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
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