Garmin GDR 66, Инструкция по установке

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GDR 66 Installation Manual Page 3-1
190-00303-24 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 44 and 62-pin D-subminiature connectors.
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 harnesses in
accordance with aircraft manufacturer authorized interconnect standards.
Contacts for the 62 and 44 pin connectors must be crimped onto the individual wires of the aircraft wiring
harness. Tables 3-1 and 3-2 list contact part numbers (for reference) and recommended crimp tools.
Table 3-1: Pin Contact Part Numbers
Manufacturer 62 pin connector (P662), 44 pin connector (P661)
18-20 AWG
(Power Only)
22-28 AWG
Garmin P/N 336-00044-00 336-00021-00
Military P/N N/A M39029/58-360
AMP N/A 204370-2
Positronic N/A MC8522D
ITT Cannon N/A 030-2042-000
DRAFT