Publication detail

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

HLINKA, J.

English title

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

Type

Peer-reviewed article not indexed in WoS or Scopus

Language

en

Original abstract

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.

Keywords in English

dependability Aircraft General Aviation failure rate probability

Released

2003-11-21

Publisher

Výzkumný a zkušební letecký ústav

ISSN

1211-877X

Book

Letecký zpravodaj

Journal

Letecký zpravodaj

Volume

2003

Number

3

Pages from–to

48–

Pages count

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"
}