Textron Cessna 182S - Page 372

CESSNA AIRCRAFT
COMPANY
MODEL 182/T182
WIRING DIAGRAM MANUAL
H1016
ELECT BUS I
FUELP
1
0
'P
1
2
2H1025-IPCO25(20)
BEACONI
026 T 1'
2HIO26-2PC025(18)
BEACHIO IGHT
LANDING
LILHT
'0
2HI027-3PCO25(14)
LANDING LIGHT 10
HI015 rs;"
AVIONIPS5 1"5 2H1023-4PC025(14)
CABINH
LTP
R
/P
FLAs
7
f
' H I 021
CROSSFEE0 BUS
~CROSSFEl B~~US
2H1015-1PC024(20)
J I
2HI015-2PC024
REFER TO 24-20-01 1-(10)-- :
1
---
HIO016-2DO010 (14)- D 1001
2H1007-3PCO24(1)6
2D11007-H1i016(14
.
-
I
-1
1
H 1014
ALW r. IELP
D "
2
22HI010-15PC025--
ELECT BuS 2 H 1022 2j P 2H1022-4PC024
2ARNIYG S- 2H I022-14PC0 25(20)
REFER TO
24-20-01 -- (10)--- -
HIOD4-2DI002(14)--f1
2----
0D1006-HI014(141
I
I
D I002
DIOO6-HIO102114 Q D 1 002 2H 1003-9PCO24
TAX 1 OL ?HIT024
AV I DN ICS 2 1
TAI LIGHT'
l
HNAI
OLGT
I A
2HI024-5PCO25(14)
S
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rS>
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nAITTv. HT
1's--
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uH
mI
011
12H1029-7PC025(20)
STROBDE
L TS'
2H1031-8PC025(20)
H1032 - -
2HIO02-9PC025(18)
PITOT HEAT 1
HI 01 .1 . 2HI01-1OPCO25(14)
PROP
2D
2HIO34-11PC025(14)
HEAT
- R REFER
TO
24-20-01
HI020
ESSENTIAL BUS
r
D 1006Q1
H51UI034
I
--
2
2H1022-22PC023
SIANDBY BATT
3
2H1022-23PC023
SwNOBY
HI INOLS-
1t
2
2H1035-5PC024
HPFD36
1
0
2
2H0I36-1PC023
H 037
'1 ,
2H1037-2PCO23(18)
ADC/AHRS 10 2H1037-3PCO23(18)
NHAVI/l3x
8
I2H1038-6PC024 (16)
HNAV/ENG
'IA
2MH1038-4PC023(16)
H
1039
1 ?
2HIO39-SPCO23(20)
Comm I BO 8
:: . l0071/
H1018
AVN
U1
I
III018-12PC025(14)
8Hinitn
ln10't.0 ~2H1040-7PC024(16)
NAY
T9EIQ
"W•
2H1040-6PC025(16)
1tnA~v ~I/E)I 1A/ 2H1041-6PC023(16)
AOCPAHRS
O
2HIO 4-8PCO23(18)
2HID041-PC023(18)
Po
2H1042 H42-9PCO23
HTIO943
I't
2
2H I043-10PCO23
TAS
(OPTION)
2H1044-11PCO23
FIS
(OPTION)
I
2HI045-12PC023
(OPTION)
2HI046-13PC023
HI019
AVN
0B
1
2
H1019-13PC025(14)
j~~H104~~um~~~~ °^2H1047-15PC023
AUTO PILOT
k5
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HPORA
vi
2
2H1048-17PC025
HUI
409 10t4
2
2H1049-18PC023
IH050 '1,2
2H1050-19PC023(20)
H1051 rt?
2
2H1051-20PCO23
H ID52 I
1
?.
2IO052-21PCO23
CIRCUIT BREAKER
PANEL
Figure 05 (Sheet 2)
CBP 2, P1-,O .-- c
2 ----
3
------
- REFER TO SHEET 4
4 ----- ;
---- 15 -- P--
ELET1
CR PNL-
R
I .----.
REFER
TO 24-50-01
2 ---- .REFER TO 33-11-02
3 ------ REFER
TO 27-50-01
4 ----
t REFER TO
77-40-01
5
----. REFER
TO 33-10-01
6 ----
t REFER TO
77-40-01
7
---- REFER
TO 77-40-01
8 -----
REFER TO 33-10-01
9 -----
REFER TO
33-10-01
6----,
7 ---- '
7 ....
8 ---- e
19
'--
-REFER
TO
SHEET
11 -----
12 ----
13
.-----
PCO2& PLJCWOC23
AV PNL DI
22
---- REFER
TO 25-60-01
23
---- PREFER
TO 22-10-04
24
1
2
3
4
5
NOTES:
1. ALL
WIRE 22AWB, UNLESS
OTHERWISE NOTED.
/ CAP AND STOW WIRE WHEN OPTION IS NOT
INSTALLED.
; INSTALL
PROTECTIVE
TUBING OVER DIODE
AS SHORW:
_ F
I
^SHRINK SLEEVE
(M23053/5 REF)
OTY 2
4 USE HIGH CURRENT CONTACTS (REF 53373-X).
Q ROUTE ALL WIRES
CLEAR
OF R1010
RESISTOR BY AT
LEAST
0.5 INCH.
RESISTOR MAY GET
HOT.
4
----- REFER TO 31-60-01
----- REFER TO 34-21-01
.--- REFER
TO
34-21-01
----
(REF NAV 1)
----
P (REF
COWI
1)
6 -----
(REF NAV
1)
7
---- REFER
TO 34-21-01
8 --- '--REFER TO 34-21-01
9 ---- PREFER 10 31-60-01
10
----. REFER
TO 34-40-01
11 -----
(REF
TRAFFIC)
12 ----- REFER
TO 34-40-01
13 ----
REFER
TO 34-52-01
14
-- ... REFER
TO 22-10-04
15 ----. REFER TO 22-10-04
16 ----- REFER TO 22-10-04
17 ---- REFER TO 34-53-01
18 --.-- REFER TO 23-50-01
19 ----.
(REF
COM
2)
20 ----
(REF NAV
2)
21 ----
REFER TO 31-60-01
0770519F2
© CESSNA AIRCRAFT COMPANY
24-61-01
Figure
05
Page 4
Feb 13/2006