The airplane has a relatively steep spin mode (low angle of attack) with a high load factor and high velocity. The airplane recovers almost immediately after any deviation from the prospin control positions, except for one maneuver with reduced flexibility in the elevator control system.


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    Titel :

    Spin tests of a single-engine, high-wing light airplane


    Beteiligte:
    Stewart, E. C. (Autor:in) / Suit, W. T. (Autor:in) / Moul, T. M. (Autor:in) / Brown, P. W. (Autor:in)

    Erscheinungsdatum :

    1982-01-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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