Textron Cessna 182S User Manual

CESSNA
AIRCRAFT COMPANY
MODEL 182/T182
WIRING DIAGRAM MANUAL
--- r (REF
ALTERNATOR
SYSTEM)
REFER TO
24-20-01
j B2x
PR017
J-BX
PIER DISC
/ rFl--- (VEND)---- A ---- (REF ALTERNATOR SYSTEM)
ACU____
3 0
1REFER TO
ACU K1I 2 24-20-01
ALTERNATOR
R
--- (VEND)--------
B ----
(REF ALTERNATOR SYSTEM)
UNIT "if~iVDRELAY
3
o
J1 PE018
:L-
UNIT__________________
-BOX DISC
ISENSET B----(VEND)-
J
(VEND)-
C -- -- (REF ALTERNATOR
SYSTEM)
POWER
E-
(VEND)--
...
REFER
TO
I POVIR
aI
E-----(VEND)-----· E ,--- (VEND) ------
'
24-20-01
FIELD A
,
(VEND)-----------
-------------
H ---- (REF ALTERNATOR
SYSTEM)
LO VOLTAGE
H
VEND)--------;-
-----------
A-- --.
(REF ALTERNATOR
SYSTEM)
J 1019
GND F ----
AMMETER/VAClUU
CURRENT
CURRENT
SENSE DISC
Q
EL
2 S009
N.- ;ESOR | ·- r--T1 1 NOT USED MASTER
I--.VEND)
..---
VEND).---.A--I
-----. (VEND)----.------
F FPBD18-2J
1019
2 AEER
SW
I TC
VEND).---B--- B--(-- VEND) , - G -- GPB1B-3J 1019 3 AUMETER
I.*~
a-~
-1
4 NOT
USED
.L- -.
K2
^5
NOT USED
START
' (REF
ENGINE INSTRUMENTS) ----- 6 LIGHTING
POWER
K4
RELAY
7 NOT USED
Bi '
I OWR
BATTERY
8 POLARIZING
PIN
JUNCTION
RELAY
| 2K2-MNDO02(4)
I
-HHtGIOD1-9JI019-9
GND
L
I DnV
.
.
|
frer
^a.
I DUA
-+UCOO1-A1K3(04)-
-d; _
Lrf------------
(VEND
------------------
E -- --
C
ui NIT
[~-
(VEND)
SYSTEM)D
74-10-OI
PCaOB0PlANELJDCaS0ClT
J Cf(VEND..---
4REFER
TO
PC0
01 J[C0
IC
(VEND)------------
--------- D-0P0B-18-BPC001
18 --
1JCOO-B2SI009,----.
D--
(
F4I
BATT
(--- (VEND )-
-----
----------.
-
HOURMETER)F
r.E
HOURETR
:RNAI
REL
A
HLILH IUG I 00
31-20-01GI 001
'
MUGIO10-20PCOOI
20-----------20JC001-C2SIO09----------
I---------(VENE
REFER TO
91-10-02
NOTES:
--------- -----R--EC--EPTIC--AL- REFER TO *N i?+ 1. ALL WIRE 22AWG. EXCEPT AS N
(ŽNE RECEPT ICAL
REFER
1
N 1
GROUND
STRAP (REF
FUSELAGE
,---
(REF IE TRUSS GND)91-10-02
T
VENDOR SUPPLIED ASSY
i
M T
INSTALL
POLARIZING PIN
INTO
F;,,/2\~ IG"E~~~
REWALL7
~ ~PIN S IS STUD LOCATED ON
AC
,,
A
GN008FIOALs
BATTERY POWER AND
GND WIRES
*~~y""""~~~~~
GC00D~~2
C0NVOLUTETERMINAL
TO
THE ENGINE
FIRE'
~-~-UC0G-GCOO24 9-02THOCO-2 COV, UT TN SC
-( -UCOOl-GC002(04-'
REFER TO
SHALL BE TWISTED
7 TURNS (i
::C
91-10-02
THE CONVOLUTE
TUBING. SECUI
ucN
WAYT9E +
DTED
WIRE
ROUTING)
PIN 8
OF J1019
J.
TO RUN THRU
OSITIVE
BATTERY
WALL. WIRES
2 TURNS) INSIDE
RE ENDS WITH HEAT
SHRINK TUBING
TO PREVENT UNTWISTING
PRIOR TO
BUNDLE
INSTALLAT
ION.
7 FUSE
IS REPLACED BY CIRCUIT
BREAKER ON
CONFIGURATION
EFFECTIVE EC42884
& ON OR
COMPLIANCE
WITH SERVICE
BULLETIN S800-24-01
(REFERENCE).
Q/ 40AMP CIRCUIT
BREAKER WAS JOAMP
PRIOR TO
EC51558.
40AMP
CIRCUIT
BREAKER
SHALL BE
USED
FOR
FIELD REPLACEMENT
ON ALL AIRCRAFT
EQUIPPED
WITH MC01-JA
ELECTRICAL
POWER CONTROL UNITS
(REFERENCE
CURRENT
APPROVED
VENDOR DRAWING
FOR
MC01-3A).
CONNECTOR. WIRE AND FUSE ARE PART OF STANDYBY
BATTERY
ASSY.
077051211
BATTERY SYSTEM
Figure
01 (Sheet
1)
© CESSNA AIRCRAFT COMPANY
24-30-01
Figure 01
Page 0
Feb 13/2006

Textron Cessna 182S Specifications

General

Brand	Textron
Model	Cessna 182S
Category	Tools
Language	English