Right Wing Trailing Edge; Right Wing Leading Edge - Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual

SECTION 4
NORMAL PROCEDURES
PREFLIGHT INSPECTION
6

RIGHT WING Trailing Edge

1. Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
2. Spoiler . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
3. Flap Leading Edge Vortex Generators . . . . . . . . . . . . . CHECK
4. Aileron and Trim Tab . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
5. Static Wicks (4 total) . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
6. Fuel Tank Vent . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
7

RIGHT 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
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.
4-16
(Continued)
WARNING
are not
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U.S.
MODEL 208B 867 SHP
GARMIN G1000
(verify condition and security)
(verify condition and security)
(verify condition and security)
(verify condition and security)
(verify condition)
(verify opening is clear)
performed, airplane
FAA APPROVED
208BPHCUS-00
CESSNA