Continued Airworthiness
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AC 33.4-1 - Instructions for Continued Airworthiness
www.faa.govINSTRUCTIONS FOR CONTINUED AIRWORTHINESS AND MANUFACTURER’S MAINTENANCE MANUALS HAVING AN AIRWORTHINESS LIMITATIONS SECTION (§ 21.50(b)) 5. GUIDANCE FOR § 21.50(b). a. General. Section 21.50(b) requires that the holder of a design approval for an aircraft engine for which application was made after January 28, 1981, …
GTN 625/635/650/725/750 and GMA 35 Instructions for ...
static.garmincdn.comInstructions for Continued Airworthiness Page 3 of 12 1. INTRODUCTION 1.1 Purpose This document is designed for use by the installing agency of the Garmin GTN 6XX/7XX Navigators and GMA 35 audio panel as Instructions for Continued Airworthiness in response to 14 CFR § 23.1529, and Part 23 Appendix G.
The Aircraft Maintenance Program and its importance on ...
fenix.tecnico.ulisboa.ptThe ultimate responsibility for Continued Airworthiness is assigned in ICAO Annex 8 to the State of Design but the programme to achieve it is a matter for the State of Registry. In Europe, the Aviation Authority in title is EASA (European Aviation Safety Agency), which will be presented in the following paragraphs.
EUROPEAN MILITARY AIRWORTHINESS REQUIREMENT …
eda.europa.euOct 04, 2016 · Military Airworthiness Authority (NMAA) in a form and manner established by such authority. 145.A.20 Terms of approval The maintenance organisation shall specify the scope of work deemed to constitute approval in its Maintenance Organisation Exposition (MOE). (Appendix II to this EMAR
Approval of Part 145 Organizations - ICAO
www.icao.intthe airworthiness of maintenance work undertaken on products parts and appliances Form 1 can be either pre-printed or computer generated Block 12 (Remarks) must reference the data used (including revision status) The Form 1 must comply with the format inAppendix II toAnnex 1 (Part M).As from 28 September 2010.