CESSNA
AIRCRAFT
COMPANY
MODEL
182/T182
WIRING
DIAGRAM
MANUAL
PART
NUMBER
1234567
NOMENCLATURE
JC023
S2350-10
S2353-5
PC1007
UG913A/U
PC1010
225559-2
PF1002
UG913A/U
PF1010
225559-2
PT1011
PT1012
PT1013
PT1014
PT1015
PT1016
PT1017
PT1018
PT1019
PT1020
PT1021
PT1022
PT1023
PT305
PT309
PT311
PT312
PT317
PT901
PT902
PV1002
UC1007
UC1010
UF1002
UF1010
UT304
UT307
UT901
S3284-1
S3284-1
S3284-1
S3284-1
S3284-1
S3284-1
S3284-1
S3284-1
S3284-1
S3284-1
225555-6
S3284-1
S3284-1
330-00185-44
330-00185-78
330-00185-44
330-00185-78
330-00185-44
03-06-1023
S2216-4
SK2701
FC120N2
S3284-1
C598501-0104
GARMIN
INTEGRATED AVIONICS
SYSTEM
18281318
&
ON
18208232
&
ON
.
CONNECTOR
.........................
.
CONTACT
.
CONNECTOR
ANTENNA
COAX
(ZONE
340)
....
.
CONNECTOR
.........................
.
CONNECTOR
COAX
(ZONE 210)............
.CONNECTOR
.........................
.
CONNECTOR
.........................
.
CONNECTOR
.........................
.
CONNECTOR
.........................
.
CONNECTOR
.........................
.
CONNECTOR
.........................
.
CONNECTOR
.........................
.
CONNECTOR
.........................
CONNECTOR
.........................
CONNECTOR
.........................
CONNECTOR
.........................
CONNECTOR
.........................
.
CONNECTOR
.........................
.CONNECTOR
.........................
CONNECTOR
.........................
CONNECTOR
.........................
CONNECTOR
.........................
CONNECTOR
.........................
CONNECTOR
.........................
.CONNECTOR
.........................
.
CONTACT
.CONNECTOR
........................
.
CONTACT
CONNECTOR
.........................
ANTENNA
COMM
(ZONE
210).....
ANTENNA
GPS
2..............
ANTENNA
COMM
(ZONE
210).....
ANTENNA GPS
1 ..............
INTEGRATED
AVIONICS UNIT
1
. . .
V00779
V00779
V00779
............
V27264
. .
.V28198
V28198
80001
80003
.
INTEGRATED
AVIONICS
UNIT
2........................
.
FAN
AVINONICS
COOLING
............................
-
ITEM
NOT ILLUSTRATED
©CESSNA
AIRCRAFT
COMPANY
34-60-01
01
R
01
R
01
R
01
R
01
R
01
R
01
R
01
R
01
R
01
R
01
R
01
R
01
R
01
R
01
R
01
R
01
R
01
R
01
R
01
R
01
R
02
R
01
R
01
R
01
R
RFR
RFR
03
01
R
RFR
RFR
RFR
RFR
Figure
01
Page
1
Mar 1/2004
FIG
REF
DES
01
EFFECTIVITY
FROM
TO
UNITS
PER
ASSY
01
01
01
01
R
R
R
R
............
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