Textron Cessna 182S - FIGURE 02 - BATTERY SYSTEM

CESSNA
AIRCRAFT
COMPANY
MODEL 182/T182
WIRING DIAGRAM MANUAL
.--- t (REF ALTERNATOR SYSTEM)
REFER TO
24-20-01
Fl J-BOX PWER DISC
*Q .. 3N----VEND)---------
--
A ----- (REF
ALTERNATOR SYSTEM)
F2 ! REFER TO
-------
I
REFER
TO
* ACV
F3 2
24-20-01
ALTERNAXTOR
R EAY1
Q ---- (VEND) I C (REF ALTERNATOR
SYSTEM)
CONTROL
tDALTERNATOR
*
S\
(
UNIT
0
"
RELAY
-* -!-"-'ir-----------
J1 J
0
oxm0O 18
Ii .[__ · J-BOX
SEINSE B
V---vEND)
-
r-
(VEND)
C -.- --
t (REF
POWER
E
---- (VEND)----
(
--.
VEND)----
*
U~L1 UP4
JN4
tI>-ELD
(
A
;,-
(-
VE
D)
R
H REF
K2
I LOtt VOLT-(A - (V E STARG
-- (VE ND)--- .-. (R--- (VENDF----- 0
* POWER BATTERY --
JUNCT ION RELAY t -A2K2-M1N002(4)
any, -.. E (RE
m___ p . ..--------
.(VEND)
------ E ----- t (REF
-°,h -o-(VEND )- -- < I
_-Of
l )
__(VEND) ---- D
F4
--- (VEND)- ---------- ' ---------
(VEND)----------- ------
B ----- (REF
:3R
5
:RNAL
RELAY
ALTERNATOR SYSTEM)
REFER TO
24-20-01
ALTERNATOR
SYSTEM)
ALTERNATOR SYSTEM)
J 1019
AMMETER/VACUUM
rPBO18-2JI019(20)
GPBOI1-3J1019(20)
-c
C
_1
E
t
(REF ENGINE
MAGNETO
SYSTEM)
REFER
TO
74-10-01
CLOCK & HOURMETER)
REFER TO
31-20-01
.- IVEN
~-(VEND
..--
(VEND
-
_-…---
(VEND)-
---
(i\ t E10122
1 NOT USED
2 AIMETER
3 AMMETER
4 NOT USED
5 NOT USED
INSTRUMENTS) ----- 6 LIIGHTING
7 NOT USED
8 POLARIZING
PIN
--- HHGOO1-9J1019- 9 GNO
S 1009
MASTER
SW ITCH
B I
B1 I
PCCPOPANEL
1
!0I
C
-1
DPBO18-18PC001(20)-18 ------- 1 JCO I -B2S1009----?
A
BATT
G1001
j 1C100,-lOO20PCO1 20 -
REFER TO
91-10-02
It----
20JC0OO-C2S1009----------i
I
.----------.-------------------
_-------
.
. ------- --------
EXTERNAL POWER REER TO
--
(R
INE
TRUSS
RECEPTICAL
:91-10-02
A
GNO
FIREWALL
Y GC002
-(-UCOOl-GCOO2(0,4)J REFER TO
-. ...... 91-10-02
WA99M 0 =
VWXO
NOTES:
1. ALL WIRE 22AWG. EXCEPT AS NOTED
GROUND STRAP (REF FUSELAGE WIRE ROUTING)
3 VENDOR SUPPLIED ASSY
4
INSTALL POLARIZING
PIN INTO PIN B OF
J1019
PIN S IS STUD LOCATED ON ACU.
BATTERY POWER AND GNO WIRES TO RUN THRU
CONVOLUTE TUBING FROM THE POSITIVE BATTERY
TERMINAL TO THE ENGINE FIREIALL. WIRES
SHALL BE
TWISTED 7 TURNS (±2
TURNS) INSIDE
THE CONVOLUTE TUBING. SECURE ENDS WITH HEAT
SHRINK
TUBING
TO PREVENT
UNTWISTING
PRIOR
TO
BUNDLE INSTALLATION.
/ FUSE IS REPLACED BY CIRCUIT BREAKER ON
CONFIGURATION EFFECTIVE EC42884 & ON OR
COMPLIANCE WITH SERVICE BULLETIN SBOO-24-01
(REFERENCE).
Q 40AMP CIRCUIT
BREAKER WAS 30AMP
PRIOR TO
ECS155B. 40AMP
CIRCUIT BREAKER
SHALL BE USED
FOR FIELD REPLACEMENT ON ALL AIRCRAFT EOUIPPED
WITH MC01-3A ELECTRICAL POWER CONTROL UNITS
(REFERENCE
CURRENT APPROVED
VENDOR DRAWING
FOR
MC01-3A).
/j CONNECTOR WIRE AND FUSE ARE PART OF STANDYBY
BATTERY ASSY.
0770512 12
BATTERY SYSTEM
Figure
02 (Sheet
1)
© CESSNA AIRCRAFT COMPANY
24-30-01
Figure 02
Page 0
Feb 13/2006
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