Textron Cessna 182S - FIGURE 02 - GDL-69 A FIS DATA LINK

CESSNA AIRCRAFT
COMPANY
MODEL 182/T182
WIRING DIAGRAM
MANUAL
NOTES:
1. ALL WIRE 22AIG UNLESS OTHERWISE NOTED.
[c>GROUND SHIELDS
TO THE BACKSHELL OF THE
CONNECTOR USING
THE GARMIN SUPPLIED GROUNDING BLOCK ON THE CONNECTOR.
SHIELD
WIRES MUST
BE NO LONGER THAN
3'.
3. THE FOLLOWING SPECS ARE PART OF THIS DRAWING:
CSAMO12 SHIELDED CABLE INSTALLATION.
CES2716 *IRE
TERMINATIONS.
[>USE
392404
CABLE.
C:>DETAIL A SHOWS THE PHYSICAL LOCATION OF THE CONTACTS ON PC512.
[E>CONNECTORS
P11028
AND PC1009
ARE PART OF ECS
CABLE 500-96273-01.
[:>PART OF GARMIN CONNECTOR KIT 011-00997-00.
G[>INSTALL THE 50FFM-007-TNC ATTENUATOR DIRECTLY TO THE FIS RECEIVER.
O_>16
GAUGE WIRE IS PART OF
GRAMIN TERMINATED WIRE
GROUP.
I)-ft-' 2
:,)=t "
S> THE
WIRE LENGTH
BETWEEN
PC512 AND
JC523
SHOULD BE 10' +/- 0.5'.
_> P 531
AUDIO PANEL
U1531
37 AUDIO GROUND
18 AUDIO IN 1R
17 AUDIO IN 1L
56
AUDIO
IN
2L
57
AUDIO
IN 2R
76 AUDIO GROUND
P1533 <:
DATA LINK
(P691)
AUDIO LOW
17 ---
(ORN)-
AUDIO
OUT R
18---H
(BLU)-
AUDIO
OUT
L
19-I-----(HT)-
ETHERNET IN 1A 23-
ETHERNET IN 1B 22
ETHERNET OUT 1A 25
ETHERNET OUT B 24
AUDIO
INHIBIT
64
AFCT P1R 1 35
POWER
GND
78
(16)
[>
E>
(WHT/BLU)
(WHT/ORN)
(ORN/WHT)
(BLU/WHT)
JC031
6] sEL JC023
1 AVN
Ca PNL
DISC
REFER
TO
24-61-01
[ PF903
F REFER TO
91-10-02
> P1312
MFD
U1312
ETHERNET OUT 3A
11 ETHERNET
OUT 3E
12ETHERNET
IN 3A
1 ETHERNET
IN
38
_,ETHERNET IN 218
< ATTENUATOR
P1
1028
PI 1 028
DETAIL A
B>
PC1009
GDL-69A
FIS
DATA LINK
Figure
02 (Sheet
1)
© CESSNA AIRCRAFT COMPANY
23-20-01
E>
PC51
ENTERTAINMENT
AUDIO
rr JC523
PC523
(ORN)
(BLU)
(.HT)
(HT)-t
5----
(BLU)-H-6--
(ORN)-
7t --
j1i 3
C=
3927127_1
Figure
02
Page 0
Feb 13/2006
?0 40