This content is not included in your SAE MOBILUS subscription, or you are not logged in.
ARP4754A/ ED-79A - Guidelines for Development of Civil Aircraft and Systems - Enhancements, Novelties and Key Topics
ISSN: 1946-3855, e-ISSN: 1946-3901
Published October 18, 2011 by SAE International in United States
Citation: Landi, A. and Nicholson, M., "ARP4754A/ ED-79A - Guidelines for Development of Civil Aircraft and Systems - Enhancements, Novelties and Key Topics," SAE Int. J. Aerosp. 4(2):871-879, 2011, https://doi.org/10.4271/2011-01-2564.
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.
This presentation constitutes a comparison between the documents SAE  / EUROCAE  and SAE  / EUROCAE ; it highlights ARP4754A/ED79A enhancements, novelties and key topics (e.g. Development Assurance Level Assignment FDAL & IDAL).