Engineering

Alessandro Landi, M. Nicholson

2011.10.18SAE International Journal of Aerospace

DOI: 10.4271/2011-01-2564

要旨

<div class="section abstract"><div class="htmlview paragraph">ARP4754A/ED-79A guidelines addresse the development cycle for aircraft and systems that implement aircraft functions. The current trend in system design is an increasing level of integration between aircraft functions and the systems that implement them. While there can be considerable value gained when integrating systems with other systems, the increased complexity yields increased possibilities for errors, particularly with functions that are performed jointly across multiple systems. Following the Aviation Rulemaking Advisory Committee (ARAC) recommendations to respond to this increased integration which referenced ARP4754/ED-79 in advisory materials for compliance to 14CFR/CS 25.1309 (see AMC 25.1309, published in 2002 and AC25.1309-Arsenal draft) the use of ARP4754A/ED79A in aircraft certification has become increasingly widespread.</div><div class="htmlview paragraph">This presentation constitutes a comparison between the documents SAE [<span class="xref">1</span>] / EUROCAE [<span class="xref">2</span>] and SAE [<span class="xref">3</span>] / EUROCAE [<span class="xref">4</span>]; it highlights ARP4754A/ED79A enhancements, novelties and key topics (e.g. Development Assurance Level Assignment FDAL &amp; IDAL).</div></div>

引用形式

LANDI, Alessandro; NICHOLSON, M. ARP4754A/ ED-79A - guidelines for development of civil aircraft and systems - enhancements, novelties and key topics. SAE International Journal of Aerospace, 2011, 4: 871–879.