• 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