Load for a test of the engine mount on the JA-400 aircraft according to UL-2 and LTF-UL
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F16%3A00301185" target="_blank" >RIV/68407700:21220/16:00301185 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Load for a test of the engine mount on the JA-400 aircraft according to UL-2 and LTF-UL
Original language description
The report specifies the load for strength testing of the engine mount structure in the ultralight airplane JA-400. There are mentioned size and position of the load required by regulation UL-2 a LTF-UL for the basic test cases representing possible loading generated during traffic and specific cases (required, side and ground).
Czech name
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Czech description
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Classification
Type
O - Miscellaneous
CEP classification
JT - Propulsion, engines and fuels
OECD FORD branch
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Result continuities
Project
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Continuities
N - Vyzkumna aktivita podporovana z neverejnych zdroju
Others
Publication year
2016
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů