Cessna T182 1982 Pilot Operating Handbook page 157

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SECTION 7
CESSNA
AIRPLANE
&
SYSTEMS DESCRIPTIONS MODEL T182
FUEL QUANTITY INDICATORS
REDuCED
CAPACITY
STANDPIPE
V(;NT
VENT
~~~~~
I ....
,,~~.~~
. ~ .. ~ .. ~ .. :~ I ~~~tK
V .... · l Vll\ rF
DRAIN
RIGHT FuEL TANK VALVE)
VALVr.
~
lJ
l l
':1H'\li,(
n
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I (J,\:I All
I\l)Xllli\HV
rUi
L PUMP
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t
E
I
i~ON1IHJl.
~::==
9
1:
~~
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r-.'IXTltHr
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TO lNc"WtL f.,·tAXtMUM f U[ L
(:/.. 1')'\(.1 T Y Will
"j
HI lUI II
r~(,
"'1m M1NlM1/l CROSS Fl£OINt,
Wt11 rJ j'A.fH
11lWI A'IW
1••
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pv.n
THl fUrl
C)lLltIOH VAlVi. 1" I tTIH.H
If
r
I
fiJi
HHil1l P()\)I I lOtI
TO Ef\:",INE
•
CONDIT10"J
SYSTEM SHOWN ~"I r
II
FUEL SELECTon VALVE
IN UOTH POSITION.
10 lNGINl •
Flit: l
PRE.&$UA €
GAGE
(RIGHT HALF OF
II
DUAL INSTRUMENT)
CODE
FuEL SUPPLY
c=:J
VENT
c=:J
MECHANICAL
LINKAGE
ELECTRICAL
CONNECTION
Figure 7-6. Fuel System
7-26 2i August 1981