DocumentCode :
1908447
Title :
Shortcomings in MIL-STD-1629A guidelines for criticality analysis
Author :
Agarwala, Ajay S.
Author_Institution :
Boeing Helicopters, Philadelphia, PA, USA
fYear :
1990
fDate :
23-25 Jan 1990
Firstpage :
494
Lastpage :
496
Abstract :
Some shortcomings in the industry guidelines MIL-STD-1629A in performing failure mode, effects, and criticality analyses are highlighted. It can be shown that if the MIL-STD-1629A guidelines are followed, then the contribution of several terms to the item-criticality numbers (the final step in completing a criticality analysis) is erroneously omitted. As a result, the item-criticality numbers for the lower severities of the item are incorrect. As a separate issue, a broader definition of β is recommended to properly treat failures in redundant systems
Keywords :
failure analysis; MIL-STD-1629A guidelines; criticality analysis; failure mode analysis; item-criticality numbers; Chromium; Failure analysis; Guidelines; Hazards; Helicopters; Logistics; Maintenance; Mission critical systems; Performance analysis; Safety;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Reliability and Maintainability Symposium, 1990. Proceedings., Annual
Conference_Location :
Los Angeles, CA
Type :
conf
DOI :
10.1109/ARMS.1990.68007
Filename :
68007
Link To Document :
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