CESSNA
AIRCRAFT
COMPANY
MODEL
182/T182
WIRING DIAGRAM
MANUAL
PART
NUMBER
1234567
NOMENCLATURE
PC024
S2349-3
S2099-1
S2099-2
S2099-3
S2099-4
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
PNO18
PN019
PN020
PN021
PN022
PN023
PN025
R1
6280-3SG-513
RN65E4990B
R2
RN65E4990B
R3
RN55C1001F
R1013
SN001
TI001
UC001
UF003
UI001
U1006
U1008
UL002
UL004
UN004
UN006
UN011
UN014
UN015
UN016
UN017
UN018
UN019
UN020
UN021
UN022
UN023
UN024
UN025
UN026
CCF-5525R5F
011-00981-00
S3370-1
011-00979-00
P165-5281
0770582-3
P165-5282
S2253
S2253
S2253
S2253
S2253
TE-12525-01
*
CONNECTOR
ELECTRICAL
CIRCUIT
BREAKER
PANEL
DISCONNECT (ZONE
220) ............................
CONTACT
CONTACT
·.
CONTACT
·.
CONTACT
*
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........
.CONNECTOR........
.
RESISTOR
..........
.............................
V023K3
.............................
.
RESISTOR
.......................................
.
RESISTOR
.......................................
.
RESISTOR
............................
.
SWITCH OIL
PRESSURE
(ZONE
120)..........
.
THERMOCOUPLE
.......................
.
TIMER/MONITOR
PROPELLER
DEICE
(ZONE
211)
.
TRANSDUCER
VACUUM
PRESSURE
.........
.
MODULE
CONFIGURATION
................
.
TRANSDUCER
OIL PRESSURE (ZONE
120)
..........
.
COMPUTER
ENGINE/AIRFRAME MONITOR
..........
.
TRANSMITTER
LEFT
FUEL
QUANTITY
(ZONE
510).....
.
SIGNAL CONDITIONER
FUEL
QUANTITY
............
.
SENSOR
OIL
TEMPERATURE (ZONE
120)
...........
.
TRANSDUCER
FUEL
PRESSURE
(ZONE
120).........
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
...........
PROBE
TIT (ZONE
120)
............
...........
V91637
...........
VOTRC3
...........
VOTRC3
...
V22863
...
V22863
-
ITEM
NOT ILLUSTRATED
©
CESSNA AIRCRAFT
COMPANY
FIG
REF
DES
EFFECTIVITY
FROM
TO
UNITS
PER
ASSY
01
01
01
01
01
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
RF
01
01
R
01
R
01
R
01
RF
01
01
RF
01
01
RF
RF
01
RF
01
RF
RF
RF
RF
01
RF
RF
RF
01
RF
01
01
01
01
81318
&ON
8232
&
ON
81318
&ON
8232
&
ON
81318
&ON
8232
&
ON
Figure 02
Page
3
Feb
13/2006
. . .
..................
..................
..................
..................
..................
..................
..................
...........
..................
..................
..................
..................
..................
..................
77-40-01