
5. If icing conditions are unavoidable, plan a landing at the nearest
airport.
6. With an ice accumulation of ¼ inch or more on the wing leading
edges, be prepared for a significantly higher power requirement,
approach speed, stall speed, and landing roll.
7. Open left window and, if practical, scrape ice from a portion of
the windshield for visibility during the landing approach.
8. Use a 10
to 20
landing flap setting for ice accumulations of 1
inch or less. With heavier ice accumulations, approach with
flaps retracted to ensure adequate elevator effectiveness in the
approach and landing.
9. Approach at 95-100 KIAS with 20° flaps and 105-115 KIAS with
0° - 10° flaps, depending upon the amount of ice accumulation.
If ice accumulation is unusually large, decelerate to the planned
approach speed while in the approach configuration at a high
enough altitude which would permit recovery in the event that a
stall buffet is encountered.
10. Land on the main wheels first, avoiding the slow and high type of
flare-out.
UNCONTROLLED
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