CESSNA
AIRCRAFT
COMPANY
MODEL
182/T182
WIRING
DIAGRAM
MANUAL
P1037
GEA71
ENGINE/AIRFRAME
RS
4
RS
4
CONFIG
MODULE
CONFI
G
MOUL
CONFIG
OODUI
CONFIG
MODULI
THERMOCOUPLE
THERMOCOUPLE
1*
EGT
TEMP ANALOG
*1
EGT
TEMP ANALOG
*2
EGT
TEMP
ANALOG
I
*2
EGT
TEMP ANALOG
I
03
ECT
TEMP
ANALOG
*3
EGT
TEMP
ANALOG
I
.4
EGT
TEMP
ANALOG
II
*4
EGT TEMP
ANALOG
II
*5
EGT TEMP
ANALOG
IF
.5
EGT TEMP
ANALOG
II
*6
EGT
TEMP
ANALOG
II
*6
ECT
TEMP
ANALOG
II
*I
CHT
TEMP ANALOG
R1 CHT
TEMP ANALOG
*2
CHT
TEMP
ANALOG
.2
CHT
TEMP ANALOG
.3
CHT
TEMP
ANALOG
93
CHT
TEMP
ANALOG
*4
CHT
TEMP
ANALOG
4
CHT
TEMP
ANALOG
*5
CHT
TEMP
ANALOG
*5
CHT
TEMP
ANALOG
#6
CHT TEMP ANALOG
*6
CHT TEMP
ANALOG
PC031l
J
dC0
1
ELECT/AVN
D
1
C
REFER
TO
33-10-01
---
I
--
,LREFER
TO
UIOOB
REFER
TO
33-40-01
#---
6
-
23-50-01
g
RS
485
1
A S
5P1037-2PC031(WHT)----
-2
-'
RS
485
1 B
--
6P1037-PC031(BLU)----3
- E
'-
4
--
EL
REFER
TO
LUj
34-10-01
s85
2
A 7 -f---
7P1037-7PC031(WIHT
45
2
B
-
7
-
BPO037-BPCO31(BLU1
GROUND
1
---
(BLK)(VEND
)--
I
CNF
EPOWER
21
-
RED)
VEND)4
IOi
.E
DATA
40-(YEL
VEND)3
E
CLOCK
60
-----
(HT(vEND--
2
t
REF
HI
6--
(YEL)(VEND)--
TIOUPLE
/
THERMOCOUPLE
REF
LO
69
-
RED)(VEND
AS)-
I
/JNOII
PN011
*I
EGT
SENSOR
D1SC.
IN 7
HI
A
IN
7
LO
4S-i49P1037--JNOII(RED)(24
t
()-U--
VEND)-
/'IJN012
PN0]2
2
^
EGTSENSOR
D15C
IN
HI 50
n-oPI037-+JON12(YEL)(L24)
(END-f
IN
LO
51J-IPIO37--JNOI2(RED
)(24)L
(VEND)
_I Q
JN013
5PN
5O
*3
EG
SENS
DIRSC
IN
9
HI
52-ft-52P1037-+JNO13(YEL)(24H
(VENDn'-f
IN
9
LO
53--53PI37--JN13(RED)
(24)-U|-i
VEND)
1
_ \
QiSJN014
PN014
*4
EGT SENSOR
OISC
N
10
HI
54
-f-54P0I37-+JN0I4(YEL)24
-
(VEND
N
0
LO
55
y-55PI037--:JND4
(RED){24
)
j-
(VEND)'-
N
11
0LO
57IIOJ7--JNOI
RED
(.EJ
/'nJN015
PN01
5
s Q
EGT
SENSOR
DIDSC
1
56I B
P
1 5
037-+JNO15(YEL(
24)--In-t
(VEN
11
LO
579
7PIDo37--JNO
I
5(RED)i24)-flJ}IVEND)-
Q
GA
JNI
OC.HTSENSORDI5C
N
12
HI
5-
IOP037-+JND16(YEL)(24)-A-IT
1
-(VENOfl-
I
12
LO
59
-
PIO37--JN016(RED)
(24)-
-(VEND)-
/iJN017
PN017
1l CHT SENSOR
DISC
IN
H
26-26PIO37-+JNO7(
YEL)(
24)
(VEND--
2
1
24
L
VEN
IN 2
LO
2927PIOJ7--JNO1
R7(NE(24
VEND)
2
CHTSENSOR
DISC
I
IN
2
HI
25--2PIO37-+JNOIB(YEL)24
-
VENDf
IN
2
LO
29-29PI57--JNO(REDI(24
(VEND
/gJN019
PNO19
J.CH2SENSOR
DI
IN
4
HI
30
33P:1037-+JN019(YEL)
(24)-fRT-f
(VEND-l-
IN
4
LO
314J31PIO37--JNOi2(RED)I24)-U-
---
(VEND)
I:N 3 LO ^
Bp
lJiDPvND'N
IN
4
HI
3.-fj-7PI1037-+JNO2O(YEL)(24
)-f--(VEN
IN
4
L
J4'y34PID37--JNO2OIREOD()
2 4
-
---
V£ VND)I
i/JN021
PN021
e5
CHT SENSOR
DICSC
IN
5
HI
36--36PIO7-JND21(0
YEL)(24)-
-I-I-(VEND'
IN
5
LO
36013BPIO
37--JNO21(RED)
(24
(VEND)---
IN
6
HI
17--17P107-+JN022(YE24
4SE
VEND.
