190-01553-00
GTR 200 Installation Manual
Revision B
Page D-3
APPENDIX D Interconnect Examples
Figure D-3 GTR 200- Power & Ground/GMA 240/GNS 430/aera 79X Interconnect Example
s
POWER
POWER GND
PILOT MIC HI
PILOT MIC LO
1
*PTT PILOT
PILOT HEADSET LEFT
PILOT HEADSET RIGHT
PILOT HEADSET LO
COPILOT MIC HI
COPILOT MIC LO
*PTT COPILOT
COPILOT HEADSET LEFT
COPILOT HEADSET RIGHT
COPILOT HEADSET LO
RECEIVER AUDIO OUT HI
RECEIVER AUDIO OUT LO
20
35
17
36
10
29
15
16
34
12
11
30
MUSIC 1 IN LEFT
MUSIC 1 IN RIGHT
MUSIC 1 IN LO
AUX 1 AUDIO IN HI
AUX 1 AUDIO IN LO
AUX 2 AUDIO IN HI
AUX 2 AUDIO IN LO
19
18
37
32
31
9
28
P2001
GARMIN
7.5A CIRCUIT BREAKER 14V AIRCRAFT
5A CIRCUIT BREAKER 28V AIRCRAFT
*DISC1
*DISC2
2
22
NOTE 8
NOTE 8
AVIONICS POWER BUS
USE 20 AWG FOR POWER AND GROUND
J2001
COM ANTENNA
P2002
GTR 200
LIGHTING BUS
*TRANSMIT INTERLOCK IN
*TRANSMIT INTERLOCK OUT
3
5
4
TO LIGHTING BUS NOTE 10
RS-232 IN
RS-232 OUT
NC
24
23
s
4
COM MIC KEY
14
TRANSMIT INTERLOCK
GARMIN
GNS 430
J4002
P4002
30
COM 2 MIC KEY* OUT
15
COM 2 MIC AUDIO OUT HI
COM 2 AUDIO LO
14
COM 2 AUDIO IN HI
13
GARMIN
GMA 240
J2401
P2401
NOTE 13
s
14
13
33
NC
NC
NC
NC
NC
NC
NC
NC
NC
COM 1 MIC KEY* OUT
12
O
TX2 (DATA OUT) ORANGE WIRE
GARMIN
AERA 79X
B
POWER GROUND/DATA GROUND BLACK WIRE
NC
NC
NC
NC
NC
NC
NC
NOTE 15
Summary of Contents for GTR 200
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