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6 POST INSTALLATION CONFIGURATION AND CHECKOUT
6.1
System Configuration Overview
The required GTX 35R/45R configuration and checkout procedures are as follows:
•
Complete the installation checks.
•
Configure the GTX 35R/45R for the specified installation.
•
Complete ground checks to make sure it interfaces to external equipment.
6.2
Mounting, Wiring, and Power Checks
Examine the wire harness to make sure the connection to aircraft systems and avionics equipment is
correct before the unit is energized. Point-to-point continuity must be examined to expose any faults such
as shorting to ground or wiring discrepancies. All faults or discrepancies must be corrected before
continuing.
Before and during the installation make sure:
•
All cables are properly attached.
•
Shields are connected to connector shield blocks.
•
Movement of the flight and engine controls through the full range of motion do not touch cabling
and control systems.
•
Wire is installed as described in section 3.14.
Make sure these items are completed after the installation or a continuity check.
•
Power and ground checks.
•
Faults and discrepancies are corrected.
•
Installation rack is correctly attached.
•
Unit is correctly seated in the installation rack.
190-01499-10
Rev. 1
GTX 35R/45R Installation Manual (Non-Certified Aircraft)
Page 6-1
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