APPENDIX A
A.1
Continued Airworthiness
Other than for regulatory periodic functional checks, maintenance of the GTX 330 is "on condition" only. Refer to
the GTX 330 Maintenance Manual, (Garmin P/N 190-00207-05). Periodic maintenance of the GTX 330 is not
required.
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 construe 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 GTX 330 unit installation. Some of the checklist items do not apply, in
which case they should be marked "N/A" (Not Applicable).
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS, GARMIN GTX 330
1.
Introduction
[Aircraft that has been altered: Registration (N-) number, Make, Model and Serial Number]
Content, Scope,
Purpose and Arrangement:
the modification of the above aircraft by installation of a GARMIN GTX 330.
Applicability:
Definitions and Abbreviations:
Precautions:
Units of Measurement:
Referenced Publications: GARMIN GTX 330 Installation Manual, P/N 190-00207-02
GARMIN GTX 330 Maintenance Manual, P/N 190-00207-05
GARMIN STC # [applicable STC number for the specific model installed, refer to Appendix B of this manual].
GARMIN GTX 330 Pilot's Guide, P/N 190-00207-xx.
Distribution:
2.
Description of the Alteration
Installation of the GARMIN GTX 330, with interface to Encoding Altimeter or Blind Encoder. Refer to
section 4 and figures 4-1 and 4-2 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 GTX 330 Pilot's Guide.
4.
Servicing Information
N/A
GTX 330 Installation Manual
190-00207-02
CERTIFICATION DOCUMENTS
This document identifies the Instructions for Continued Airworthiness for
Applies to aircraft altered by installation of the GARMIN GTX 330.
None, N/A.
None, N/A.
None, N/A.
This document should be a permanent aircraft record.
Page A1
Rev. 1
Печатать страницу