Textron Cessna Grand Caravan Ex 208B - LEFT WING Trailing Edge

SECTION 4 CESSNA
NORMAL PROCEDURES MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
PREFLIGHT INSPECTION (Continued)
4 LEFT WING Trailing Edge
1. Fuel Tank Vent Opening . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify opening is clear)
2. Aileron and Servo Tab. . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify condition and security)
3. Static Wicks (4 total) . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify condition)
4. Spoiler . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify condition and security)
5. Flap Leading Edge Vortex Generators . . . . . . . . . . . . . CHECK
(verify condition and security)
6. Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify condition and security)
208BPHCUS-004-14