Right Wing Trailing Edge; Right Wing Leading Edge - Cessna Grand Caravan 208B G1000 Manual

CESSNA
MODEL 208B G1000

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

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.
FAA APPROVED
208BPHBUS-00
WARNING
are not performed,
(Continued Next Page)
SECTION 4
NORMAL PROCEDURES
(verify condition and security)
(verify condition and security)
(verify condition and security)
(verify condition and security)
(verify condition)
(verify no obstructions)
aircraft
U.S.
4-13