Textron Cessna 182S - Page 370

CESSNA
AIRCRAFT COMPANY
MODEL 182/T182
WIRING
DIAGRAM
MANUAL
HI016
ELECT
BUS
I
I.
IFUELPU IP
5
2HI025-1PC025(20)
FUEL PUI~'
H 102.6 HI** 2IoD26-2PCO25(1R )
BEACONLPIHT +
2H1026-2PC0251B)8
LANo DING L
1T
2
2H1027-3PC025(14)
AV
1ON
3
1
r.2
2HI023-4PCO25(14)
H1015 I,-pf
CABIN
LTS/PWR
1'
H107 '% CRIHI01 BU
FLAPS 1o 0
CROSSF
BUS
2H1015-1PC024(20)
REFER
TO 24-20-01
_
r
2HI015-2PC024
(REF ALTERNATOR
SYSTEM) '-(10)-- . H016-2DI001(14)-i-
DI001 2HI007-3PCO24(16)
- 2D1007-I11016(14]
--
"
J
CIB
H 14 ALTH.' FlELOO
2HI010-15PCO25
H 101 4 2MNI022-4PC024
REFER
TO 24-20-01
ELECTHBUS
2 1WAR,2
1
--
2H1022-4PCO25120
)----
REFER TO 24-20-01 A NI
(REF
ALTERNATOR
SYSTEM) -- (10>--
·- H1014-2D1002(14)-4]-
-- 2D10O6-H101414)
D
I1
002
1
PAHL
I2GHT
S
W
NAVX L IGHT SF
I
2H1028-5PC025(14
H 1029
.,-I
NAV. LIGHT
15
2H1028-6PC025
(14)
2H1029- 7PCO25(20)
STROEIE
'
9
H1TS
I
2I031-BPCO25(20)
P
3IOTHEAT
i7
2NI032-9PC025(18)
H 1020
ESSENTIA BUS
r D 1006Q
H 1034 1,2
STANDBY
BATT
STNOBY IND LTS 1
H1036 1s2
ADC/AHRS
1
NAV1 'G1N
C ^o 1 I , 007
H I01_8
AVN Ul 1
H 1040
NAV 1/ENG 15
HI 041 1Z,.
AdC/AHRS '
H 'pP
4
2 12 2
H"SITOO43 1 5
TAS Q
(OPTION)
FIS
.
(OPTION)
ADF
.
(OPTION)
AVN BUS 2
ApQL
8
'I
XPR 5
H1051
1 2
HAIUO4 I'
HlPO1
5 2
i2
H?5:3'2 5
2HI034-11PCO25(14)
- 2H1022-22PC023
2H
I 022-23PCO23
2HI035-5PC024
2H1036-1PC023
2HIO37-2PCO23(18)
2H1037-3PCO23(18)
2H1038-6PC024( 16R)
2HI038-4PC023(16)
2HI039-5PC023(20)
I ---- f
1 ----.
- REFER TO SHEET 3
3
----
4 --.--
------- 15 --..
ELET CB PNL DI
I
---- I REFER
TO 24-50-01
2 ---- REFER TO 33-11-02
3 ---- REFER TO 27-S0-01
4 ---- , REFER TO 77-40-01
5
----. REFER
TO 33-10-04
6 ---- REFER TO 77-40-01
7 ----. REFER TO 77-40-01
8 ---- , REFER TO 33-10-04
9 ----. REFER
TO 33-10-04
CB&SITCH PANEL DISC
0 ,
5----'
6
----
7
----.
8 ----
'9
4
--
- REFER
TO
SHEET
3
11
----
12 ---.
------- 13 ----
PC023 JC023
AVNB
PNL
ISC
22 ---- REFER TO 25-60-01
23 ----.
REFER TO
22-10-04
24
1
2
3
4
5
111018-12PC025(14)--
2HIO040-7PCO24(16)
2HIO40-6PCO23(16)
2HIO41-7PC023(18)
2HI041-8PC023(18)
2H1042-9PCO23
2HIO043-10PC023
2H1044-11PC023
2HI045-12PCO23
2HIO46-13PC023
H1019-13PCO25(14)
2H1047-14PCO23
2H1047-15PC023
2H1047-16PC023
2H1048-17PCO23
2HI049-18PC023
2H1050-1BPC023(20)
2HI051-20PCO23
2HI052-21PCO23
6
7
8
9
10
11
12
NOTES:
1. ALL WIRE 22AWB. UNLESS OIHERWISE NOTED.
2
CAP AND STOV WIRE
WHEN OPTION IS
NOT
INSTALLED.
Q INSTALL PROTECTIVE TUBING OVER DIOOE
AS SHOWN:
SHRI NK SLEEVE
(M23053/5 REF)
OTY 2
4 USE HIGH CURRENT CONTACTS (REF 53373-X).
/6
ROUTE
ALL WIRES
CLEAR OF ROO10
RESISTOR BY AT
LEAST 0.5 INCH.
RESISTOR MAY GET
HOT.
----. REFER
TO 31-60-01
----. REFER TO 34-21-01
---- .REFER
TO 34-21-01
---- , (REF NAV 1)
----. (REF COMu 1)
----. REFER TO 34-50-01
----. REFER TO 34-21-01
----. REFER TO 34-21-01
----. REFER TO 31-60-01
---- REFER TO 34-40-01
---- (REF TRAFFIC)
---- , REFER TO 34-40-01
13 ---- REFER TO 34-53-01
14
15
16
17
18
10
20
21
----. REFER
---- ; REFER
---- REFER
----
REFER
----
REFER
TO
TO
TO
TO
TO
----
REFER
TO
----
P REFER
TO
---- REFER TO
22-10-04
22-10-04
22-10-04
34-54-02
23-50-01
34-50-02
34-50-02
31-60-01
0770519F1
CIRCUIT
BREAKER
PANEL
Figure 05 (Sheet 1)
© CESSNA AIRCRAFT COMPANY
24-61-01
Figure 05
Page 2
Feb 13/2006
-