L 13 Main Spar Fatigue

Result code in 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>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

L 13 Main Spar Fatigue

Original language description

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.

Czech name

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Czech description

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Type

D - Article in proceedings

CEP classification

JU - Aeronautics, aerodynamics, aeroplanes

OECD FORD branch

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Project

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Continuities

S - Specificky vyzkum na vysokych skolach

Publication year

2011

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection

New Trends in Civil Aviation 2011

ISBN

978-80-01-04893-1

ISSN

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e-ISSN

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Number of pages

6

Pages from-to

34-39

Publisher name

ČVUT v Praze a OSL ČR

Place of publication

Praha

Event location

Prague

Event date

Sep 26, 2011

Type of event by nationality

EUR - Evropská akce

UT code for WoS article

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