Cessna 208B - Page 109

CESSNA SECTION 4
MODEL 2088 (675 SHP)
NORMAL PROCEDURES
I
PREFLIGHT INSPECTION (Cont~nued)
LEFT WlNG Leading Edge (Continued)
7. Fuel Quantity - VISUALLY CHECK. See Figure 4-2 for fuel
quantity versus depth if using Universal XL Fuel Gage.
8. Fuel Filler Cap - SECURE.
9. Outboard Fuel Tank Sump Quick-Drain Valve (if installed and
airplane parked with one wing low on a sloping ramp)
- DRAIN
(using fuel sampler) to check for water, sediment and proper fuel
before each flight and after each refueling. If water is observed,
take further samples until clear. Take repeated samples from all
fuel drain points until all contamination has been removed.
10.Navigation and Strobe Lights - CHECK for condition and
cleanliness.
@LEFT WlNG Trailing Edge
1. Fuel Tank Vent - CHECK for 0bst~~tionS.
2. Aileron and Servo Tab - CHECK condition and security.
3. Static Wicks
- CHECK condition.
4. Spoiler - CHECK condition and security.
5. Flap
- CHECK condition and security.
(Continued Next Page)
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( Revision 23
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U.S. 4-9