Dwg. Number: 005-C0315-00 Rev. A Confidential This drawing and the specifications contained herein are the property of GARMIN Ltd. or its subsidiaries as the basis for manufacture or sale of products without written permission. Record of Revision Description of Change...
5. SPECIAL INSTALLATION INSTRUCTIONS ... 6 Table 1 STC Data ... 4 Table 2 Related Data (Substantiating Data)... 4 Table 3 Required Equipment List ... 5 GMX 200 STC Installation STC Master Data List 005-C0315-00 Rev A Page 2 of 6...
STC which is not required for installation. Scope This document applies to the installation of the GMX 200 units when installed IAW the data listed in this document on the Approved Model List aircraft as defined for this STC. This document includes general installation requirements, special installation instructions, and it provides an index of STC data including both data required for installation and data associated with the STC, but not required for installation.
Garmin 190-00607-04 2.1.2 Continued Airworthiness Instructions for continued airworthiness are found in Garmin document number 190-00607-00 Instructions for Continued Airworthiness. See Table 1 for document revision. Substantiating Data The documents listed in Table 2, or later FAA-approved revisions, contain information related to this STC but are not required for follow-on installations.
All wire used in the installation shall be of appropriate standard aircraft quality grade and size as described in AC 43.13-1B, Chapter 11, Sections 5-20. Circuit Protection All GMX 200 unit modification circuits shall be protected in accordance with AC 43.13-1B, Chapter 11, Section 4, Circuit Protection Devices. Electrical Load Analysis An electrical load analysis shall be performed on each aircraft, as described in AC 43.13-1B, Chapter 11...