User's Manual

GTS Processor Installation Manual Page B-10
190-00587-50 Revision A
APPENDIX B Interconnect Examples
Figure B-10 GTS Processor Dual Transponder Interconnect Example
GTS 820/850
ARINC 429 OUT 2 A
ARINC 429 OUT 2 B
23
24
P8001
GARMIN
TRANSPONDER #1
ARINC 429 IN 2 A
ARINC 429 IN 2 B
33
36
31
P3301
s
NOTES:
1. ALL WIRES 24 AWG OR LARGER UNLESS OTHERWISE SPECIFIED.
2. GROUND DESIGNATIONS: SHIELD BLOCK GROUND AIRFRAME GROUND
3. AT THE GTS 8XX, CONNECT SHIELD GROUNDS TO THE CONNECTOR BACKSHELL -- THE SHIELD LEADS MUST BE LESS
THAN 3.0 ". CONNECT OTHER SHIELD GROUNDS TO AIRCRAFT CHASSIS WITH AS SHORT A CONDUCTOR AS PRACTICAL.
4. CONFIGURE THE ARINC 429 BUS SPEED TO MATCH THE GTS PROCESSOR OUTPUT SPEED.
5. REFER TO GARMIN TRANSPONDER INSTALLATION MANUAL FOR ADDITIONAL INSTALLATION DETAILS.
7. IF ONLY ONE TRANSPONDER IS INSTALLED, CONNECT AS SHOWN FOR TRANSPONDER #1.
s
EXTERNAL SUPPRESSION I/O
48
EXTERNAL SUPPRESSION I/O
ARINC 429 IN 2 A
ARINC 429 IN 2 B
25
26
ARINC 429 OUT 2 A
ARINC 429 OUT 2 B
30
28
s
P8002
s
s
4
GTX
33/33D
330/330D
33
36
31
P3281
30
28
GTX
328
--
--
17
P3271
--
--
GTX
327/32/
320A
GARMIN
TRANSPONDER #2
ARINC 429 IN 2 A
ARINC 429 IN 2 B
33
36
31
P3301
EXTERNAL SUPPRESSION I/O
ARINC 429 OUT 2 A
ARINC 429 OUT 2 B
30
28
s
s
GTX
33/33D
330/330D
33
36
31
P3281
30
28
GTX
328
--
--
17
P3271
--
--
GTX
327/32/
320A
13
EXTERNAL STANDBY SELECT
13
EXTERNAL STANDBY SELECT
TRANSPONDER 2
TRANSPONDER 1
TO DME/UAT
ARINC 429 OUT 3 A
ARINC 429 OUT 3 B
28
29
ARINC 429 IN 3 A
ARINC 429 IN 3 B
30
31
6. THE GTX 330 ARINC 429 OUT 2 PORT IS HIGH-IMPEDANCE WHEN THE EXTERNAL STANDBY SELECT INPUT IS
GROUNDED. THIS ALLOWS ARINC 429 OUTPUTS FROM DUAL GTX 330 UNITS TO BE HARD-WIRED TOGETHER SINCE THE
EXTERNAL STANDBY SELECT INPUT WILL BE ACTIVE FOR ONE OF THE TWO GTX 330’S AT ANY GIVEN TIME.
8. THE GTS PROCESSOR IS NOT TO BE INSTALLED IN AN AIRCRAFT WITH A TSO-C119a-ONLY COMPATIBLE TRANSPONDER.
DRAFT