CESSNA SECTION 4
MODEL 208B 867 SHP NORMAL PROCEDURES
GARMIN G1000
U.S.
FAA APPROVED
PREFLIGHT INSPECTION (Continued)
3 LEFT WING Leading Edge
• It is essential in cold weather to remove even the
smallest accumulations of frost, ice, snow, or
slush from the wing and control surfaces. To
assure complete removal of contamination,
conduct a visual and tactile inspection up to two
feet behind the protected surfaces at one
location along the wing span as a minimum.
Also, make sure the control surfaces contain no
internal accumulations of ice or debris. If these
requirements are not performed, airplane
performance will be degraded to a point where a
safe takeoff and climb may not be possible.
• Prior to any flight in known or forecast icing
conditions, check that PITOT/STATIC tube(s) and
STALL warning heaters are warm to touch after
turning PITOT/STATIC and STALL HEAT switches
ON for 30 seconds, then OFF. Make sure the pitot
covers are removed prior to turning PITOT/
STATIC HEAT ON.
1. Wing Tiedown . . . . . . . . . . . . . . . . . . . . . . . . . . . DISCONNECT
2. Stall Warning Vane . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify freedom of movement and warm to the touch)
Make sure elevator control is off the forward stop in order to
check audible warning.
3. Pitot/Static Tube . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify security, openings for stoppage and warmth)
4. Landing and Taxi/Recognition Lights . . . . . . . . . . . . . . CHECK
(condition and cleanliness of cover)
(Continued Next Page)
208BPHCUS-00 4-11
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