Cessna 150 1968, Руководство пользователя

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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 i n Section IV.
FUEL STRAINER DRAIN KNOB.
Refer to fuel strainer servicing procedure, Section IV.
F UE L QUANTITY DATA (U. S. G ALLO N S)
USABLE FUEL
UNUSABLE
TOTAL
TANKS ALL FLIGHT FUEL
CONDITIONS
FUEL
VOLUME
1WO, STANDARD WING
22. 5
3. 5
26. 0
(13 GAL. EACH)
'fVIO, LONG RANGE WING
(19 GAL. EACH)
35. 0 3. 0 38. 0
Figure 2-2.
2-1