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Textron Cessna 182S User Manual

Textron Cessna 182S
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CESSNA
AIRCRAFT
COMPANY
MODEL
182/T182
WIRING
DIAGRAM
MANUAL
CNOO1
SACU-BMNOO1
(08)
- -- -- --
-- -- --
-- -- -- --
-- -- --
-- -- -- --
-- --
-----
F
P-BO
R
DISC
.
VESN--
VN
----------
A
APB019-HIO14
F2
----
(VEND)--
------------
B
BPBOlS-HIDI0
ACU
F(F
ALTERNATOR
TK1-E
-C
CONTROL
ALTERNATOR
---
VEND)----------
--
.ONFIGURATION)
U
I
JT
P
/
m
UNIT
RELAY
JBOX
DISC
B
0
1
8
PC
PANEL
d
SENSE
B---(VEND)---
:
(VEND)--------------------------
C
CPBO-17PCOO
(20)
[--
POWER
E
---
::(:VEND)---
.-- .
_
-(VEN)----I
FIELD
A[
(VEND)------------------------
H
--
HPB01-Fw001
(20)-
LOW
VOLTAGE
H
(VEND)-----------
;
GND
F
-----
iCUWRET
CURRENT
SENSE
DISC
----
A
AP018-16J1006(20)
a..
ENSER
I
N
-
_VEND
.----
--
A------(VEND)---------------
F ----
(REF
BATTERY
SYSTEM)
REFER
TO
:--
--------
(:vEND
:------------
VEND)i---
------------
GC
----
r.
(AMMETER)
24-30-01
K2
STI
RT
K4
RELAY
BATTERY
RELAY
I
.
_---__o
V,--.--------
VEND)------------
-----------
E
-----
(REF
MAGNETO
SYSTEM)
REFER
TO
74-10-01
I(-^.
, . .
.
I
:
(VEND)---.
4
'-~iO-^'"'~
P
E,(VEND)------------
-----------
D
---
(REF
BATTERY
SYSTEM)
REFER
TO
POWER
----
(GND
MASTER
SW
ON)
24-30-01
JUNCTION
--
:-
-E
-
N
BO
T
X
N
-------
VEND)-
-------------
JdL-------
(VEND)
----.-----------
B
----
(REF CLOCK
&
HOURMETER)
REFER
TO
31-20-01
EXTERNALAY
*/7k
!PORER
RELAY
.......
I
-"
*L
IS---
L---(------(VEND
!__________i______
I
i_______
____
L(REF
BATTERY
SYSTEM)
REFER
TO
-I------
(STARTER)
24-30-01
i8
HLFLr IU
91-10-02
4(10)
6(10)
01
(REF
BUS BAR
I
SWITCH
PANEL)
REFER
TO
(28V
MASTER
SW ON)
24-61-01
J1006
ANNUNC
IATOR
PANEL
U1005
|
VOLTS
(REF
WARNING/CAUTION
ANNUNC I
ATOR)
RFFFR
TO
31
-O-C
-........
..
-
..- -
.....-
OI-
-o
1-)g- .... _--------- ----------------.
EXTERNAL
POWER
vGN002
REFER
TO
i
RECEPTICAL
91-10-02
(REF
BATTERY
SYSTEM)
(REF
BATTERY
SYSTEM)
(BATTERY)
(CND
STRAP)
REFER
TO
REFER
TO
24-30-01
24-30-01
H1014
BUS
42
(REF
(BUS
BAR
&
REFER
TO
SWITCH
PANEL)
24-61-01
BUS
16
HI016
il
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
PN008.
Q INSTALL
CAVITY
PLUG/SEAL
IN
PIN
C ON
PBO19
WHEN
OPTIONAL
CONFIGURATION
IS
NOT
INSTALLED.
DISCARD
CAVITY
PLUG/SEAL
(PART
OF
PB019
KIT).
7
INSTALL
PROTECTIVE
TUBING
AS
SHOWN:
ALTERNATOR
>
rSHRINK
SLEEVE
(M23053/5-105-9
REF)
RING
TERMINAL
/
VARGLAS
SLEEVE
(P618015
REF)
16
/
WIRE
(HPBIB-ALT.FIELD(20))v
5
FUSE
IS
REPLACED
BY
CIRCUIT
BREAKER
ON
CONFIGURATION
EFFECTIVE
EC42884
&
ON
OR
COMPLIANCE
WITH
SERVICE
BULLETIN
SB00-24-01
(REFERENCE).
Li
IRE
NOT
TO
BE
STAMPED
WITH
POINT
TO
PINT
DATA.
STAMP
AS
SHOWN.
u
40AMP
CIRCUIT
BREAKER
WAS
30AMP
PRIOR
TO
EC51558.
40AMP
CIRCUIT
BREAKER
SHALL
BE
USED
FOR
FIELD
REPLACEMENT
ON
ALL
AIRCRAFT
EQUIPPED
WITH
MCOl-3A
ELECTRICAL
POWER
CONTROL
UNITS
(REFERENCE
CURRENT
APPROVED
VENDOR
DRAWING
FOR
MCO1-3A).
0770510G2
ALTERNATOR
SYSTEM
Figure
02
(Sheet
1)
©
CESSNA
AIRCRAFT
COMPANY
0
24-20-01
Figure
02
Page
0
Feb
13/2006

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Textron Cessna 182S Specifications

General IconGeneral
BrandTextron
ModelCessna 182S
CategoryTools
LanguageEnglish

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