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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    Titel :

    Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure


    Erscheinungsdatum :

    11.06.2013



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





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