L 13 Main Spar Fatigue

Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21260%2F11%3A00185197" target="_blank" >RIV/68407700:21260/11:00185197 - isvavai.cz</a>
Výsledek na webu
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Jazyk výsledku
angličtina
Název v původním jazyce
L 13 Main Spar Fatigue
Popis výsledku v původním jazyce
This paper presents most important information concerning the problem of main spar fatigue cracking occurred in L-13 "BLANIK" glider. It reviews the L-13 type design certification and fatigue evaluation history. The basic methods of fatigue evaluation inaeroplane structure are explained. The paper also focuses on the recent fatal accident caused by main spare fatigue in 2010. Mandatory actions required by Civil Aviation Authorities as a result of this accident are reviewed. There are introduced some examples of existing solutions for continuing airworthiness and best practices for dealing with fatigue issues in aging aeroplanes structures.
Název v anglickém jazyce
L 13 Main Spar Fatigue
Popis výsledku anglicky
This paper presents most important information concerning the problem of main spar fatigue cracking occurred in L-13 "BLANIK" glider. It reviews the L-13 type design certification and fatigue evaluation history. The basic methods of fatigue evaluation inaeroplane structure are explained. The paper also focuses on the recent fatal accident caused by main spare fatigue in 2010. Mandatory actions required by Civil Aviation Authorities as a result of this accident are reviewed. There are introduced some examples of existing solutions for continuing airworthiness and best practices for dealing with fatigue issues in aging aeroplanes structures.

Rok uplatnění
2011
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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