CESSNA
SECTION 7
MODEL 162
NORMAL PROCEDURES
GARMIN G300
U.S.
PREFLIGHT INSPECTION
(Continued)
8
NOSE
1.
Engine Cooling Air Inlets - CHECK (clear of obstructions)
2.
Propeller and Spinner - CHECK (for nicks and security)
3.
Air Filter - CHECK (for condition and blockage by dust or other
foreign matter)
4.
Nosewheel Strut and Tire - CHECK (strut and general condition
of tire (weather checks, tread depth and wear, etc.))
5.
Nosewheel Fairing - CHECK (security and condition) (if
installed)
6.
Engine Exhaust Outlet - CHECK (security and condition)
7.
Engine Oil Dipstick/Filler Cap:
a.
Oil level - CHECK
b.
Dipstick/filler cap - SECURE (lever horizontal and facing aft)
NOTE
Do not operate with less than 3.5 quarts. Fill to 5 quarts
for extended flight.
8.
Fuel Strainer Quick Drain Valve - DRAIN (bottom left side of
engine cowling)
Drain at least a cupful of fuel (using sampler cup) from valve 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 and then gently rock wings and lower tail to
the ground to move any additional contaminants to the sampling
points. Take repeated samples from all fuel drain points,
including the fuel strainer and fuel sump valve, until all
contamination has been removed. If contaminants are still
present, refer to WARNING below and do not fly the airplane.
NOTE
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.
(Continued Next Page)
162PHUS-00
7-11
Содержание 162 SKYLANE
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