Cessna T188C - Table of Contents

MODEL
188
& T188
SERIES
SERVICE
MANUAL
SECTION 12
FUEL SYSTEMS
Page No.
TABLE OF CONTENTS
Aerofiche/Manual
FUEL SYSTEM ... .. 2A2/12-1 Inspection ....... .2A20/12-19
Description .......
. 2A2/12-1
Cleaning ........
2A21/12-20
Precautions
...........
2A3/12-2
Reassembly
.......
2A21/12-20
Trouble
Shooting
(Carbureted
Vented
Fuel Filler
Caps
Engine)
.... ........
2A3/12-2
(18803297
& ON) ....
2A21-12-20
Trouble Shooting
(Fuel-Injected
Description.
.... 2A21/12-20
Engine)
....
.
2A4/12-3
Inspection,
Cleaning
and
Fuel Vent
(Metal Tank)
..... 2A15/12-14
Repair
. .........
2A21/12-20
Description
2A15/12-14
Fuel Quantity
Transmitters
. .
2A21/12-20
Checking
....
....
. 2A15/12-14
Fuel Reservoir
.....
2A21/12-20
Fuel
Vents (Rubberized
Cell) ..
2A15/12-14
Description
.. ..
2A21/12-20
Description
....
....
.2A15/12-14
Removal
and Installation
.
. 2A21/12-20
Checking
........
2A15/12-14
Fuel
Strainer
(Metal
Tank) ..
. .2A22/12-21
Fuel Tank (Metal) ........
2A16/12-15
Description ........
2A22/12-21
Description
......
.2A16/12-15
Removal and
Installation
... 2A22/12-21
Removal and Installation . . 2A16/12-15 Disassembly and Reassembly 2A22/12-21
Fuel
Cells . .
........
2A16/12-15
Fuel
Strainer (Rubberized
Cell) . .2A22/12-21
Description
.........
2A16/12-15
Description
.........
2A22/12-21
General
Precautions
....
.2A16/12-15
Removal
and Installation
2B1/12-24
Removal
. ........
. 2A16/12-15
Disassembly
and Reassembly
.
2B1/12-24
installation
........
.2A18/12-17
Auxiliary
Fuel Pump ......
.2B1/12-24
Removal and
Installation of
Fuel
Description
........
2B1/12-24
Shut-Off Valve
(Metal Tank) .. 2A18/12-17
Removal and Installation
Removal and Installation of Fuel (Metal Tank) ... 2B1/12-24
Shut-Off Valve
(Rubberized Cell) . 2A18/12-17
Removal and Installation
Vented
Fuel
Filler Caps
(thru
(Rubberized
Cell)
......
2B1/12-24
18803296)
.........
.. 2A18/12-17
Electric Fuel
Pump Circuit
(A188
Description
.
.......
.2A18/12-17
Series)
........
.
2B2/12-25
Metal "Flush
Type" Filler
Description
.......
2B2/12-25
Caps
.
........
A18/12-17
Rigging
Throttle
Microswitch
. 2B3/12-26
Inspection
.....
2A18/12-17
Auxiliary
Fuel
Pump
Rate
Cleaning.
.
.. .2A18/12-17
Adjustment
........
2B3/12-26
Reassembly
....
.
2A19/12-18
Emergency
Boost
Check.
.. .2B3/12-26
Red Plastic
"Flush Type"
Priming System
......... 2B4/12-27
Filler Caps
. . ....
. . 2A20/12-19
Description
........
2B4/12-27
12-1. FUEL
SYSTEM. The
fuel system,
as defined
a remotely-controlled
drain
valve with the
control
by this manual,
is that portion
of the entire system
handle
located adjacent
to the oil
dipstick in the
en-
up
to and including
the fuel line connected
to the
gine
compartment.
Access to the
control handle is
engine driven
fuel pump. The Auxiliary
fuel pump gained through
the oil dipstick door in the upper
en-
and
the applicable
throttle rigging
procedures are
gine
cowling. The
fuel tank is vented
through an
covered
in this section.
overboard
vent line connected
to a fitting
in the filler
neck. Another fitting in the top of the tank is used
12-2.
DESCRIPTION.
On standard
fuel instal-
for the
vapor return
line on fuel-injected
engines,
lations, the fuel
supply is contained in a rigid
metal and is capped on
carburetor-equipped engines.
A
tank, enclosed In a plastic vapor barrier, and fuel quantity transmitter, located in the bottom of
mounted immediately behind the firewall in the air- the tank, is electrically connected to the fuel quantity
craft fuselage. The Specification Chart, figure 1-1, indicator, located in the instrument cluster panel in
gives
fuel capacities.
the cockpit.
The fuel
quantity indicator
is discussed
Fuel flows through a finger screen in the tank outlet in Section 15. Schematic diagrams are illustrated in
to
a shut-off valve,
through the fuel
strainer, to
the figure
12-1. System
details are illustrated
in suc-
carburetor.
On
fuel-injected
engines,
fuel flows
ceeding
figures.
from the shut-off valve, through an auxiliary electric
fuel pump,
through the fuel strainer,
to the engine- On optional
fuel system installation, cells
are
driven fuel pump.
The fuel strainer is equipped
with located in the wings,with
a reservoir between the cells
Revision
1
12-1