Procedure which uses statistical methods of data analysis which provide sole means for mathematical determination of reliability from safety aspect; suggestion is made that aircraft safety should require catastrophic failure rate of less than 10-3 after 10,000 flying hours; it is shown how requirement of this type may be met, but methods are sufficiently flexible for adaptation to any requirement considered necessary in future.


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    Title :

    Assessing helicopter safety with respect to component fatigue


    Additional title:

    Aircraft Eng


    Contributors:
    Hall, A.D. (author)

    Published in:

    Publication date :

    1963


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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