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4 th Edition Rev. 9 August 2012 Company Profile EASA Parte 145 e Parte 21 EN 9100:2009; EN 9110:2009 EN 9120:2009; ISO 9001:2008 AER-Q-2120;20 июл. 2012 г. — EASA PART 21 Design Organization. Certificat d'approbation n. EASA 21. Quality Manual for details VOR/LOC CONVERTER & G/S INDICATOR. 21 июн. 2019 г. — English Edition: 21 June 2019 EASA Safety Information Bulletin No. converter, recirculation fans, HEPA filters, etc.). Автор: EH Rocklyn · 1965 — 21(n.3). 9). ,Dialogo fino a larrivederlal. Unit. 4,5,6. 10) Domande1 If in Italian you have occasion to refer to a part or porticn of. 14 июл. 2021 г. — EXECUTIVE SUMMARY. The objective of this Notice of Proposed Amendment (NPA) is to maintain a high level of safety for unmanned.AW189 Final Report 05052015.pdf - EASAeasa.europa.eu › system › files › dfueasa.europa.eu › system › files › dfu applicable requirements of EASA part 21. - Necessary tooling for the manufacturing of the tanks is under partner responsibility and tooling shall be. 5 мая 2015 г. — M. Alessandro Celona. Pilot / OEB Member. ENAC /ITALY Flight Inspector - Helicopters. M. Jean-Marc Sacazes. EASA – Section Manager. Автор: J Czarnigowski · 2017 · Цитируется: 2 — The analysis covers the EASA decision on certification specifications as well as recommended means of compliance and related standards on testing and designing 5 янв. 2017 г. — 1. in compliance with the applicable requirements of EMAR M and EMAR 145; If the applicant holds an EASA Part 66. 20 июл. 2012 г. — “EASA PART 21 Design Organization” Automatic, semi-automatic and manual test benches (III level G.S. RECEIVER VOR-LOC CONVERTER.