Textron Cessna Grand Caravan Ex 208B - RIGHT WING Leading Edge; RIGHT WING Trailing Edge

SECTION 4 CESSNA
NORMAL PROCEDURES MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
PREFLIGHT INSPECTION (Continued)
6 RIGHT WING Trailing Edge
1. Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify condition and security)
2. Spoiler . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify condition and security)
3. Flap Leading Edge Vortex Generators . . . . . . . . . . . . . CHECK
(verify condition and security)
4. Aileron and Trim Tab . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify condition and security)
5. Static Wicks (4 total) . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify condition)
6. Fuel Tank Vent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify opening is clear)
7 RIGHT WING Leading Edge
WARNING
• 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.
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208BPHCUS-004-16