Instruction Manual

GMX 200 P/N 190-00607-00 Rev.A
Instructions for Continued Airworthiness Page 4 of 7
9) MFD: Multi-Function Display unit
10) PMI: Primary Manufacturing Inspector
11) POI: Primary Operations Inspector
12) STC: Supplemental Type Certificate
13) TC: Type Certification or Type Certificate
14) TSO: Technical Standard Order
2. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
2.1 Introduction
Content, Scope, Purpose and Arrangement: This document identifies the Instructions for
Continued Airworthiness for the modification of the
aircraft by installation of the Garmin GMX 200.
Applicability: Applies to aircraft altered by installation of the
Garmin GMX 200.
Definition of Abbreviations: See Section 1.6
Precautions: None
Units of measurement: None
Referenced publications:
(or later FAA approved revisions)
190-00607-04 Rev. B GMX 200 Installation
Manual
005-C0315-00 Rev. A GMX 200 STC Master Data
List
Retention: This document, or the information contained within,
will be retained in the aircraft’s permanent records.
2.2 Description of Alteration
Installation of the Garmin GMX 200 and other system interfaces. The GMX 200 consists of a LCD
display, keypads, keyboard and rotary knob.
2.3 Control, Operating Information
See the GMX 200 Installation Manual, listed under the reference documentation in paragraph 2.1 of this
document, for system operation and self-test information.
2.4 Servicing Information
None. In the event of system failure, return the unit to the manufacturer or an approved Garmin repair
station.