Textron Cessna 182S - Alternator System; Battery System

CESSNA
AIRCRAFT
COMPANY
MODEL
182/T182
WIRING
DIAGRAM
MANUAL
CN001
SACU-BMNOO1 (08)
--------------------------------------
J
P17
I i J 2 P8 1 7
1
'
J-BOX PWER OlC
N-(VEND)·-
----------
A
APB017-HI01
-- (VEND)--
-----------
BPB017-HI01
-OX
DI
CB PAN1EL
I
------.-----.----------
c
CPBO18-17PCOO1----0-I-
---
----------.----------
H -HPBO01-FMN01
-
I
,IS-C
,I
- A
APB018-16J1006
· (VEN)----L---
F
-----
I REF
BATTERY
SYSTEM)
REFER
TO
-t
- 0-EIID):::-L _
o ..
F (REF BATTER
Y S
YSTEM)
REFER TO
VEND)---
-
.L.-------
CG. ---
. (AMEATER)
24-30-01
.----.-
i
I
.---- ... ---- r--- . E ------. (REF MAGNETO SYSTEM) REFER TO 74-10-01
-----------
---.....-- .....-
----- (REF
BATTERY SYSTEM)
REFER TO
END)
-----
-------.
B ------
(REF
CLOCK
& HOURHETER)
REFER
TO
31-20-01
I*| | ~
(REF
BATTERY
SYSTEM)
REFER
TO
(STARTER)
24-30-01
ACU
ALTERNATOR
CONTROL
UNIT
SENSE
POWER
FIELD
LOW VOLTAGE
GCND
I
POWER
JUNCTION
I BOX
L____________
-GUNO01-GN008
08)(O
7=
----------------
--
-- -------- -
.- -- - -
- - - -- - ----
-- ----
EXTERNAL POWER
* GN002
REFER TO
1 .~RECEPTICAL
91-10-02
(REF
BATTERY
SYSTEM)
(REF
BATTRY
SYSTEM)
(BATTERY)
(CN0
STRAP)
REFER
TO
REFER
TO
24-30-01
24-30-01
CN08s
REFER TO
91-10-02
4(10)
6(10)
c01
(REF BUS
BAR &
SWITCH PANEL)
REFER
TO
28V MASTER
SW ON)
24-61-01
U1006
ANNUNCIATOR
PANEL
UIO00
16
VOLTS
(REF
WARNING/CAUTION
ANNUNCIATOR)
REFER TO
31-50-01
1s014
US 2
(REF (BUS
BAR &
REFER TO
SUITCH PANEL)
24-61-01
HUS
1
016
NOTES:
1.
ALL WIRE 22AIC.
EXCEPT AS NOTED
VENDOR
SUPPLIED
ASSY.
PIN
S IS
STUD
LOCATED
ON
ACU.
INSTALL
16 INCHES
OF VARGLAS
SLEEVE
(P616015
REF)
ON FIELD
WIRE STARTING
AT PN008.
t INSTALL
CAVITY
PLUG/SEAL
IN PIN
C ON
PB019 WHEN
OPTIONAL
CONFIGURATION
IS
NOT INSTALLED.
ti
DISCARD
CAVITY
PLUG/SEAL
(PART
OF
PB019
KIT).
\ INSTALL
PROTECTIVE
TUBING
AS
SHOWN:
ALTERNATOR
'
rSHRINK SLEEVE
(M23053/5-105-9
REF)
RING
TERMINAL
,
/
VARGLAS
SLEEVE
(P618015
REF)
I----/----I
/
1 16 I/
WIRE
(HPOI1B-ALT.FIELD(20))v
f5 FUSE IS REPLACED BY CIRCUIT BREAKER ON
CONFIGURATION
EFFECTIVE
EC42884
& ON
OR
COMPLIANCE
WITH
SERVICE
BULLETIN
B500-24-01
(REFERENCE).
Lj WIRE
NOT TO
BE STAMPED
WITH
POINT
TO PINT
DATA.
STAMP
AS
SHOWN.
40AMP
CIRCUIT
BREAKER
WAS
30AMP
PRIOR
TO
EC51558.
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
C01 -3A).
077051OG1
ALTERNATOR
SYSTEM
Figure
01
(Sheet
1)
©
CESSNA
AIRCRAFT
COMPANY
24-20-01
Figure 01
Page 0
Feb
13/2006