Garmin GMX 200 Installation Manual - page 31
GMX 200 Installation Manual
Page 4-3
190-00607-04
Revision F
Pin #
I/O
Pin Name
Description
46
-
RESERVED
Do not connect
47 -
RESERVED
Do not connect
48 -
RESERVED
Do not connect
49 -
RESERVED
Do not connect
50 -
RESERVED
Do not connect
51
-
RESERVED
Do not connect
52
O
429 OUT 2A
ARINC 429 Output 2A (Weather Radar)
53
O
429 OUT 2B
ARINC 429 Output 2B (Weather Radar)
54
-
RESERVED
Do not connect
55
-
RESERVED
Do not connect
56
-
RESERVED
Do not connect
57
-
RESERVED
Do not connect
58
I
429 IN 1B
ARINC 429 Input 1B (Traffic)
59
I
429 IN 1A
ARINC 429 Input 1A (Traffic)
60
-
RESERVED
Do not connect
61
I
429 IN 2A
ARINC 429 Input 2A (TAWS)
62
I
429 IN 2B
ARINC 429 Input 2B (TAWS)
4.2
27B
Functional Descriptions
4.2.1
61B
Power
The GMX 200 will accept input power from 9 to 33 VDC. Both sets of power inputs must be connected
in the installation.
P2001-1 Aircraft
Power
P2001-16 Aircraft
Power
P2001-2 Power
Ground
P2001-12 Power
Ground
Refer to
X
Appendix E
X
for recommended power connections.
4.2.2
62B
Configuration Module
The GMX 200 stores installation-specific configuration information in an aircraft configuration module
located in the backshell of P2001. This eliminates the need to set up aircraft specific configuration items
again if a new GMX 200 is installed. The configuration module is mounted within the connector
backshell as described in Section
X
3.4.2.2
X
.
P2001-17 Configuration Module Clock (from GMX 200)
P2001-19 Configuration Module Data (bi-directional)
P2001-24 Configuration Module Power (from GMX 200)
P2001-27 Configuration Module Ground
Refer to
X
Appendix E
X
for interconnect information.