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

    Erscheinungsdatum :

    1982


    Format / Umfang :

    93 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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

    Stewart, E. C. / Suit, W. T. / Moul, T. M. et al. | NTRS | 1982


    Crash Tests of Three Identical Low-Wing Single-Engine Airplane

    C. B. Castle / E. Alfaro-bou | NTIS | 1983


    Crash tests of three identical low-wing single-engine airplane

    Castle, C. B. / Alfaro-Bou, E. | NTRS | 1983



    Investigations of Modifications to Improve the Spin Resistance of a High-Wing, Single-Engine, Light Airplane

    DiCarlo, D. J. / Manuel, G. S. / Stough, H. P. et al. | SAE Technical Papers | 1989