Dependability Assessment Possibilities for General Aviation Class Aircraft during Development and Certification
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F03%3APU38536" target="_blank" >RIV/00216305:26210/03:PU38536 - isvavai.cz</a>
Result on the web
—
DOI - Digital Object Identifier
—
Alternative languages
Result language
angličtina
Original language name
Dependability Assessment Possibilities for General Aviation Class Aircraft during Development and Certification
Original language description
General aviation (GA) aircraft are designed according to FAR-23 / JAR-23 regulations. Regulations use "direct" (deterministic) requirements for basic structure of an airplane, while for the rest of critical systems it uses "universal" (dependability) requirements. Contribution shows basic possibilities of dependability parameters estimation for parts designed in accordance with "direct" requirements. Second part of the text deals with possibilities of creation of simple software application for dependaability assessment.
Czech name
—
Czech description
—
Classification
Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
—
Result continuities
Project
<a href="/en/project/LN00B051" target="_blank" >LN00B051: Aerospace research centre (ARC)</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2003
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
Letecký zpravodaj
ISSN
1211-877X
e-ISSN
—
Volume of the periodical
2003
Issue of the periodical within the volume
3
Country of publishing house
CZ - CZECH REPUBLIC
Number of pages
4
Pages from-to
48-51
UT code for WoS article
—
EID of the result in the Scopus database
—