Cessna 150 - SECTION II DESCRIPTION AND OPERATING DETAILS; FUEL SYSTEM.; FUEL STRAINER DRAIN KNOB.

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DESCRIPTION AND OPERATING DETAILS
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The following paragraphs describe the systems and equipn ::. ent who se
function and operation is not obvious when sitting in the airplane. This
section also covers in somewhat greater detail some of the items listo:_-d
in Check List form in Section I that require further expla uation.
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 c edure, 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
,