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.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Eddy Current Inspection of Open Fastener Holes in Aluminum Aircraft Structure


    Erscheinungsdatum :

    22.09.2020



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    Eddy Current Detection of Pitting Corrosion Around Fastener Holes

    Heida, J. H. / Advisory Group for Aerospace Research and Development; Structures and Materials Panel | British Library Conference Proceedings | 1995



    Automatic X-ray crack inspection for aircraft wing fastener holes

    Xu, J. / Liu, T. / Yin, X.M. et al. | Tema Archiv | 2010