Textron Cessna 182S User Manual

CESSNA
AIRCRAFT
COMPANY
MODEL
182/T182
WIRING
DIAGRAM
MANUAL
P I
303
AUTOPILOT
COUP
U1303
ILS
ENERGIZE
7
PANEL
LIGHTING
12
P
I 304
AUTOPILOT
COUP
U1304
SERVO
VALID
CLUTCH
LO
PITCH
DRIVE
Cu
SERVO
CUD
REF
P 900
[-
PANEL
LE LIGHT
ING
PT300
<B
P
ITCH SERVO
UT300
28.
7
24
K
F
0
I
L
NOTES:
1
ALL
WIRE
22
AVG.
UNLESS
OTHERWISE
NOTED.
C(>GND
STUD
IS LOCATED
ON
THE BACK
OF THE AUTOPILOT
COMPUTER
RACK.
[D>PART
OF
ALLIED
SIGNAL
INSTL
KIT 050-03375-O001.
[:>PART
OF
ALLIED
SIGNAL
KIT
050-03245-0000.
E>GND
STUD
IS
LOCATED
ON
FUSELAGE
BULKHEAD
156.00.
[J
PART
OF
ALLIED
SIGNAL
INSTL
KIT
050-00398-OODO(2
REQ)
[Z>ND
STUD
IS
LOCATED
ON
FUSELAGE
BULKHEAD
172.00.
[E>GROUND
SHIELDS
TO
THE BACKSHELL
OF THE
CONNECTOR
USING
THE
GARMIN
SUPPLIED
GROUNDING
WIRES
FASTENED
TO THE
CONNECTOR.
SHIELD
WIRES
SHOULD
BE NO
LONGER
THAN
3'.
9. THE
FOLLOWING
SPECS
ARE
PART
OF THIS
DRAWING:
CSAMO12
SHIELDED
CABLE
INSTALLATION.
CES2716
WIRE TERUMINATIONS.
I[>16GA
WIRE
IS PART
OF GARMIN
TERMINATED
WIRE
GROUP.
[>PART
OF
GARMIN
KIT
011-01000-00
[REF).
SERVO VALID
CLUTCH LO
PITCH
DRIVE
Cw
SERVO Cm REF
6
TRIM
SENSE
-
23
PITCH
FEEDBACK
47
PITCH
FEEDBACK
48
(WHT)
(BLU)
(WHT)
(BLU)
REFER
TO
91-10-02
5JI
GS301
<
REFER
TO
91-10-02
TRIM
SENSE
+
TRIM
DRIVE
CV
SERVO CMD REF
TRIM
FDB
1
TRIM
FDB
2
CLUTCH
LO
TRIM
FAIL
OUT
32
3C-
2
4
(WHT)
(BLU)
(WHT)
(BLU)
<:
GS303
REFER
TO
91-10-02
GPS
SELECT
26
J
TRIM SENSE
+
R
TRIM
SENSE
-
P
PITCH
FEEDBACK
A
PITCH
FEEDBACK
C
POWER
GND
N
CHASSIS
GND
E
CLUTCH
HI
H 28VDC IN
PT301
PITCH
TRIM
UT301
E CLUTCH HI
H 28VDC
IN
L
TRIM DRIVE
CT
D
SERVO
CiD REF
J
TRIM
FOB 1
R TRIM
FDB
2
F CLUTCH
LO
A
TRIM
DISABLE
C POWER
GND
N
CHASSIS
GND
n[>
PT31
1
INT.
AVN.
*2
UT307
TRIM
FAIL
ANUNC
2 GPS
ANNUNCIATE
r 25
ANNUNCIATE
*2
DUAL
AXIS AUTOPILOT
Figure
10
(Sheet
2)
©
CESSNA
AIRCRAFT
COMPANY
0
m>
3924149B2
0
22-10-04
Figure
10
Page 2
Feb
13/2006
40
I4Al--1:3

Textron Cessna 182S Specifications

General

Brand	Textron
Model	Cessna 182S
Category	Tools
Language	English