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
Link To Document :
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