Before Starting Engine - Cessna Grand Caravan 208B G1000 Manual

SECTION 4
NORMAL PROCEDURES
PREFLIGHT INSPECTION
If any water is detected in the fuel system, the inboard fuel tank sump
and external sump quick-drain valves, fuel reservoir quick-drain valve,
and fuel filter quick-drain valve should all be thoroughly drained until
there is no evidence of water or sediment contamination. If the airplane
is parked with one wing low on a sloping ramp, draining of the outboard
fuel tank sump quick-drain valves (if installed) is also recommended.
Prolonged storage of the airplane will result in a water buildup in the
fuel which "leaches out" the fuel additive. An indication of this is when
an excessive amount of water accumulates in the fuel tank sumps.
Refer to Section 8 for fuel additive servicing.
To prevent loss of fuel in flight, make sure the fuel tank filler caps are
tightly sealed after any fuel system check or servicing. Fuel system
vents should also be inspected for obstructions, ice or water, especially
after exposure to cold, wet weather.
The interior inspection will vary according to the planned flight and the
optional equipment installed. Prior to high-altitude flights, it is important
to check the condition and quantity of oxygen face masks and hose
assemblies. The oxygen supply system (if installed) should be
functionally checked to ensure that it is in working order and that an
adequate supply of oxygen is available.

BEFORE STARTING ENGINE

•
It is the responsibility of the pilot in command to
make sure that the airplane is correctly loaded
within the weight and center of gravity limits
prior to takeoff.
•
Failure to correctly use seat belts and shoulder
harnesses could result in serious or fatal injury
in the event of an accident.
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WARNING
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U.S.
CESSNA
MODEL 208B G1000
FAA APPROVED
208BPHBUS-00