DocumentCode
1738577
Title
Functional failure path analysis of airborne electronic hardware
Author
Beland, Steven C. ; BonJour, B.
Author_Institution
Boeing Co., Seattle, WA, USA
Volume
1
fYear
2000
fDate
2000
Abstract
RTCA DO-254, “Design Assurance Guidance for Airborne Electronic Hardware,” outlines an approach for providing design assurance confidence for functions of a range of design assurance levels. In order to decompose the hardware functions, DO-254 provides a brief overview of Functional Failure Path Analysis (FFPA) but is limited in detail and provides no examples. This paper presents a detailed explanation of FFPA and illustrates it with a representative example
Keywords
avionics; certification; design engineering; failure analysis; reliability; RTCA DO-254; airborne electronic hardware; aircraft system certification; design assurance confidence; design assurance levels; functional failure path analysis; verification activities planning; Airplanes; Assembly; Computer architecture; Failure analysis; Hardware; Hazards; Process planning; Refining; Software safety; Technology planning;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 2000. Proceedings. DASC. The 19th
Conference_Location
Philadelphia, PA
Print_ISBN
0-7803-6395-7
Type
conf
DOI
10.1109/DASC.2000.886874
Filename
886874
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