500 SERIES INSTALLATION MANUAL Page A-1P/N 190-00181-02 Rev GAppendix A. CERTIFICATION DOCUMENTSA.1 Continued AirworthinessThis section provides assistance to the installing agency in preparing Instructions for ContinuedAirworthiness (ICA) in response to Bulletin Number HBAW 98-18, “Checklist for Instructions forContinued Airworthiness for Major Alterations Approved Under the Field Approval Process”, effective10/7/98.Aviation Authority approved installers are hereby granted permission to reference appropriate serviceinstructions and excerpts from this Installation Manual to accomplish the Instructions for ContinuedAirworthiness. This permission does not construe suitability of the documents. It is the applicant’sresponsibility 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 notapply, in which case they should be marked “N/A” (Not Applicable). In this sample, square braces areused 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 Airworthinessfor 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 Seriesunit].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 190-00181-02Garmin [500 Series unit] Maintenance Manual, P/N [190-00181-05 forGNS 530, 190-00181-65 for GPS 500].Garmin STC # [applicable STC number for the specific modelinstalled, refer to Appendix B of this manual].Garmin Sample Flight Manual Supplement, P/N [part number of theapplicable SAFMS, refer to section 3.1 of this manual].Garmin [500 Series unit] Pilot’s Guide, P/N [part number of theapplicable Pilot’s Guide].Distribution: This document should be a permanent aircraft record.2. Description of the AlterationInstallation 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 interconnectinformation. Antenna installation, removal and replacement should be in accordance with applicableprovisions of AC43.13-1B and 43.13-2A.3. Control, Operation InformationRefer to the [500 Series unit] Pilot’s Guide.4. Servicing InformationN/A5. Maintenance InstructionsMaintenance of the [500 Series unit] is ‘on condition’ only. Periodic maintenance is not required.Refer to the [500 Series unit] Maintenance Manual.