RELIABILITY OF GENERAL AVIATION CLASS AIRCRAFT MECHANICAL SYSTEMS

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F03%3APU37506" target="_blank" >RIV/00216305:26210/03:PU37506 - isvavai.cz</a>

Výsledek na webu

—

DOI - Digital Object Identifier

—

Jazyk výsledku

angličtina

Název v původním jazyce

RELIABILITY OF GENERAL AVIATION CLASS AIRCRAFT MECHANICAL SYSTEMS

Popis výsledku v původním jazyce

In the last years there has been significant growth in complexity of GA (General Aviation) class airplanes as well as in numbers of those airplanes. Together with this fact, new reliability assessment methods were used to provide sufficient level of safety of some systems. Also airworthiness authorities included requirements dealing with this fact into regulations used for GA aircraft certification. Most commonly used regulations, FAR-23 and JAR-23, give "direct" requirements for design of several maincomponents of an airplane and "universal" (dependability) requirements for the rest of systems. Dependability requirements are based on downgraded transport aircraft category requirements (FAR/JAR-25) and were established on results of accident reports analysis. Reports indicated overall goals for safety requirements. Subsequently typical number of critical subsystems on a common GA aircraft was found and reliability requirements for each subsystem were established so the overall safety

Název v anglickém jazyce

RELIABILITY OF GENERAL AVIATION CLASS AIRCRAFT MECHANICAL SYSTEMS

Popis výsledku anglicky

In the last years there has been significant growth in complexity of GA (General Aviation) class airplanes as well as in numbers of those airplanes. Together with this fact, new reliability assessment methods were used to provide sufficient level of safety of some systems. Also airworthiness authorities included requirements dealing with this fact into regulations used for GA aircraft certification. Most commonly used regulations, FAR-23 and JAR-23, give "direct" requirements for design of several maincomponents of an airplane and "universal" (dependability) requirements for the rest of systems. Dependability requirements are based on downgraded transport aircraft category requirements (FAR/JAR-25) and were established on results of accident reports analysis. Reports indicated overall goals for safety requirements. Subsequently typical number of critical subsystems on a common GA aircraft was found and reliability requirements for each subsystem were established so the overall safety

Druh

D - Stať ve sborníku

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

—

Projekt

<a href="/cs/project/LN00B051" target="_blank" >LN00B051: Centrum leteckého a kosmického výzkumu (CLKV)</a><br>

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění

2003

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

3rd International Conference on Advanced Engineering Design

ISBN

80-86059-35-9

ISSN

—

e-ISSN

—

Počet stran výsledku

10

Strana od-do

—

Název nakladatele

Neuveden

Místo vydání

Neuveden

Místo konání akce

Praha

Datum konání akce

1. 6. 2003

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

—