IN
6I
17
-17PIO37-JNO22(YEL)
24(VEN
IN
6
LO
8e~?&PIO37--JNO22(RED)24)--t-Vt
(VE)-
1e1
EGT
SENSOR
I.t
lENSOR
I.EGT
ENSOR
JUNE0
1E7NsO
164 ECT
SENSOR
|
2CH?'ENSOR
E2 CHSENSOR
.LC
ENSOR
I|N2O
5
1
CHT
SENSOR
| H
YNi2~OR|
P
1037
GEA71
ENGINE/AIRFRAME
PF003
VACUUM
PRESSURE
TRANSDUCER
UF003
U100
VACUUM
PRESS
ANALOG
IN
3
HI
42
42P1037-CPF03
C
OUTPUT
VACUUM
PRESS
ANALOG
IN
3
LO
4-
-----
43P1037-APF---
A GN
SIGNAL
GROUND
3
---- 15P
10
37-BPFO
B
INPUT
SV
+5V
TRANSDUCER
POIER
1
15P1037-BJN004(20)
OIL
PRESSURE
ANALOG
IN
2
H
24----
24P1037-CJN0D4(20)
OIL
PRESSURE ANALOG
IN
2
LO
25.-
25P1037-AJN004(20)
TRANSDUCER
LO
(GND) 12
JN004
OIL
PRESSURE
TRANSDUCER
U1006
B
INPUT
5
C
OUTPUT
A GNO
I
MNLO.tP
SENSOR
OIL
TEMP
ANALOG
IN
1
HI
22--C---
22P1037-1UNO04(2)-----
I
OUTPUT
OIL
TEMP
ANALOG
IN
1
LO
23P---I=--23P37-GN04
(20
U--N1
IUN011
O^A
JN009
PNn09
FUEL
FLOW
N1004
4
FUEL
NFLOW
9
TRANSPUCE
2ISC
ITRANSDUCER
T12V TRANDUCER
PO ER
16
I16PI037-CJN009(20)T
C
IED(VEND)--
INPUT
12V
FUEL
FLOW
DIGITAL
IN
1
2
-
2P1037-BNO009(20)
8
T(VEN)---
OUPUT
TRANSDUCER
LO
(1GND)
1
--
1--
3P1D37-AJNOO9(20)
A
LK(V
END)-
01
*1OV
TRANSDUCER
POWER
14
14P1037-2PNO25(WHT)
TACHOMETER
DIGITAL
IN
2
3
3PI037-3PND25(BLU)
TRANSDUCER
LO
(GND)
11
11P1037-1PNO25(ORN)
P C 4
PNJC024
PEL
0
4C
PNLE
ISC
REFER
TO
IJIL
24-61-01
POWER
2
(AVN
BUS
12 3737P1037-7JCo2416---
POWER 1
(ESSENTIAL
BUS)
35
35P1037-6JC02416
POWER GROUND
2C
20PO037-KGI001
VLTS-ESSNTL
BUS ANALOG
IN
S
HI
46-
46PI37-6JCO24(16)
VDLTS-ESSNTL
BUS ANALOG
IN
5
LO
47
7P1037-RGIOOI
VOLTS-MAIN
BUS
ANALOG
IN
4
LO
45
--
VOLTS-MAIN
BUS
ANALOG
IN
4
HI
44
44PI037-4JC024
LOW
OIL
PRESS'
DISCRETE
IN
3 76---
1
038
---
16_
GEA71
ENGINE/AIRFRAME
.R
TD
UIOD8
LH
FUEL
OTY
ANALOG
IN
2A
HI
LH
FUEL
OTY
ANALOG
IN
2A
LO
41OV
TRANSDUCER
POWER
SIGNAL
GROUND
NOTES:
1.
