Description And - Cessna 150 Owner's Manual

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Section II
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DESCRIPTION AND OPERATING DETAILS
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The following paragraphs describe the systems and equipn::.ent whose
function and operation is not obvious wh en sitting in the airplane. Thi s
section also covers in somewhat greater detail some of the items listo:_-d
in Check List form in Section I that require further explauation.
FUEL SYSTEM.
Fuel is supplied to the engine from . two tanks, one in each wing.
From these tanks, fuel flows by gravity through a fuel shutoff valve aml
fuel strainer to the carburetor.
Refer to figure 2-2 for fuel quantity data. For fuel system servke
information, refer to Lubrication and Servicing Procedures in Section IV.
FUEL STRAINER DRAIN KNOB.
Refer to fuel strainer servicing pro cedure, Section IV.
FUEL QUANTITY DATA (U.S. GALLONS)
USABLE FUEL
UNUSABLE
TOTAL
TANKS
ALL FLIGHT FUEL
CONDITIONS
FUEL
VOLUME
. TWO, STANDARD WING
22.5 3. 5
26.0
(13 GAL . EACH)
TWO, LONG RANGE WING
35.0 3.0 38.0
(19 GAL. EACH)
Figure 2-2.
2-1
,