CESSNA
AIRCRAFT
COMPANY
MODEL
182/T182
WIRING
DIAGRAM
MANUAL
7LE
L
/AVN
DISC
'AIRFRAME
REFER
TO
33-10-01
1--- I
-.
REFER
TO
UIOOB
REFER
TO
33-40-01
---
6
--*
23-50-01
--
9
RS
485
1
A 5 -fl---n
5P1037-2PC31(HT)-----
2
-
RS
485
1 B
6
--------
6P1037-3PC031BLU)-----
--
R70
~-l\- 4
--
L
REFER
TO
I--
34-10-01
RS
485
2
A
7
fl
7P107-7PCo31
WHT)
n
7
-"
RS
485
2
B
RBO
9BP1037-8PC031(BLU)>
8
-/
CONFIG
MOOULE GROUND
1
(BLK)(VEND
1
CONFIGURATION
CONFIG
MOULE
POWER
21-
RED)(VEND)
4 VM
ATUE
CONFIG
MODULE
DATA
40-((YEL)VEND)
3
-3
CONFIG
MODULE
CLOCK
60-
(WHT)(VEND)-2
/(
]
THERMOCOUPLE
REF
HI
6&--
(YEL)(VEND
|
THEROUPLE
0
1
(VED
THERMOCUPLE
L1SI
THERMOCOUPLE
REF
LO
69--
(RED)(VEND
ASSY
/'J
NO11
PN011
*I
EGT
SENSOR
DISC/
TEMP
ANALOG
IN
7
HI
48-
-8P1I037-+JNOI
(YEL)(24)-fllf-
(VENDf
TEMP
ANALOG
IN
LO
49-
PI037--JNO11(RED)(24)--H
((J-
VEND)--
_ QJ 2N2
EG
TSENSOR
DISC
TEMP
ANALOG
IN
8
HI
0--
IOP7-+JN012(YEL)(24)
+
(VEND
TEMP
ANALOG
IN 8 LO
5g1j
P
N2(RED)24)-i- -(VENSN
TEMP
ANAL
LO
53-----53PIO37--JNO13(RED)(24)-
-U-
(VEND)-
_n
/QJN014
PNO4
*4
EGT
SENSOR
DISC0
TEMP
ANALOG
IN
10
HI
54
-fi-54PI037-+JNO4I(YEL)(24)-fl-+f-f(VENDfl
TEMP
ANALOG
IN
1O 5
_
(VEND)-y
TEMP ANALWNLOG
5
LO
:I5P037--JNO1I(RED)(24)--J
4
I-(VENDO)--
Q
QJNO015
PN0]5
*5 EGT
SENSOR
01.C;
TEMP
ANALOG
IN
12
HI
58--658PI037-.JNOI0(YEL)(24)-fl-
l-(VEN
fl--
TEMP
ANALOG
IN
11
LO
59--5PI1037--JND16(RED)(24)-(VEND)--
/'
IJN
01
PNO1]
Q CGT
SENSOR
DISCc
TEMP
ANALOG IN
12
HI
526
--
6PI037-JNO17(YEL)(24)-fl
-'- (VEND
TEMP
ANALOG
IN 1
LO
27
1
-7PI037--JN017(RED)(24)-t
-U
-U-(VEND)
NJ
NO1
PN017
*2
CHT
SENSOR
DISC^
TEMP
ANALOG
IN
2
HI 2R
-2'8PIO037-+JN1T(YEEL)(24)-
(VEND"fI
TEMP
ANALOG
IN
2
LO
29
-29PI037--JND(RED
(2
4
)
.
(VEND)--
_M g/JN017
PN018
5
CHT
SENSOR
DISC/
8
TEMP
ANALOG
IN
3
HI
28-f-3PIOJ7-+JNO19(YEL)(24
)-
(VEND-iN
TEMP
ANALOG
IN
3
LO
2
7(PI0,37--JN01(RED)(24)
-(VEND)-U
_ 5
1
iNJN0O1
PNO19
3
CHT
SENSOR
DISCS
TEMP
ANALOG
IN
3 HlO
36--fi3P17-+JNO21(YEL)(24)-F
(VENDV--
-
TEMP
ANALOG
IN
3
LO
3-38IPI037--JN021
(RED)
(24)-J-l
(VEND)-L
*6
CH SENSOR
Di
I
TEMP
ANALOG
IN
6
HI
1
7>-f-17PIO37-+JNO22(YEL)(24
)
+-
-(VEN
TEMP
ANALOG
IN
6
LO
8
--
18PI037--JN22(RED)
(24){---V
(VEND)---
TEP
AALOG
IN
5
H37
21
L(24)V
TEMI,,P
ANALOG
IN
LO 59--~,5P
IO57--
JND21(RED)
(I4)
- -
NO)d-(VlrND
e6
CHTSENSOR
Is/,1
TEMP ANALOG
INN
6
HI
7---P;7*JNG22(YEL)(24)-VEN
TEMP ANALOG
6
LO
IR
a
--
N022(RED)(24)-'.
