
190-01553-00 GTR 200 Installation Manual
Revision G Page D-7
APPENDIX D Interconnect Examples
Figure D-7 Dual GTR 200/GMA 240 Interconnect Drawing
PO W
ER
POW
ER
G
ND
PI
LO
T
MI
C
HI
PI
LO T
M I
C
L
O
1
*P
TT
PI
LO
T
R
E C
E
I
VE R
AU DI
O
OU T
HI
RE C
E I
V
E
R
AUD
I
O
O
UT
LO
2
0
35
1
7
3
6
10
29
P2001
GARMIN
7.5A CIRCUIT BREAKER 14V AIRCRAFT
7.5A CIRCUIT BREAKER 14V AIRCRAFT
5A CIRCUIT BREAKER 28V AIRCRAFT
5A CIRCUIT BREAKER 28V AIRCRAFT
*
DI
S
C1
*
DI
S
C2
2
2
2
NOTE 8
NOTE 8
AVIONICS POWER BUS
USE 20 AWG FOR POWER AND GROUND
USE 20 AWG FOR POWER AND GROUND
J2001
COM ANTENNA
P2002
GTR 200 AS COM 1
12
COM 1 MIC KEY* OUT
11
COM 1 MIC AUDIO OUT HI
COM 1 AUDIO LO
10
COM 1 AUDIO IN HI
GARMIN
GMA 240
J2401
P2401
27
ID IN
ID LO
*TRANSMIT INTERLOCK IN
*TRANSMIT INTERLOCK OUT
*TRANSMIT INTERLOCK OUT
P
O
WER
POW ER GND
PI
LO T
M
IC HI
PIL
O
T M
I
C
L
O
1
*P T T PILO T
R E CE IVE R AUDIO OU T
H
I
RE CE IVE R AUD I
O
OU T LO
2
0
35
17
3
6
10
29
P2001
GARMIN
7.5A CIRCUIT BREAKER 14V AIRCRAFT
7.5A CIRCUIT BREAKER 14V AIRCRAFT
5A CIRCUIT BREAKER 28V AIRCRAFT
5A CIRCUIT BREAKER 28V AIRCRAFT
*
DISC1
*DISC
2
2
22
NOTE 8
NOTE 8
AVIONICS POWER BUS
USE 20 AWG FOR POWER AND GROUND
USE 20 AWG FOR POWER AND GROUND
J2001
COM ANTENNA
P2002
30
COM 2 MIC KEY* OUT
COM 2 MIC AUDIO OUT HI
COM 2 AUDIO LO
14
COM 2 AUDIO IN HI
13
27
ID IN
ID LO
*TRANSMIT INTERLOCK IN
*TRANSMIT INTERLOCK OUT
GTR 200 AS COM 2
TIE TOGETHER TO IDENTIFY GTR AS COM 2.
TIE TOGETHER TO IDENTIFY GTR AS COM 2.
SEE NOTE 16.
LEAVE OPEN
TO IDENTIFY
AS COM 1.
SEE NOTE 16
J2002
J2002
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