SECTION 4
NORMAL PROCEDURES
PREFLIGHT INSPECTION
4
LEFT WING Trailing Edge
1. Fuel Tank Vent Opening . . . . . . . . . . . . . . . . . . . . . . . . CHECK
2. Aileron and Servo Tab . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
3. Static Wicks (4 total) . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
4. Spoiler . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
5. Flap Leading Edge Vortex Generators . . . . . . . . . . . . . CHECK
6. Flap . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
4-14
(Continued)
U.S.
MODEL 208B 867 SHP
GARMIN G1000
(verify opening is clear)
(verify condition and security)
(verify condition)
(verify condition and security)
(verify condition and security)
(verify condition and security)
FAA APPROVED
208BPHCUS-00
CESSNA