ALL
WIRE
22AWG.
UNLESS
OTHERWISE
NOTED.
WIRE
AND
CONNECTOR
SUPPLIED
WITH
SENSOR.
CONFIGURAT ION
MODULE
AND THERMOCOUPLE
ASSY
ARE
LOCATED
IN
THE
CONNECTOR
BACKSHELL.
GROUND
STUD
LOCATED
ON
LH
MAGNETO CASE
LABLED
AS
GND'.
\
WIRE
SHIELD
TERMINATIONS
AND
CONIECTOR
BACKSHELL
GROUNDING
SHALL
BE
ACCOMPLISHEDBY
USING
GARMIN BACKSHELL
GROUND
WIRE HARNESS
('SPIDER').
/
SOLDER
WIRES
TO
RESISTOR
AND
COVER
WITH
HEAT
SHRINK
TUBING.
/Q
ASSEMBLE
0770582-3
FUEL
OTY
SIGNAL
CONDITIONER
(REF
DES
ULOD4
A UROD4)
IN
BUNDLE AS
SHOWNs
COVER
-
TERMINAL
BOARD
LT f^
T-
-
: r
-TERMINAL
BOARD
C.' ! **
l .! , '.
' i.' .
SHRINK
SLEVING
COVER
-COVER
WALL
BETWEEN
R1
&
R2
PN025
TACHOMETER
SENSOR
UNO28
12
INPUT .1V
3
OUTPUT
I
GND
,--- REFER TO
30-30-00
|OU
ER
'.---,-
REFER
TO
74-10-00
s
--
-----
4JC024-(+)E,1003
----
I
54
n
54P1038-3UL0o04(WHT)
55-Yia
55P1038-2ULDO2(BLU)
14---P-14
3-10UL004(HT)
31
31PI038-2UL002(BLU)
__ ~ 4I3
RH
RUEL
OTY
ANALOG
IN
3A
HI 56
56P1038-3UR004(WHT)
RH
RUEL OTY
ANALOG
IN
3A LO
57
57P103B-2UR002(BLU)
Q-
-
----
14PI038-lo0URO
04
(HT
SIGNAL
GROUND
32
32P1038-2UR002(BLU)
PBO1.x
LON VOLTS' RED
DISCRETE
IN
IA
60-
---
60P1038-APB016(20)---
ANALOG/CURRENT
MON
IN
1A
HI
44
--
*44PO
138-FPBO18(20)
ANALOG/CURRENT
MO
IN
IA
LO
4
45PI038-GPB018(120)
-----
I
(UAIN
BATTERY
CURRENT)
R-vIDw1j
J
9
CC0H 6
P
C?6P034
Rmo113/ ~
StI
CH
PNL
DISC
MANIFOLD
ANALOG/CURRENT
MON
IN
2A
HI
46-
46PI038-11
JC026--
-
REFER
TOTRANSUCER
ANALOG/CURRENT
MON
IN
2A LO
47-
47P1038-16JC026
-
1
-
24-61-01
UNDO
(STANDBY
BATTERY
CURRENT)
*5V
TRANSDUCER
POWER
15-
15P1038-BPC0O34B
INPUT
5V
ANALOG
IN
1A
HI
52
52P1038-CPC034
C
OUTPUT
ANALOG
IN
1A
LO
53--1-
-
53P 1038-APC034
A GND
TRANSDUCER
LO
(GND)
12-
TERMINAL
BOARD FRONT
LAYOUT
(COVERS
NOT SHOWN)
TERMINAL
BOARD
REAR
LAYOUT
(COVERS
NOT SHMON)
LQ
INSTALL
H610033
NYLON
TUBE
BETWEEN
THERMOCOUPLE
WIRE
AND
CONNECTOR
CLAMP
AS
SHOWN.
CNNECTOR
CLAMP
[C/
ON
/
/-H610033
TUBE
/
THERMOCOUPLE
WIRE
-
..
2
0770582C2
I!
-------
2.0
---
ENGINE/AIRFRAME
MONITOR
Figure
01
(Sheet
1)
©
CESSNA
AIRCRAFT
COMPANY
77-40-01
Figure
01
Page
2
Feb
13/2006
GFI
o
91-10-6_
m
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