CESSNA SECTION 9 - SUPPLEMENTS
MODEL 208B 867 SHP SUPPLEMENT 1
GARMIN G1000
U.S.
FAA APPROVED
EMERGENCY PROCEDURES (Continued)
FAILURE OF ICE PROTECTION SYSTEM OR EXCESSIVE
ICE ACCUMULATION (OBSERVED OR SUSPECTED) ON
PROTECTED AIRPLANE SURFACES
(Continued)
• Maintain a minimum airspeed of 120 KIAS with WING
FLAPS UP (110 KIAS minimum if climbing). If unable to
maintain this airspeed in level flight, allow altitude to
decease to maintain airspeed.
• If there are unshed ice accumulations along the wing,
wing strut, or stabilizer leading edges during approach
and landing, follow the procedures listed under
Inadvertent Icing Encounters in Section 3, Emergency
Procedures, of the POH/AFM.
• With an accumulation of 0.25 inch (6.35 mm) or more on
the wing leading edges, be prepared for a significantly
higher power requirement, approach speed, stall speed,
and longer landing roll.
• If necessary, set up a forward slip for visibility through
the left portion of the windshield during the landing
approach.
• Select the minimum flap setting required for available
field length. Use a minimum approach speed for the
selected landing configuration. With ice suspected on
the airframe, or operating at OAT 5°C (41°F) or less in
visible moisture, do not extend WING FLAPS beyond
TO/APR for landing.
S1-23208BPHCUS-S1-00
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