Garmin SA01692SE Instruction Manual

GMX 200

Instructions for Continued Airworthiness

FAA STC Project No. ST9731SE-A

Document Number 190-00607-00 Rev. A

Garmin Ltd. Or its subsidiaries

c/o Garmin International, Inc.

1200 E. 151st Street

Olathe, Kansas 66062 USA

Confidential

This drawing and the specifications contained herein are
the property of Garmin Ltd. or its subsidiaries and may not
be reproduced or used in whole or in part as the basis for
manufacture or sale of products without written permission.

Record of Revision

Rev. Date Description of Change

1 6/02/06 Initial Release
A 6/19/06 Production Release

1.

INTRODUCTION...................................................................................................................3

1.1 PURPOSE ............................................................................................................ 3

1.2 Scope....................................................................................................................3

1.3 Document Control.................................................................................................3

1.4 Airworthiness Limitations Section......................................................................... 3

1.5 Permission to Use Certain Documents.................................................................3

1.6 Definitions.............................................................................................................3

2. INSTRUCTIONS FOR CONTINUED AIRWORTHINESS .................................................... 4

2.1 Introduction...........................................................................................................4

2.2 Description of Alteration........................................................................................4

2.3 Control, Operating Information............................................................................. 4

2.4 Servicing Information............................................................................................ 4

2.5 Periodic Maintenance Instructions........................................................................5

2.6 Troubleshooting Information................................................................................. 5

2.7 Removal and Replacement Information...............................................................5

2.8 Diagrams...............................................................................................................6

2.9 Special Inspection Requirements.........................................................................6

2.10 Application of Protective Treatments....................................................................6

2.11 Data Relative to Structural Fasteners................................................................... 6

2.12 Special Tools ........................................................................................................ 6

2.13 Additional Instructions for Aircraft Operating under FAR 121/135 ....................... 6

2.14 Overhaul Period....................................................................................................6

2.15 ICA Revision and Distribution............................................................................... 6

2.16 Assistance.............................................................................................................7

2.17 Implementation and Record Keeping...................................................................7

GMX 200 P/N 190-00607-00 Rev.A
Instructions for Continued Airworthiness Page 2 of 7

1. INTRODUCTION

1.1 PURPOSE

This document is designed for use by the installing agency of the Garmin GMX 200 as Instructions for
Continued Airworthiness in response to Federal Aviation regulation (FAR) Part 23.1529, and Part 23
Appendix G. They include information required by the operator to adequately maintain the Garmin GMX

200.

1.2 Scope

This document identifies the Instruction for Continued Airworthiness for modification of the aircraft for
installation of the Garmin GMX 200.

1.3 Document Control

This document shall be released, archived, and controlled in accordance with the Garmin document
control system. When this document is revised, refer to Section 2.15 for information on how to gain FAA
acceptance or approval and how to notify customers of changes.

1.4 Airworthiness Limitations Section

There are no additional Airworthiness Limitations as defined in 14 CFR § 23, Appendix G. G23.4 that
result from this modification. The Airworthiness Limitations section is FAA approved and specifies
maintenance required under §§43.16 and 91.403 of the Federal Aviation Regulations unless an
alternative program has been FAA approved.

1.5 Permission to Use Certain Documents

Permission is granted to any corporation or person applying for approval of a Garmin GMX 200 to use
and reference appropriate STC documents to accomplish the Instructions for Continued Airworthiness
and show compliance with STC engineering data. This permission does not construe suitability of the
documents. It is the responsibility of the applicant to determine the suitability of the documents for the
ICA.

1.6 Definitions

The following terminology is used within this document:

1) AC: Advisory Circular

2) ACO: Aircraft Certification Office

3) AEG: Aircraft Evaluation Group

4) CFR: Code of Federal Regulations

5) DER: Designated Engineering Representative

6) FAA: Federal Aviation Administration

7) IAW: In Accordance With

8) ICA: Instructions for Continued Airworthiness

GMX 200 P/N 190-00607-00 Rev.A
Instructions for Continued Airworthiness Page 3 of 7