• DocumentCode
    1855475
  • Title

    Implementation of an integrated safety-program: the MD-90 antiskid system

  • Author

    Redgate, Marianne L. ; Mckelvey, Michael H. ; Jolly, Carolyn L.

  • Author_Institution
    Douglas Aircraft Co., Long Beach, CA, USA
  • fYear
    1994
  • fDate
    24-27Jan 1994
  • Firstpage
    52
  • Lastpage
    58
  • Abstract
    At Douglas Aircraft Company (DAC), an integrated safety program is comprised of four major analyses, each of which is intended to provide design requirements and results that satisfy DAC, Federal Aviation Administration (FAA) and Joint Aviation Administration (JAA) requirements to maximize safety for the airplane, the flying public, and the public-at-large. These four analyses are: functional hazard analysis; system failure mode and effects analysis; fault tree analysis; zonal analysis. Every new or major-modified system designed for DAC´s latest airplane, the MD-90, incorporates an integrated safety program. One such system, the antiskid system, has repeatedly used the integrated safety program as a primary design tool and is a particularly satisfying example of what DAC calls “design for safety.”
  • Keywords
    aerospace testing; aircraft; failure analysis; reliability; reliability theory; safety systems; Douglas Aircraft Company; FAA; Federal Aviation Administration; JAA; Joint Aviation Administration; MD-90 antiskid system; antiskid system; design for safety; fault tree analysis; functional hazard analysis; integrated safety-program; system failure effects analysis; system failure mode; zonal analysis; Air safety; Aircraft; Airplanes; Design engineering; FAA; Failure analysis; Fault trees; Hazards; History; Reliability engineering;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Reliability and Maintainability Symposium, 1994. Proceedings., Annual
  • Conference_Location
    Anaheim, CA
  • Print_ISBN
    0-7803-1786-6
  • Type

    conf

  • DOI
    10.1109/RAMS.1994.291081
  • Filename
    291081