This SAE Aerospace Recommended Practice establishes the requirements and procedures for eddy current inspection of open fastener holes in aluminum aircraft structures. ARP4402 has been reaffirmed to comply with the SAE five-year review policy.


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    Title :

    Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure


    Publication date :

    2013-06-11



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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