CESSNA
AIRCRAFT
COMPANY
MODEL
182/T182
WIRING
DIAGRAM MANUAL
PART
NUMBER
1234567
NOMENCLATURE
EFFECTIVITY
FROM
TO
PC026 S2349-1
S2099-13
S2099-3
S2099-4
S3373-2
PC031
S2349-3
S2099-2
S2099-4
PC034
S2800-277
PF003
AEKTKSAD0404
P1037
P1038
PN009
PN011
PN012
PN013
PN014
PN015
PN016
PN017
PN018
PN019
PN020
PN021
PN022
PN025
R1
6280-3SG-513
RN65E4990B
R2
RN65E4990B
R3
RN55C1001F
R1013
SN001
TI001
UF003
UI001
U1006
U1008
UL002
UL004
UN004
UN006
UN011
UN014
UN015
UN016
UN017
UN018
UN019
UN020
UN021
UN022
UN023
UN024
UN025
UN028
UR002
UR004
CCF-5525R5F
011-00981-00
011-00979-00
P165-5281
0770582-3
P165-5282
S2253
S2253
S2253
S2253
S2253
0770582-3
.
CONNECTOR
SWITCH
PANEL
DISCONNECT
...............
.
CONTACT
.
CONTACT
.
CONTACT
.
CONTACT
.
CONNECTOR
ELECTRICAL/AVIONIC
DISCONNECT
(ZONE
220)..
CONTACT
ALT FOR
S2099-4
.
CONTACT
.
CONNECTOR
KIT
..................................
.
CONNECTOR
KIT
..................................
.CONNECTOR
.....................................
.CONNECTOR
.....................................
.
CONNECTOR
FUEL
FLOW DISCONNECT
.................
CONNECTOR
......
CONNECTOR......
CONNECTOR......
CONNECTOR......
CONNECTOR......
CONNECTOR......
CONNECTOR......
CONNECTOR......
CONNECTOR......
CONNECTOR......
CONNECTOR......
CONNECTOR......
CONNECTOR......
RESISTOR
........
...............................
V023K3
...............................
RESISTOR
......................................
RESISTOR
......................................
RESISTOR
......................................
V91637
SWITCH
OIL
PRESSURE
(ZONE 120)
.....................
THERMOCOUPLE
..................................
VOTRC3
TRANSDUCER
VACUUM
PRESSURE
....................
MODULE
CONFIGURATION
...........................
VOTRC3
TRANSDUCER
OIL
PRESSURE
(ZONE
120)
...............
.V22863
COMPUTER ENGINE/AIRFRAME
MONITOR
................
TRANSMITTER
LEFT
FUEL
QUANTITY
(ZONE
510)...........
SIGNAL
CONDITIONER
FUEL
QUANTITY
..................
SENSOR OIL
TEMPERATURE
(ZONE
120)
.................
TRANSDUCER
FUEL
PRESSURE
(ZONE
120)
...............
V22863
.TRANSDUCER
................
PROBE
CYLINDER HEAD
1
EGT
....
PROBE
CYLINDER HEAD
2
EGT
....
PROBE CYLINDER
HEAD
3
EGT
....
PROBE CYLINDER
HEAD
4
EGT
....
PROBE
CYLINDER
HEAD
5
EGT
....
PROBE CYLINDER
HEAD
6
EGT
....
PROBE
CYLINDER
HEAD
1
CHT
....
PROBE CYLINDER
HEAD
2
CHT
....
PROBE
CYLINDER
HEAD
3
CHT
....
PROBE
CYLINDER
HEAD
4
CHT
....
PROBE
CYLINDER HEAD
5
CHT
....
PROBE#6
CHT
SENSOR
.........
SENSOR
TACHOMETER
.........
TRANSMITTER
RIGHT
FUEL
QUANTITY
(ZONE
610)..........
.
SIGNAL CONDITIONER
FUEL
QUANTITY
..................
-
ITEM
NOT ILLUSTRATED
©
CESSNA AIRCRAFT
COMPANY
FIG
REF
DES
UNITS
PER
ASSY
B1318
&ON
8232
&
ON
81318
&ON
3232
&
ON
B1318
&ON
3232
&
ON
01
02
02
09
02
01
01
01
01
01
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
RF
01
01
R
01
R
01
R
01
RF
01
RF
01
01
RF
RF
01
RF
01
RF
RF
RF
RF
01
RF
RF
RF
01
RF
01
01
01
RF
RF
01
Figure
01
Page
3
Feb
13/2006
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I
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77-40-01
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