Univerzitná knižnica - Zborníky

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    Zmeny a doplnenia EASA časť 145 a ich vplyv na CAMO
    (University of Žilina, 2024) Krajcer, Marek; Urminský, Tomáš
    EASA Part 145, a framework that governs the approval and operation of maintenance organisations, is one of the key elements in the regulatory environment targeting the technical condition of aircraft. Changes and amendments to EASA Part 145, which followed the adoption of Commission Regulation (EU) No. 1321/2014, also affect Continuing Airworthiness Management Organizations (CAMO). This paper examines how these changes of integration are reflected in the actual operation of CAMO helping to understand the degree of interconnection between the aircraft maintenance field and the management of continuing airworthiness. The introductory chapters provide a theoretical overview of the regulations, focusing on EASA Parts 145, M, and CAMO. Based on this theoretical framework, the study presents an in-depth analysis of recent changes and amendments to EASA Part 145, identifying their impact on CAMO operations. The enrichment of the data stems from a survey distributed among experts in practice, capturing insights and firsthand experience. This survey, a central part of the paper, explores their views on the consequences of implementing changes and the challenges they face.
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    VYHODNOTENIE OPODSTATNENOSTI KÚPY A UVEDENIA LIETADLA DO KOMERČNEJ PREVÁDZKY)
    (Žilinská univerzita v Žiline, 2020) László, Michal; Urminský, Tomáš
    The issue of assessing the condition of an aircraft at lease or sale is now becoming a frequented issue by airlines. The priority is to procure the aircraft in an acceptable technical condition and without hidden defects that could have a negative impact on its subsequent operability. Responsibility for this challenging task is taken over by experienced personnel from the continuing airworthiness management environment, with the help of certified maintenance technicians for the aircraft type. The article is focused on the evaluation of the condition of the aircraft of the turboprop aircraft ATR 72-212 for regional air connections. The subject of the analysis were its main components - engines, landing gear, propellers, reducers. These components together form a major part of the value of the aircraft and therefore it is important to focus on them in detail. The requirement was a minimum 2-year maintenance-free condition to ensure the operational needs of the airline. In the model situation, we then consider conversion to the cargo version after 2 years of operation. The conclusion of the article presents the total costs associated with overhauls and replacement of components and management of work associated with the re-commissioning.