Cessna 182 1978 - Fuel System

MODEL
182
& T182
SERIES
SERVICE
MANUAL
SECTION
12
FUEL SYSTEM
Page No.
Page
No.
TABLE
OF
CONTENTS
Aerofiche/Manual
TABLE
OF CONTENTS
Aerofiche/Manual
FUELSYSTEM
.....................
2D1/12-1
Removal/Installation
...........
2D17/12-17
Description
......................
2D1/1-12
Di
embly
...................
2D17/12-17
Precautions
.....................
2D112-1
Cleaning Inspection
Troubleshooting
..................
2D2/12-2
and
Repair
..............
2D17/12-17
Fuel
Cells
........................
2D11/1211
Reassembly
.
.............
1812-18
Description
....................
2D11/1211
Fuel
Strainer
....................
2D18/12-18
General
Precautions
...........
2D11/12-11
Description
...................
2D1812-18
Removal
......................
2D11/1211
Removal/Installation
..........
2D1812-18
Repair
........................
2D11/12-11
Dissembly/Assembly
.........
2D18/12-18
Installation
...................
2D11/12-11
Priming System
..................
2D23/12-23
Filler
Caps
.......................
2D11/12.11
Description
....................
2D23/12-23
Description
................
.... ................
2D11/12-12
Filler
Cap-Metal
...............
2D12/12.11
Auxiliary Electric
Fuel
Inspecti
..................
2D12/12-12
Pump(T182)
..................
2D2312-23
Cleaning
...................
2D12/12-12
Reassembly
.................
2D13/12.13
Cleaning
LSE
Fuel
Priming
System
(T182
Opt
.......
2D23/12-23
Filler Caps .................
2D14/12-14
Filler Cap-Red
Plastic
..........
2D15/12-15
Inspection...
..................
2D15/12.15
Description
......................
Cleaning ...................
2D15/12-15
Leak Classification
............... 2D23/12-23
Leak Testing Metal
or
Sealant
.........................
2D24/2-24
Red Plastic
Caps ...........
2D15/12-15
Fuel Quantity
Transmitter ........
Fuel Vents .......................
2D16/12-16
.................
-
Adjustment ...................
2D16/12-16
Fuel Selector
Valve ...............
2D17/2.17
Fuel Quantity
Transmitter
.......
12-1.
FUEL SYSTEM.
12-3.
al precautions and rules during fueling, defueling,
12-2. DESCRIPTION.
A rubberied
bladder-type
tank or
integral fuel
bay purging,
repairing assembly
fuel
(cell) tank, or and integral
fuel tank is located in
or diassembly
of system
the inboard
bay of each
ing. When the
fuel system is
system
checks and repairs
on the airplane
fuel system:
in operation,
depending
upon
the aircraft'
configura-
tion, gravity,
an electric or engine-driven
fuel pump,
draws the
fuel from the tanks
through the
tank strain-
er, a selector
valve,
fuel strainer,
electric
or engine
driven
fuel pump to the
carburetor. In
the 1977
During all
fueling procedures
fire fight-
through 1978
Models, system ventilation
is provided
ing equipment
must be available.
Attach
by vented
fuel cap and a vent line and check valve
ex- a round wire from approved
ground
tends from the
left wing tank and emerges through the
stakes to the mooring eyebolt on L
and
lower
wing
with
1979 Models, a vent line
and check valve is also
and RH wings. Ground fuel
nozzle to air-
used on the right wing tank. The forward fuel lines plane during fueling operations.
from the right and
left tanks are also utilied
as vapor
return line and are teed into a tank crossover
vent a. Plugs or cap should
be placed on all discon-
line connected
to the right and left vent
lines. The fuel
nected hoses, lines
and fittings to prevent
reid-
strainer
has a quick-drain valve
on the bottom of the
ual fuel drainage,
thread damage, or entry
of dirt
bowl and is used to remove
water and sediment
from
or foreign material
into fuel system.
I the system. Fuel sump
drain valves (one in
each tank)
re located in the bottom,
inboard end of each
fuel tank
and are provided
for draining trapped
water and sedi-
ment. Integral fuel tank equipped aircraft 18265176
and On,
incorporating
SK182-100
have
four
additional
quick-drain valve installed in each fuel bay.
Revision 3 12-1