SECTION 2
CESSNA
AIRPLANE AND SYSTEM DESCRIPTION
MODEL 162
GARMIN G300
U.S.
FUEL SYSTEM
(Continued)
FUEL INDICATING SYSTEM
Fuel quantity is measured by two sight gages located in each wing root
just forward and above the cabin door opening. The sight gages are
vented and include orifice fittings at the top and bottom of the sight
tube. The fuel levels are aided with floating aluminum balls for
increased readability. There are two scales displayed on each fuel sight
gage. The aft scale shows fuel levels to be read in level flight. The
markings should not be relied upon for accurate readings during skids,
slips or unusual attitudes. The forward scale shows fuel levels as read
on level ground. Minimum takeoff is indicated when the center of the
ball is at the "MIN/TO" line on the forward scale in level ground attitude
which represents 3 gallons per side or 6 gallons total (1/4 tanks).
.
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FUEL QUANTITY SIGHT GAGE
Figure 2-2*
162PHUS-01
2-16
Summary of Contents for 162 SKYLANE
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