Garmin International Inc 0104455 Manual De Usuario

GTS Processor Installation Manual

Page B-10

190-00587-50

Revision A

ARINC 429 OUT 2 A

ARINC 429 OUT 2 B

23

24

ARINC 429 IN 2 A

ARINC 429 IN 2 B

33

36

31

s

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

s

s

4

GTX 

33/33D

330/330D

33

36

31

30

28

GTX 

328

--

--

17

--

--

GTX 

327/32/

320A

ARINC 429 IN 2 A

ARINC 429 IN 2 B

33

36

31

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

30

28

GTX 

328

--

--

17

--

--

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