Genesys GDR- COM Series, Installation Manual, Page: 43 / 62

GDR-XXXX NAV/COM INSTALLATION MANUAL
64-000109 Page 43 of 62
22. WIRING DIAGRAMS
This section will provide generic diagrams for installation of auxiliary equipment to the
GDR-XXXX. Refer to the aircraft wiring diagrams for actual connections.
NOTE: Wiring codes in the diagrams are for reference and may not reflect the actual wire
codes on the aircraft. Refer to the aircraft installation drawings for correct codes
and connections.
WIRING NOTES:
1. Unless noted otherwise, all new wire to meet MIL-W-22759/16 or later
revision. All shielded wire to be MIL-C-27500E with shields type (T) and
jackets type (14). For additional routing, bonding, and grounding details,
reference AC43-13-1B Chapter 11, Sections 9, 10, 11, and 15 or the
airframe manufacturers Maintenance Manual.
2. Grounds to be as short as possible unless otherwise indicated. Grounds
under 6 inches in length do not require a wire number. Shield preparation
should not exceed 3 inches from connector. Shield grounds may not be
accomplished by daisy-chaining. Splicing or individually grounding shields
to appropriate ground devices.
3. All wires 22AWG unless otherwise specified.
4. Small parts and electrical components required for installation that are not
specifically called out in the parts lists shall meet the requirement for
aerospace use as “Accepted Parts” or “Standard Parts”. Selection of these
parts shall be in accordance with guidance provided in FAA Advisory
Circular AC20-62D, Dated 5/24/96 or later revision.
5. Due to the many different configuration possibilities and options, the
drawings are divided into function groups (Power, Communications, etc.) to
allow flexibility in the installation.