Cessna TR182 1979 Pilot Operating Handbook page 156

SECTION 7
AIRPLANE
&
SYSTEMS DESCRIPTIONS
CESSNA
MODEL TR182
FUEL QUANTITY INDICATORS
DRAIN
VALVE
RIGHT FUEL TANK VALVE)
CONDITION:
SYSTEM SHOWN WITH
FUEL SELECTOR VALVE
IN BOTH POSITION.
FUEL
STRAINER
DRAIN
CONTROL
0------
TO ENGINE •
AUXILIARY
FUEL PUMP
AUXILIARY
D/
FUEL PUMP
SWITCH
ENGINE~DRIVEN
FUEL PUMP
FUEL
PRESSURE
GAGE
THROTTLE
CONTROL
0 _- --
--
MIXTURE
CONTROL
CARBURETOR
CODE
TO ENSURE MAXIMUM FUEL
CAPACITY WHEN REFUELING
AND MINIMIZE CROSS-FEEDING
WHEN PARKEDONA SLOPING
SURFACE. PLACE THE FUEL
SELECTOR VALVE IN EITHER
LEFT OR RIGHT POSITION.
TO ENGINE
VENT
I::;{::::}}:/:i
FUEL SUPPLY
MECHANICAL
LINKAGE
ELECTRICAL
CONNECTION
Figure 7-6. Fuel System
7-28 1 October 1978