Section II
DESCRIPTION AND OPERATING DETAILS
The following paragraphs describe the systems and equipment whose
function and operation is not obvious when sitting in the airplane. This
section also covers in somewhat greater detail some of the items listed
in Check List form in Section I that require further explanation.
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 and
fuel strainer to the carburetor.
Refer to figure 2-2 for fuel quantity data. For fuel system service
information, refer to Lubrication and Servicing Procedures in Section IV.
FUEL STRAINER DRAIN KNOB.
Refer to fuel strainer servicing procedure, Section IV.
FUEL QUANTITY DATA (U.S. GALLONS)
TANKS
USABLE FUEL
ALL FLIGHT
CONDITIONS
UNUSABLE
FUEL
TOTAL
FUEL
VOLUME
TWO, STANDARD WING
(13 GAL. EACH)
22.5
3. 5
26. 0
TWO, LONG RANGE WING
(19 GAL. EACH)
35. 0
3. 0
38. 0
Figure 5-4.
5-1
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