Textron Cessna 182S - FIGURE 05 - CIRCUIT BREAKER PANEL

CESSNA
AIRCRAFT
COMPANY
MODEL
182/T182
WIRING
DIAGRAM MANUAL
HI016
ELECT BUS 1
FUEL Op5
1
2H1025-1PC025(20)
BEACH1026 1 2 2H1026-2PC025( 18)
LANDHINGI.AlT
127
2HI027-3PC025(14)
AVIONI
1 1 '
2HI023-4PC025(14)
HI0115 § 5%a
CABIN LTS/PR
HO007
1 2
Hl I 91
FLAPS
10
H 1021
REFER TO 24-20-01
_
s
2H1015-2PC024
(REF ALTERNATOR
SYSTEM)
1--(10)--p -- H1016-2D1001
(14)-M
DI001
2HI007-3PC024(16)
20 1007-H 1016(14)
H D01014 ALTF'PI.
2
IP I 2H1010-15PC025--
ELECT
BuS
2
Hr?7ltl
2H1022-4PCO24
REFER
TO 24-20-01
ELECT
BUS
2
HI
'
-o
2H-O22-14PCo02l5(20)
(REF ALTERNATOR
SYSTEM)
-1--(10)--
-H 1014-201002(14)-)-
2D1006-HI014(14)
- -
'
\D002
H
1002i
'x"
>
PANEL
LIGHTIS '1r
2H1003-8PC024
HH I 0HI03-9PC024
TAXI
LIG
0
HT
'
H I10 I29 TI' I
2H1024-5PC025
(14)
NAV.L TG( T '--1
2HI028-6PC025(14)
mn~~lH
1031
1O1
2H1029-7PC025(20)
STROBE
LIGHTS
2H031-8PC025(20)
ITO 3EAT
1Io
2H 1032-9PC025
(181
H 1020
ESSENTIAL BUS
,
r
'- D 1006/
H1034 1^-2
STANDBY
BATT
12D
STNOBY
INDTS
12
H 1036 1Z2
PFD 5
ADCAHORS7 11~
cH 10
3 9
'2
0.m gA1007d
HIQ18
AVN
US
1
NAV I1/EN II
TAS
R
Q
HIP
42
5Fb
(OPTION)
FIS
/
(CPT ION)
(OPTION) _
H104
7
19
AVN BU 2
HIQ21 't2
H 1052
1
2
2H1034-1 1PC025(14)
2HI022-22PC023
2H I 022-23PC023
2HI035-5PC024
2HI036-1PC023
2HI037-2PC023(18)
2H1037-3PC023(18)
2H1038-6PC024(16) -
2H1038-4PC023(16)
2H1039-5PC023(20)
BPF?, CHPA 9 i
5
S
1 ---- ,
2 ----.
- REFER TO SHEET 3
3 ----
4 ----
15 ----
PCL024
JC024
ELECT
CB PNL
DISC
1
----. REFER
TO 24-50-01
2
---- REFER
TO 33-11-02
3 ---- t
REFER TO 27-50-01
4 ----. REFER
TO 77-40-01
5
---- t REFER
TO 33-10-04
6 ----
t REFER TO
77-40-01
7 ----
REFER TO 77-40-01
8 ---- t REFER TO 33-10-04
9 ----
REFER
TO
33-10-04
CB sICHPANL [SC
5 ---- '
6
----
f
7 ----....
8
----
14 .... ·
--- _
- REFER
TO
SHEET
3
Ao
11 --. f
12 ----
13 ---- t
PCo23 PJC023
AVN CB PNL DIS
22
---- REFER
TO 25-60-01
23 ----
REFER TO
22-10-04
24
1
2
3
4
5
111018-12PC025(14)
2H1040-7PC024
16)
2H1040-6PC023(16)
2H1041-7PC023(18)
2H1041-8PC023(18)
2H1042-9PC023
2HI043-10PC023
2H1044-11PC023
2H1045-12PC023
2H1046-13PC023
6
7
8
9
10
11
12
13
H1019-13PC025(14)
2H1047-14PC023
2H1047-15PC023
2H1047-16PC023
2H1048-17PC023
2H1049-18PC023
2H1050-19PC023(20)
2H1051-20PC023
2H1052-21PC023
NOTES:
1. ALL
WIRE 22AB8. UNLESS
OTHERWISE NOTED.
£Q CAP AND STOW WIRE HEN OPTION IS NOT
INSTALLED.
Q2
INSTALL PROTECTIVE
TUBING OVER
DIODE
AS
SHOWN:
ISHRINK SLEEVE
(u23053/5 REF)
OTY 2
Q
USE HIGH
CURRENT
CONTACTS
(REF S3373-X).
5 ROUTE ALL WIRES
CLEAR OF RI010
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 COMM 1)
---- t 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
---- t (REF
TRAFFIC)
----. REFER
TO 34-40-01
---- t
REFER TO
34-53-01
14 ----
REFER
TO 22-10-04
15 ----
REFER TO 22-10-04
16
---- REFER
TO 22-10-04
17 ----. REFER TO 34-54-02
18 ----. REFER TO 23-50-01
19
---- REFER
TO 34-50-02
20 ---- ' REFER TO 34-50-02
21 ---- t REFER TO 31-60-01
0770519F1
CIRCUIT
BREAKER
PANEL
Figure 05 (Sheet 1)
© CESSNA AIRCRAFT COMPANY
24-61-01
0
Figure 05
Page 0
Feb 13/2006
-