Genesys GDR- COM Series, Installation Manual, Page: 23 / 62

GDR-XXXX NAV/COM INSTALLATION MANUAL
64-000109 Page 23 of 62
CHAPTER 2 – SYSTEM INSTALLATION
CAUTION: It is critically important that this installation manual be read and understood completely
and thoroughly before starting component installation and wiring.
A successful installation should begin with careful consideration and planning of mounting
locations, cable routing and any associated airframe modifications that may be required.
The conditions and tests required for TSO approval of this article are minimum performance
standards. Those installing this article, on or in a specific type of class of aircraft, must determine
that the aircraft installation conditions are within the TSO standards. TSO articles must have a
separate approval for installation in an aircraft. This article may be installed only according to 14
CFR Part 43 or the applicable airworthiness requirements.
14. LIMITATIONS AND NOTES
A. Notes and Warnings
NOTE: No special airworthiness limitations exist. Maintenance is required per FAR
43.16 and FAR 91.403.
15. PRE-INSTALLATION INFORMATION
A. Always follow good avionics installation practices per FAA Advisory Circulars
43.13-1B, 43.13-2A, and AC 23-1311-1A or later FAA approved revisions of these
documents.
B. Follow the installation procedures in this chapter as it is presented for a successful
installation. Read and understand the entire chapter before beginning the
installation procedures. Perform the post installation checkout before closing the
work areas in case problems occur.
C.
Complete an electrical load analysis on the aircraft prior to starting modification to
ensure the aircraft electrical system has the ability to carry the GDR electrical load
per AC 43.13-1B, Chapter 11. Refer to Chapter 1, Table 3 for the power
consumption of each component. Record the aircraft electrical load; identify
system configuration and location of equipment on FAA Form 337.