190-01553-00
GTR 200 Installation Manual
Revision B
Page D-2
APPENDIX D Interconnect Examples
Figure D-2 GTR 200- Power & Ground/Intercom/GDU 37X Interconnect Example
s
s
s
s
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
*DISC1
*DISC2
MUSIC 1 IN LEFT
MUSIC 1 IN RIGHT
MUSIC 1 IN LO
AUX 1 AUDIO IN HI
AUX 1 AUDIO IN LO
LIGHTING BUS
AUX 2 AUDIO IN HI
AUX 2 AUDIO IN LO
*TRANSMIT INTERLOCK IN
*TRANSMIT INTERLOCK OUT
RECEIVER AUDIO OUT HI
RECEIVER AUDIO OUT LO
RS-232 IN
RS-232 OUT
NC
20
s
35
17
36
14
13
33
15
16
34
12
11
30
10
29
2
22
19
18
37
32
31
9
28
3
5
4
24
23
s
P2001
COM ANTENNA
P2002
GARMIN
7.5A CIRCUIT BREAKER 14V AIRCRAFT
5A CIRCUIT BREAKER 28V AIRCRAFT
NOTE 11
TO LIGHTING BUS NOTE 10
NOTE 9
NOTE 8
NOTE 8
RECORDER OUTPUT
NOTE 12
COPILOT HEADSET JACK
NOTE 5
COPILOT MIC JACK
NOTE 5
COPILOT PUSH TO TALK
PILOT HEADSET JACK
NOTE 5
PILOT MIC JACK
NOTE 5
PILOT PUSH TO TALK
14/28V AVIONICS POWER BUS
USE 20 AWG FOR POWER AND GROUND
NOTE 7
NOTE 7
J2001
GTR 200
s
s
3
STEREO AUDIO OUT LEFT
19
STEREO AUDIO OUT RIGHT
STEREO AUDIO OUT LO
20
MONO AUDIO OUT HI
MONO AUDIO OUT LO
1
18
13
RS-232 OUT 3
GARMIN
GDU 37X
J3701
P3701
NOTE 15
Содержание GTR 200
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