(VEN)
P
1037
GEA71
ENGINE/A
IRFRAME
PF003
VACUUM
PRESSURE
TRANSDUCER
UFOO3
Ul
00
VACUUM
PRESS ANALOG
IN
3
HI
42
42PI037-CPFO3---
C
OUTPUT
VACUUM
PRESS
ANALOG
IN
3
LO
43------P107-
P037-APFOO
A cGN
SIGNAL
GROUND
39
15PI037-BPFO03
-
INPUT
5V
45V
TRANSDUCER
POWER 15
15P1037-BJN004(20)
OIL
PRESSURE ANALOG
IN
2
HI
24--=
24PI037-CJN004(20)
OIL
PRESSURE
ANALOG
IN
2
LO
25-"
25P1037-AJN004(20)
TRANSDUCER
LO
(GND)
12
|UNi1
4EOR
| GT1
SENSOR
I-YE21
ENSORI
JN004
OIL
PRESSURE
TRANSDUCER
u..IOO6
B
INPUT
5V
C OUTPUT
A GND
I
L
TEi
SENSOR
OIL
TEMP
ANALOG
IN
1
HI
22---C:--
22P
1037-1UN004(20)
--
|
1
OUTPUT
OIL
TEMP
ANALOG
IN
1
LO
23---c==3--23P1037-GN004(20)
,UN011
O404)
JN009
PN009
IrUEL
FLOW
FUEL
FLO
TRANSDUCER
DISC
TRANSOUCER
*12V
TRANDUCER
POWER
16--16P-
16P17037-CJN009(20)
--
C-RED(VENO)-
INPUT 12V
FUEL
FLOW
DIGITAL
IN
1
2
--
2P1037-BJN009(20)
BII-
T(VEND)-
OUPUT
TRANSDUCER
LO
(GND)
13-
PI-3P1037-AJN009(20)-
A-- BLK(VEND)- GOND
.NE0T
ENISOR
UN
01
7
t
OV TRANSDUCER
POWER
*4
EGT
SENSOR
TACHOMETER
DIGITAL
IN
2
TRANSDUCER
LO
(GND)
I.NW
qENSOR
POWER
2
(AVN
BUS
1)
jUN
19
POWER
1
(ESSENTIAL
BUS)
1e6
EGT
SENSOR
POWER
GROUND
VOLTS-ESSNTL
BUS ANALOG
IN
5 HI
VOLTS-ESSNTL
BUS ANALOG
IN
5
LO
VOLTS-MAIN
BUS
ANALOG
IN
4
LO
VOLTS-MAIN
BUS
ANALOG
IN
4
HI
j
UN020
LOW
OIL
PRESS'
DISCRETE
IN
3
q
CHT
SENSOR
I
038
GEA71
ENGINE/AIRFRAME
y ?
IN021
CH
SENSOR
I CH
iENSOR|
1« CHT
SENSORI
1
CHPREMSOR
I
U1008
LH
FUEL
OTY
ANALOG
IN
2A
HI
LH
FUEL
OTY
ANALOG IN
2A
LO
*10V
TRANSDUCER
POWER
SIGNAL
GROUND
RH
RUEL
OTY
ANALOG
IN
3A
HI
RH
RUEL
OTY
ANALOG IN
3A
LO
SIGNAL
GROUND
'LOI
VOLTS'
RED
DISCRETE
IN
1A
ANALOG/CURRENT
MON
IN
1A
HI
ANALOG/CURRENT
MON
IN
1A LO
(MAIN
BATTERY
CURRENT)
ANALOG/CURRENT
MON
IN
2A
HI
ANALOG/CURRENT
MON
IN
2A
LO
(STANDBY
BATTERY
CURRENT)
45V
TRANSDUCER
POWER
ANALOG
IN
1A HI
ANALOG
IN
IA
LO
TRANSDUCER LO
IGND)
14
n
14P1037-2PN025(WHT)
nI
2
3
3PI1037-3PN0251(BLU)
3
11
11P1037-1PN025(ORN)
U|
1
\ Dna-
m
n.a
NOTES:
1.
ALL
WIRE
22AWG.
UNLESS
OTHERWISE
NOTED.
W
IRE
AND
CONNECTOR
SUPPLIED
WITH
SENSOR.
CONFIGURATION
MODULE AND
THERMOCOUPLE
ASSY
ARE
LOCATED
IN
THE
CONNECTOR
BACKSHELL.
/
GROUND
STUD
LOCATED
ON
LH
MAGNETO
CASE
LABLED
AS
'GND'.
\
*WIRE
SHIELD
TERMINATIONS
AND
CONNECTOR
BACKSHELL
GROUNDING
SHALL
BE
ACCOMPLISHEDBY
USING
GARMIN
BACKSHELL
GROUND
WIRE
HARNESS
('SPIDER').
Q
SOLDER
WIRES
TO
RESISTOR
AND COVER
WITH
HEAT
SHRINK
TUBING.
