Textron Cessna 182S - FIGURE 04 - ALTERNATOR SYSTEM

CESSNA
AIRCRAFT
COMPANY
MODEL
182/T182
WIRING
DIAGRAM MANUAL
0
CN001
H1014
BUs *2
SACU-BMNO01 (06)
r-----.------------------------------------------
-
i.
-
F1 i J--X PwR DISC
* b---
(VENo)--,----------
A
F2
--- (VEND) ------------- B
ACU
K1
F
(REF
TIONA
* ALTERNATOR KcT
AT R
ALTERNATOR
J ----
(VENDE------------
C CONFIGURATION)
CONTROL
ALTERNATOR
I , .11 PPflR
SENSE
g~I
~
POWER
FIELD
I
LOW VOLTAGE
I GND
POWER
II IlrT I nKI
.- 'BOX DiSC'"
V
(VEND)------------t------------
----
CPBO-17PC001(20)
ND)
----
c< 1
(VEND)------------
------------
H -HPBI18-ALT.FIELD(20)
(VEND)--------
-------
/
P4 J4ISC
---- A
APB018-16JI0
IT
P4AY
\s i---;-n
*
.----------
(VEND)------------
---------
E ------
(REF
MAGNETO
SYSTEM)
I f(VEND)---
;
REFER TO 74-10-01
(VEND)-----------
-----. ----- .- (REF
BATTERY SYSTEM)
F
t
I4
0
(ICEGND MASTER
SW ON)
F4
REFER
TO
24-30-01
I
- .-- (VEEND)
- ---------- r p----------
(VEND) ------ i----- -----
B ---- (REF CLOCK & HOURMETE
I
ABOX | I
_.K.s....
5 --
RFFFR TO A1-2n-n1
I ti
II
:
:
I
I
_ _
_
_ _ _
~I _<
(REF BATTERY
SYSTEM)
(STARTER)
*I|
~ ~
REFER TO
24-30-01
i
U
APBO19-H1014(10)
06(:
BPBO19-HID16(10)
PCBO
PANEL
1
SC
0 1
f[j7___
(REF BUS BAR
SWITCH PANEL)
I (28V MASTER SW ON)
REFER TO 24-61-01
J 1006
ANNUNC I ATOR
PANEL
U1005
20)
16| VOLTS
(REF
WARNING/CAUT
ION
ANNUNC I ATOR )
REFER
TO
31-5C
:R)
------------------------------
L2L
P)-------
EXTERNAL POWER VGN002
'I RECEPTICAL
(REF BATTERY
SYSTEM)
(REF
BATTEY SYSTEM)
(BATTERY)
(GNO
STRAP)
REFER
TO 24-30-01
REFER
TO 24-30-01
H
(REF BUS BAR &
SWITCH PANEL)
REFER
TO 24-61-01
BUS 1e
H 1016
o
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.
Q INSTALL
CAVITY
PLUG/SEAL
IN PIN
C ON PB019
WHEN
OPTIONAL
CONFIGURATION
IS NOT INSTALLED.
Q DISCARD
CAVITY
PLUG/SEAL
(PART
OF PB019
KIT).
4/
INSTALL
PROTECTIVE
TUBING
AS
SHOWN:
ALTERNATOR
/rSHRINK
SLEEVE
(M23053/5-105-9
REF)
RING TERMINAL
VARGLAS SLEEVE
(P618015
REF)
--
1
j
/
16
WIRE
(HPBO18-ALT.FIELD(20))-
Q
FUSE IS
REPLACED
BY CIRCUIT
BREAKER
ON
CONFIGURATION
EFFECTIVE
EC42884
& ON
OR
COMPLIANCE
WITH
SERVICE
BULLETIN
SB00-24-01
(REFERENCE).
L WIRE NOT TO BE STAMPED WITH POINT TO PINT DATA.
STAMP AS SHOWN.
/ 40
AMP CIRCUIT
BREAKER
WAS
3OAMP
PRIOR TO
EC51558.
40AMP
CIRCUIT
BREAKER
SHALL
BE
USED
FOR
FIELD REPLACEMENT
ON ALL AIRCRAFT
EQUIPPED
WITH MCOI-3A
ELECTRICAL
POWER
CONTROL
UNITS
(REFERENCE
CURRENT
APPROVED
VENDOR
DRAWING
FOR
MCO -3A).
0770510G4
ALTERNATOR SYSTEM
Figure
04
(Sheet
1)
© CESSNA
AIRCRAFT
COMPANY
0
24-20-01
Figure 04
Page 0
Feb 13/2006