SOLOY TURBINE PAC SECTION 4
POHS CESSNA T206H/206H NORMAL PROCEDURES
4-24
F.A.A. Approved May 23, 2003
FLIGHT IN ICING CONDITIONS
Flight into icing conditions is prohibited. An inadvertent encounter with
these conditions can best be handled using the checklist procedures in
Section 3. The best procedure, of course, is to turn back or change
altitude to escape icing conditions.
NOTE
The engine inlet anti-ice must be used in visible
moisture at an OAT of 5C (41F).
The engine inlet anti-ice and alternate air must be
activated for flight or ground operation in visible
moisture at an OAT of 1C (34F) and below or while
operating in falling or blowing snow regardless of
ambient temperature.
Deactivation of the systems shall not be made until
the above mentioned conditions no longer exist and
all accumulated airframe ice has dissipated.
STALLS
The stall characteristics are conventional, and aural warning is provided by
a stall warning horn, which sounds between 5 and 10 knots above the stall
in all configurations.
Power off stall speeds at maximum weight for both forward and aft C.G. are
presented in Section 5.
DESCENT
Descent should be initiated far enough in advance of estimated landing to
allow at gradual rate of descent. Descent should be at approximately 500
FPM for passenger comfort. Do not exceed Vmo during descent (aircraft
accelerates rapidly with cruise power).
The airplane is equipped with a specially marked altimeter to attract the
pilot's attention and prevent misreading the altimeter. A striped warning
segment on the face of the altimeter is exposed at all altitudes below
10,000 feet to indicate low altitude.
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