Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 236

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SECTION 4
NORMAL PROCEDURES
PREFLIGHT INSPECTION
7
RIGHT WING Leading Edge (Continued)
6. Pitot/Static Tube . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
7. Radome (if installed) . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
8. Wing Tiedown . . . . . . . . . . . . . . . . . . . . . . . . . . . DISCONNECT
9. Inboard Fuel Tank Sump and
External Sump Quick-Drain Valves . . . . . . . . . . . . . . DRAIN
Drain at least a cupful of fuel (using sampler cup) from each
sump location to check for water, sediment, and proper fuel
grade 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. Refer to Section 7, Airplane and System
Description, Fuel System Schematic for drain locations. If
contaminants are still present, refer to WARNING below and do
not fly airplane.
Collect all sampled fuel in a safe container. Dispose of the
sampled fuel so that it does not cause a nuisance, hazard
or damage to the environment.
If,
after
contamination still exists, the airplane should not
be flown. Tanks should be drained and system
purged by qualified maintenance personnel. All
evidence of contamination must be removed before
further flight.
10. Main Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
11. Main Wheel Tire . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(proper inflation and general condition (weather checks, tread
depth and wear, etc.))
4-18
(Continued)
(verify security, openings for stoppage and warmth)
NOTE
WARNING
repeated
sampling,
(check condition of gear and brakes)
U.S.
MODEL 208B 867 SHP
GARMIN G1000
(verify condition and security)
evidence
FAA APPROVED
208BPHCUS-00
CESSNA
of

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