Textron Cessna 182S - FIGURE 06 - ALTERNATOR SYSTEM

CESSNA
AIRCRAFT
COMPANY
MODEL
182/T182
WIRING
DIAGRAM
MANUAL
CN001
SACU-BMNOO1(06)
F1
J -BAX
.----
(VEND)
F2
;B----(VEND)
ACU3
ALTERNATOR
K
Tf
fp---(VEND)
~~~~L ~ ~ ,ALTERNATOR
-
1
SE*sE T~ ..... SENSE B ---- (VEND)--_ .
1
,
(VEND) ;
POWER
E ----
(VEND)----
---.
(VEN ---
FIELD A
r
(VEND)
LOW VOLTAGE
r
(VEND)
GND F -------
CURRENT
CURRENT
SENS
DISC
.. ENSOR I-
-- (VEND)--
. --- -- (VEND)----A--
(VEND)....------------
*
J ON - E --- -- (VEND)---
-- 4 --
(VEND)
START
!;*»
BOX
K3
D1
----------
VENVED
)
BE
AL
,
;Q
POW1ER RELAY
,
I
L
'
:-(EVEDD)---
|
/fD-(ND
(VEND)
POWER
-
"...-----
F-
JUNCTION
------- _-- OE\
-------------------
(VEN
o-(VEND)-'
J3
EXTERNAL
POWER
vGN002
4
RECEPTICAL
(REF BATTERY SYSTEM)
(REF BATTOrY SYSTEM)
(BATTERY)
(GND STRAP)
REFER TO 24-30-01
REFER
TO 24-30-01
38
PBO19
PW DISC
A
APBO19-H1014(10)
B
(REF T IONAL
_ CONFIGURATION)
xPsB018
ox
DISSC
C --- CPB
1B-13JC026(20)
H - HPBO1B-ALT.FIELD(20)--
QA
BPBO19-HIl16(10)
JSV&CH PNLPD 6
fL7_ , (REF CIRCUIT BREAKER &
[I-. SWITCH
PANEL - NAV
3 OPTION)
REFER TO 24-61-01
H1014
US *2
1
(REF CIRCUIT
BREAKER
&SWITCH PANEL
- NAV 3 OPTION)
REFER TO 24-61-01
BUS *1
H1016
A ---..
(L REF
ENGINE/AIRFRAME
F ------
MO)NITOR - NAV
3 OPTION))
G -----
REFER
TO
77-40-01
E ----- (REF MAGNETO SYSTEM)
REFER TO 74-10-01
0
-----
(REF
BATTERY
SYSTEM)
(GND
MASTER
SW ON)
REFER TO 24-30-01
B
.,... (REF BATTERY SYSTEM)
(STARTER)
REFER
TO 24-30-01
NOTES:
1. ALL
WIRE 22AWG.
EXCEPT AS NOTED
VENDOR SUPPLIED ASSY.
PIN
S IS
STUD
LOCATED
ON
ACU.
INSTALL 16
INCHES OF VARGLAS
SLEEVE
(P618015
REF) ON
FIELD WIRE
STARTING
AT PNO08.
L// INSTALL
CAVITY
PLUG/SEAL
IN PIN
C ON PB019
WHEN
OPTIONAL
CONFIGURATION
IS NOT INSTALLED.
/I DISCARD CAVITY
PLUG/SEAL (PART OF PBO19
KIT).
/\ INSTALL
PROTECTIVE
TUBING AS SHON:
ALTERNATOR
-
r-SHRINK
SLEEVE
(M23053/5-105-9
REF)
RING
TERMINAL
VARGLAS SLEEVE
(P618015
REF)
'
16
WIRE
(HPBO18-ALT.FIELD(2D))
/Q
FUSE
IS REPLACED
BY
CIRCUIT
BREAKER
ON
CONFIGURATION
EFFECTIVE EC42884
& ON OR
COMPLIANCE
WITH
SERVICE
BULLETIN
SBOO-24-01
(REFERENCE).
& WIRE NOT
TO BE STAMPED
WITH
POINT TO
PINT DATA.
STAMP AS SHOWN.
L 4DAMP CIRCUIT BREAKER WAS 3OAMP PRIOR TO
EC51558.
40AMP
CIRCUIT
BREAKER
SHALL BE
USED
FOR
FIELD REPLACEMENT
ON ALL AIRCRAFT
EQUIPPED
WITH MCO1-3A
ELECTRICAL
POWER
CONTROL
UNITS
(REFERENCE
CURRENT
APPROVED
VENDOR
DRAWING
FOR
MCO1-3A);
0770510G6
ALTERNATOR SYSTEM
Figure 06 (Sheet 1)
© CESSNA
AIRCRAFT
COMPANY
24-20-01
Figure 06
Page 0
Feb 13/2006