Detail publikace

Dependability Assessment Possibilities for General Aviation Class Aircraft during Development and Certification

HLINKA, J.

Anglický název

Dependability Assessment Possibilities for General Aviation Class Aircraft during Development and Certification

Typ

Článek recenzovaný mimo WoS a Scopus

Jazyk

en

Originální abstrakt

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 dependability assessment.

Klíčová slova anglicky

dependability Aircraft General Aviation failure rate probability

Vydáno

2003-11-21

Nakladatel

Výzkumný a zkušební letecký ústav

ISSN

1211-877X

Kniha

Letecký zpravodaj

Časopis

Letecký zpravodaj

Ročník

2003

Číslo

3

Strany od–do

48–

Počet stran

4

BIBTEX


@article{BUT41322,
  author="Jiří {Hlinka}",
  title="Dependability Assessment Possibilities for General Aviation Class Aircraft during Development and Certification",
  journal="Letecký zpravodaj",
  year="2003",
  volume="2003",
  number="3",
  pages="4",
  issn="1211-877X"
}