Detail publikace

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

HLINKA, J.

Originální název

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

Typ

článek v časopise - ostatní, Jost

Jazyk

angličtina

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

dependability Aircraft General Aviation failure rate probability

Autoři

HLINKA, J.

Rok RIV

2003

Vydáno

21. 11. 2003

Nakladatel

Výzkumný a zkušební letecký ústav

ISSN

1211-877X

Periodikum

Letecký zpravodaj

Ročník

2003

Číslo

3

Stát

Česká republika

Strany od

48

Strany do

51

Strany počet

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"
}