Cessna 182 1978 - Page 302

MODEL
182 & T182 SERIES
SERVICE MANUAL
FUEL QUANTITY INDICATORS
REDUCED
r
-REDUCED
CAPACITY
STANDPIPE - FILLER
CAP ,
FUEL QUANTITY
TRANSMITTERS
-r. . T .. . .
~~~~CHECK :::: ::.: : .. """"""--
--
:
;~~~~~~
-1 ..
~
:.
: .-
~-- ~..-- : .fi^ . ....
;..:- .: :-:.:-.:.I CHECK
RVALVE RGHT FUEL TANK DRI : FUEL SELECTOR . ,LEFT FUEL TANK VALVE!
Mj~i
iiiutL
iiaMK
~DRAIN
::
VALVE
§iiii
DRAIN
VALVE .. :. VALVE
RIGHT FUEL TANK VAE L
IKU~~
~
CONDITION:
DRAIN VALVE
SYSTEM
SHOWN
WITH
!UEL PUPFUEL SELECTOR VALVE
SWIT~FUEL
CHI
IIN
BOTH
POSITION.
STRAINER
DRAIN
CONTROL
: ^
MANUAL
I
ENGINE
SWIC P E SU EPRIMER
OPT.)
GAGEO__(STD.)
ENGINE
AUXILIARY
'
FUEL
PUMP
AUXILIARY
SWITCH
FUEL
PUMP
ELECTRIC
FUEL
PUMP
PRIMER
( )
rC
FUEL
SWITCH
_
-|
|
|
|
PRESSURE
IOPTS.)
SOLENOIDM
U
FE
LI KGAGE
VALVE
i
i
T
(RIGHT
HALF
OF
~
,
. ... .....
.:... . .DUAL
INSTRUMENT)
TO
ENGINE
THROTTLE
S
CODE
CONTROL - C
SU_ RCCARBURETOR
PC
FUEL SUPPLY
MIXTURE Q _
- --
I I VENT
CONTROL \0 / (
MECHANICAL
LINKAGE
TO ENSURE MAXIMUM FUEL LINKAGE
CAPACITY
WHEN REFUELING
TO
ENGINE
AND MINIMIZE CROSS-FEEDING CONNECTION
WHEN
PARKED ON A SLOPING
CNNCTN
SURFACE. PLACE THE FUEL
SELECTOR
VALVE IN
EITHER
T182
BEGINNING
WITH
LEFT
OR RIGHT POSITION.
1983 MODELS
Figure
12-1. Fuel System Schematic
(Sheet 4 of
4)
12-6