\
ASSEMBLE
0770582-3
FUEL
OTY
SIGNAL
CONDITIONER
(REF
DES
UL004
R
UR04)
IN
BUNDLE
AS
SHOWN:
COVER
-
TERMINAL
BOARD
,
,
:"~
."-'T',"J
.
=
'
.,;
TERMINAL
BOARD
* ..
,-:.- I,
. w
-
L ::::.:
:
:
...
UJ.L~
/,.;.
.
]
!,.
.
...
SHRINK
SLEVING
COVER
.OCOVER WALL
BET-EEN
R
&
R2.
%
COVER WALL
BETWEEN
RI
&
R2
PN025
TACHOMETER
SENSOR
UN028
INPUT *1OV
OUTPUT
GND
L
ELEfCB
PNL
ISyC|
E
003
-^~-.,s~
REFER
TO
30-30-00
HOURMETER
|REF4
E
---
REFER
TO
74-10-00
~~~~REFER
TO
J,
.-
4 ~l
---
4JCO24-(,)E1003----
()
REFER
TO
L
t RGND
24-61-0.
--
6 1
'
0
REFER
TO
I
37
G
37P1037-7JC024(16)
G1001
C0n5
35
--
35PI037-6JC024
(16
)G--I
JN005
20
20P1037-KGO1001
OIL
PRESSURE
46
"
46P1037-6JC024(16)|
R
p
SWITCH
SNOOI
4P
0
3
7P1037-R01I
F I
GNDE1003-AJN'005(20)Ae
41j_~r
5GIOO
-AJNOO$(20
)AIA
2
2SI
44
44P1037-4JC024
JGI0I-BJN005(20)
B I
0
--
I
76
---
Co476P1037-CJND05(20).C
_
'
GFOII
REFER
TO
5
1i
*--('6)_
LH
FuEL
07Y
SIGNALQF
T
G
F
91-10-02|
H
H
UL02
54
n
54P1038-3UL004(VH7T)
n
DR1;R2R3D21
LH
FUL
OTY
5S U
A
s55P1038-2UL002(BLU)
I I9 t
4 '499
1 ISV
ISENDER
14----------14P103B--I
UL004(WHT)
_ 8
4
L
UL004-1UL002
1
SEND
31
31PI038-2UL002(BLU;
I'
[,2
RETURN
_
2UL002-CLO10-
TIE
STRAP
(4)
TERMINAL
BOARD
FRONT
LAYOUT
(COVERS
NOT
SHOWN)
TERMINAL
BOARD REAR LAYOUT
(COVERS
NOT
SHON)
URQ04
'-2UL004
-GL010-4jl
GL010
RH
FUEL
OTY
SIGNAL/7\
REFER
TO
_
CONDT_ITINR_ASSY
-
91-10-02
56-
ni
56P1038-3URO04(WHT)
,
RI
R2RH
FUEL
OTY
57U
57P1038-2UR002(BLU)
I
I
SENDER
3n2
14P1038-10UR004(WHT)
--
_
!
-
4UR004-1UR0021
1
SEND
32
y
32PI
038-2UR002(BLU
y
-2
RETURN
1_0-BOX
DISC
LURO0CI2
GRa0R1
2UR004-aGRO1
D-I .GRO1O
60 0--P10=
-6PID38-APBO18
(20)-
A'
1
--
|
REFER
TO
44-.-44PIO34
8-FPB018(20)
FI
-ij-REFER
TO
24-20-01
91-10-02
4 5
1.0--G:145PIO,
8
-GR
20
[J) GLG.U--E
Q
INSTALL
H610033
NYLON
TUBE
BETWEEN
THERMOCOUPLE
WIRE
AND
CONNECTOR
CLAMP
AS
SHOW.
R13(5
I
PNL
DIS PC034ECTR
CLAP
J f c.~ PNLP
C6
^MANIFOLD
rCONNECTOR
CLA
46-46PI
-1
IJCO6'--
REFER
TO
7PRESSURE
/
H610033
TUBE
THERMICOUPLE
WIRE
47-47PO3-16
JC026---1
24-61-01
UN
00 6
/
15.
15P1038-BPC034
B
INPUT
5V
|
1 f
C
0770582C2
52
52P1038-CPC34
I C OUTPUT
5353P 1 038-APC03<j
A GND
~~~12__~
1-
2.0
ENGINE/AIRFRAME
MONITOR
Figure
01
(Sheet
1)
©
CESSNA
AIRCRAFT
COMPANY
P
1037
GEA71
ENGINE/
*1
EGT
*I
EGT
*2
EGT
*2
EGT
*3 EGT
*3
EGT
*4
EGT
*4
EGT
*5
EGT
*5
EGT
*6
EGT
.6
EGT
1*
CHT
el
CHT
*2
CHT
*2
CHT
*3
CHT
*3
CHT
'4
CHT
'4
CHT
*5 CHT
*5
CHT
*6
CHT
*6
CHT
77-40-01
Figure
01
Page
0
Feb
13/2006
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