The objective of the technical assessment was to evaluate the structural integrity of the wing in view of the wing static test failure and the McDonnell Douglas Aircraft Company's (MDA's) repair plans. We evaluated the root cause analyses of the wing static test failure and the validation of the retrofit design.


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    Title :

    C-17 Wing Structural Integrity


    Contributors:

    Publication date :

    1993


    Size :

    29 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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