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Cessna 182 - FUEL SYSTEM

Cessna 182
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1-27
FUEL SYSTEM
Fuel System Components
49. The aircraft fuel system consists of the following major components:
a. two bladder style vented fuel tanks;
b. vent system / check valve;
c. fuel quantity indicators for each tank;
d. rotary fuel selector valve;
e. fuel header tank;
f. fuel shutoff valve;
g. fuel strainer;
h. electric auxiliary fuel pump;
i. engine driven fuel pump;
j. fuel injection system; and
k. vapour return line.
Figure 1-32 Fuel System Components

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