Continued Airworthiness - Garmin GTX 330 Installation Manual

A.2 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.
Refer to EASA ED Decision No 2003/19/RM, Annex II, Acceptable Means of Compliance to Part-145,
Page 161. This document can be accessed via the internet address
http://easa.europa.eu/agency-measures/docs/agency-decisions/2003/2003-019-RM/
decision_ED_2003_19_RM.pdf.
Refer to FAA Order 8300.10, Airworthiness Inspector's Handbook, Volume 2, Chapter 1, Section 1.21,
Instructions for Continued Airworthiness. This document can be accessed via the internet address
http://www.faa.gov/regulations_policies/handbooks_manuals/examiners_inspectors/.
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.
190-00207-02 GTX 330 Installation Manual
Rev. U Page A-3