This paper deals broadly with three aspects of the fatigue substantiation of general aviation aircraft structures. It describes the development of the Australian fatigue substantiation requirements for general aviation aircraft; it presents the results of local work in the acquisition of loads spectra for a range of aircraft, including pressurized and nonpressurized light twins, and it discusses some specific problems affecting the safe life and fail-safe substantiation of general aviation aircraft structures. Recent Australian work on ground taxi load spectra and on the endurance and radiographic inspectability of laminated spar caps is described.


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    Titel :

    Fatigue Certification of General Aviation Aircraft in Australia


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Torkington, C. (Autor:in) / O'Brien, K. (Autor:in) / Benoy, M. (Autor:in) / Douglas, R. (Autor:in)

    Kongress:

    National Business Aircraft Meeting and Engineering Display ; 1972



    Erscheinungsdatum :

    1972-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch