GH-3100
Installation & Operation Manual
Page 2-6
Installation
TP-559
March 30, 2017
Revision K
2.3.3 Electrical Connections
1.
The installer must take the following into consideration before installing the GH-3100 Electronic
Standby Instrument System:
•
All wiring must be in accordance with industry-accepted methods, techniques, and practices.
Refer to FAA Advisory Circular AC43.13-1A for aircraft wiring requirements.
•
The installer is responsible for supplying wires, cables and connectors.
•
All wires should be 22 AWG unless otherwise noted. Use M22759 or equivalent wire and
M27500 or equivalent for twisted shielded wired for installation.
•
The length and routing of the external cables must be carefully studied and planned before
attempting installation of the equipment.
•
Wire-marking identification is at the discretion of the installer.
•
The GH Indicator and Magnetometer should be placed on separate circuit breakers.
•
Use of any cable not meeting specification voids all warranties.
2.
Refer to Figure 2-2 for connector pin assignments for the GH-3100.
3.
Refer to Figure 2-4 or Figure 2-8 for interconnect wiring diagram information.
4.
Figure 2-3 shows specific manufacturing requirements for the GH-3100 mating connector.
Figure 2-3: GH-3100 Cable Assembly (J1)
