This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures. ARP4402A results from a Five-Year Review and update of this specification.


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    Title :

    Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure


    Publication date :

    2020-09-22



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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