SECTION 4
CESSNA
NORMAL PROCEDURES
MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
PREFLIGHT INSPECTION
(Continued)
8
NOSE
(Continued)
9. Cowling . . . . . . . . . . . . . . . . . . . . . . . . . . .
CLOSE and LATCH
(right side)
10. Propeller Anchor . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
REMOVE
11. Air Inlet Covers . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
REMOVE
12. Air Inlets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
CHECK
Check starter/generator blast tube opening and oil cooler inlet
(right) and engine induction air inlet (left) for condition,
restrictions, and debris.
13. Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
CHECK
Inspect blades for nicks, gouges, looseness of material, erosion
and cracks. Also, inspect blades for lightning strike (darkened
area near tips), boots for security, condition and evidence of
grease and oil leaks.
14. Propeller Spinner. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
CHECK
(verify condition and security)
15. Nosewheel Strut and Tire . . . . . . . . . . . . . . . . . . . . . . .
CHECK
Check condition, red over-travel indicator block and cable intact
(not fallen into view), and proper inflation of tire.
16. Air Conditioning Louvers (if installed) . . . . . . . . . . . . . .
CHECK
(clear of obstructions)
17. Cowling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
OPEN
(left side of upper cowling for access and check condition and
security)
18. Engine (left side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
CHECK
(verify general condition, security, fuel, no oil leakage, and no
damage to any components)
19. INERTIAL SEPARATOR Bypass Outlet . . . .
CHECK CLOSED
(verify duct free of debris)
(Continued Next Page)
208BPHCUS-00
4-20
Summary of Contents for Cessna Grand Caravan Ex 208B
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