Eagle P139-HD, Руководство по установке

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Geneva Aviation, Inc. www.GenevaAviation.com
GA182-8 Rev D P139-HD Digital Audio System 4 of 16
Cat.
No.
UPC
Body
Width
In.
Length
In.
Max.
Wire
Bundle
Dia. In.
Military
Standard
Part No.
Tensile
Strength
Lb.
TY23M 82436 .091 3.62 .625 MS3367-4 18
TY24M 82447 .140 5.50 1.125 MS3367-5 40
TY25M 82457 .184 7.31 1.750 MS3367-1 50
1.7. The aircraft into which this product will be installed may be a new aircraft or
an aircraft that has been in service. The configuration of the wiring and
cabling will vary from aircraft to aircraft. The installation of the Geneva
Aviation Audio System should use existing wire and cable runs when
possible as it will not interfere with the existing aircraft wiring.
1.8. These instructions call out cables by reference to the drawing that defines
the cable construction details. The installer may, at the installe
r’s
discretion, substitute connectors, wire type, and connection details, so long
as the final installations operate correctly and meets FAA standards.
1.9. The Router features a COM1 Isolate mode that automatically connects the
pilot’s headset and mic switches directly to COM1 in the event of power
loss or failure of the Audio Router. The pilot may also activate the COM1
Direct mode using the EMERG/NORMAL switch on the G13115 and
G13116 control panels. This feature may also be set up for the Copilot to
activate a COM2 Isolate mode using the EMERG/NORMAL switch on the
copilot control panel.
1.10. For Non-Pilot positions, Control Panels G13115NS or G13116NS may be
used. The panels do not have an internal COM1, COM2 isolate switch.
For these panels, do not connect to the COM1 or COM2 circuits shown in
wiring diagrams G13004.