Left Side - Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual

CESSNA
MODEL 208B 867 SHP
GARMIN G1000
PREFLIGHT INSPECTION
2

LEFT SIDE

1. Wing Light. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
2. Fuel Reservoir Quick Drain Valve (located on
bottom of fuselage or left side of cargo pod) . . . . . . . . . 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.
3. Main Landing Gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
4. Main Wheel Tire . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(proper inflation and general condition (weather checks, tread
depth and wear, etc.))
FAA APPROVED
208BPHCUS-00
(Continued)
NOTE
WARNING
repeated sampling,
(check condition of gear and brakes)
(Continued Next Page)
SECTION 4
NORMAL PROCEDURES
(verify condition)
evidence
U.S.
of
4-9