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500 SERIES INSTALLATION MANUAL

Page A-1

190-00181-02

Rev

Appendix A. CERTIFICATION DOCUMENTS

A.1 CONTINUED

AIRWORTHINESS

This section provides assistance to the installing agency in preparing Instructions for Continued
Airworthiness (ICA) in response to Bulletin Number HBAW 98-18, “Checklist for Instructions for
Continued Airworthiness for Major Alterations Approved Under the Field Approval Process”, effective
10/7/98.

Aviation Authority approved installers are hereby granted permission to reference appropriate service
instructions and excerpts from this Installation Manual to accomplish the Instructions for Continued
Airworthiness. This permission does not constitute suitability of the documents. It is the applicant’s
responsibility to determine the suitability of the documents for the ICA.

Following is a suggested ICA for a Garmin 500 Series unit installation. Some of the checklist items do not
apply, in which case they should be marked “N/A” (Not Applicable). In this sample, square braces are
used to indicate instances where explicit words should be substituted (e.g., replace “[500 Series unit]” with
“GNS 530”).

Instructions for Continued Airworthiness, Garmin [500 Series unit]

1. Introduction

[Aircraft that has been altered: Registration (N-) number, Make, Model and Serial Number]

Content, Scope,
Purpose and Arrangement:

This document identifies the Instructions for Continued Airworthiness
for the modification of the above aircraft by installation of a Garmin
[500 Series unit].

Applicability:

Applies to aircraft altered by installation of the Garmin [500 Series
unit].

Definitions and Abbreviations: None, N/A.
Precautions: None,

N/A.

Units of Measurement:

None, N/A.

Referenced Publications:

Garmin 500 Series Installation Manual, P/N 190-00181-02
Garmin [500 Series unit] Maintenance Manual, P/N [190-00181-05 for
GNS 530, 190-00181-65 for GPS 500].
Garmin STC # [applicable STC number for the specific model
installed, refer to Appendix B of this manual].
Garmin Sample Flight Manual Supplement, P/N [part number of the
applicable SAFMS, refer to section 3.1 of this manual].
Garmin [500 Series unit] Pilot’s Guide, P/N [part number of the
applicable Pilot’s Guide].

Distribution:

This document should be a permanent aircraft record.

2. Description of the Alteration

Installation of the Garmin [500 Series unit], with interface to external altitude encoder and CDI
[include other equipment/systems as appropriate]. Refer to section 4 of this manual for interconnect
information. Antenna installation, removal and replacement should be in accordance with applicable
provisions of AC43.13-1B and 43.13-2A.

3. Control, Operation Information

Refer to the [500 Series unit] Pilot’s Guide.

4. Servicing Information

N/A

5. Maintenance Instructions

Maintenance of the [500 Series unit] is ‘on condition’ only. Periodic maintenance is not required.
Refer to the [500 Series unit] Maintenance Manual.