The aviation community has for many years searched for a solution to the inadvertent stall and spin of small single-engine airplanes. NASA, GAMA, and the FAA have coordinated an effort to develop technology that would markedly improve an airplane's resistance to entering a spin. Two manufacturers are proposing designs for FAA certification that incorporate spin-resistant features. The FAA has proposed certification requirements in special conditions to allow type certification of these new designs. This paper will discuss the historical perspective of FAA spin-resistant airplane efforts and procedures to be used by the FAA to test and determine compliance of the proposed designs to the standards set forth in the special conditions.


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    Titel :

    Spin resistant airplane certification issues


    Weitere Titelangaben:

    Bedingungen fuer die Zulassung von gegen Trudeln widerstandsfaehigen Flugzeugen


    Beteiligte:
    Arnold, C.E. (Autor:in)

    Erschienen in:

    SAE-Papers ; Oct ; 1-9


    Erscheinungsdatum :

    1987


    Format / Umfang :

    9 Seiten, 1 Tabelle, 14 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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