User's Manual

GTS Processor Installation Manual Page 3-1
190-00587-50 Revision A
3 INSTALLATION PROCEDURE
3.1 Unpacking Unit
Carefully unpack the equipment and make a visual inspection of the unit for evidence of damage incurred
during shipment. If the unit is damaged, notify the carrier and file a claim. To justify a claim, save the
original shipping container and all packing materials. Do not return the unit to Garmin until the carrier has
authorized the claim. Retain the original shipping containers for storage. If the original containers are not
available, a separate cardboard container should be prepared that is large enough to accommodate
sufficient packing material to prevent movement.
3.2 Wiring Harness Installation
Allow adequate space for installation of cables and connectors. The installer shall supply and fabricate all
of the cables. All electrical connections are made through two 78-pin high-density D subminiature
connectors, and one 37-pin standard density connector. Section 4 defines the electrical characteristics of
all input and output signals. Required connectors and associated hardware are supplied with the connector
kit.
See Appendix B for examples of interconnect wiring diagrams. Construct the actual harness in accordance
with aircraft manufacturer authorized interconnect standards.
*Indicates plastic insertion/extraction tool
Table 3-1 Socket and Pin Contact Part Numbers
Manufacturer
78 Pin High Density D-Subminiature Connectors P8001 & P8002
37 Pin Standard Density D-Subminiature Connector P8003
19 Pin Circular Connector P651
High Density Pin (P8001
& P8002)
Standard Socket
(P8003)
18 AWG Socket
(P8003)
Garmin P/N 336-00021-00 336-00022-00 336-00023-00
Military P/N M39029/58-360 M39029/63-368 N/A
Table 3-2 Socket Contact MIL SPEC M39029/5-115 Crimp Tooling
Manufacturer
Hand Crimping
Tool
Positioner
Insertion/Extraction
Tool
Tools Option 1
Military P/N M22520/1-01 M22520/1-02 M81969/14-11*
Daniels AF8 TH1A M81969/14-11*
Tools Option 2
Military P/N M22520/2-01 M22520/2-02 M81969/14-11*
Daniels AFM8 K1S M81969/14-11*
DRAFT