Textron Cessna 182S - Page 285

CESSNA
AIRCRAFT
COMPANY
MODEL 182/T182
WIRING DIAGRAM MANUAL
P 303
AUTOPILOT COMP
U303
HDG/CRS REF 27
HDG DATUM 2
HDG VALID IN 11
+ NAV FLAG 22
- NAV FLAG 2.
NAV DEV
+LEFT
24
NAV DEV *RIGHT 25
P 304
AUTOPILOT COUP
U1304
CRS DATUM
17-
GS DEV UP IN 9
GS
DEV DN
IN 10
GS FLAG (0 ) 31
GS FLAG
-)
12
ROLL
STR VALID
40-
ROLL STR
ROLL STR
I
ALTITUDE
INPUT
HI 41
LOW 42
A1 11
A2 13
A4 14
B1 33
- B2 34
B4 20
Cl 21
C2 3
C4 5
D4 29
-0
A1304
(IHT)
(BLU)
(WHT)
(BLU)
- GS30O1c
-· REFER TO
91-10-02
(WHT)
(BLUI
(WHT)
(BLU)
(WHT)
(BLU)
(ORN)
B> PT312
INT AVN *2
UT307
68 HDG VALID OUT
L 19 + NAV FLAG
U 20 - NAV FLAG
n 17 NAV DEV *LEFT
18
NAV DEV
+RIGHT
PT903
dl:
1
]
(16)
REFER
TO
91-10-02
L 23 VERT DEV + UP
24 VERT
DEV +
DN
25 VERT FLAG (+)
L26 VERT FLAG (-)
>D
PT313
INT AVN *2
UT307
L 47 HOG DATUM LO
4n 9
CRS
DATUM
LO
46 HDG DATUM HI
48
CRS DATUM
HI
NOTES:
1 ALL WIRE 22 AUG. UNLESS OTHERWISE NOTED.
C>GND STUD IS LOCATED ON THE BACK
OF THE AUTOPILOT COWUTER RACK.
[DI PART OF
ALLIED SIGNAL INSTL
KIT 050-03375-0001.
[I>PART
OF ALLIED
SIGNAL
KIT 050-03245-0000.
[~>GND STUD IS
LOCATED ON FUSELAGE BULKHEAD
156.00.
[E>PART OF ALLIED SIGNAL INSTL KIT 050-00398-0000(2 REQ)
[>GNOD STUD IS LOCATED ON FUSELAGE BULKHEAD 172.00.
[>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 FOLLOIING SPECS ARE PART OF THIS DRAWING:
CSAM012 SHIELDED CABLE INSTALLATION.
CES2716 WIRE TERMINATIONS.
[>,16GA WIRE IS PART OF GARMIN TERMINATED WIRE GROUP.
(U>PART OF GARMIN
KIT 011-01000-00
(REF).
<:3
PT903
-{-(16)-
REFER TO <3B
91-10-02
64 ROLL STR VALID
(WHT)
(DLU)
34 ROLL
STR
HI
36 ROLL
STR
LOW
67 DISCRETE OUT 1B
68 DISCRETE OUT 2B
69 DISCRETE OUT 3B
70 DISCRETE OUT 4B
71 DISCRETE OUT 5B
72 DISCRETE OUT 68
73 DISCRETE OUT 7B
74 DISCRETE OUT 8B
75 DISCRETE OUT 9B
77 DISCRETE OUTl10
3924149B3
DUAL AXIS AUTOPILOT
Figure
10 (Sheet
3)
© CESSNA AIRCRAFT COMPANY
22-10-04
0
0
Figure 10
Page 4
Feb 13/2006
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