The crash injury evaluation of the U. S. Army AC-1 DH 'Caribou' disclosed several desirable crash safety features including a limit landing gear strength which permits a vertical rate of descent of 14 feet per second; the location of the fuel cells outboard of the engine nacelles; troop seat belt anchorages which are directly secured to basic aircraft structure. Attention is invited to the remedial action suggested in the recommendations pertaining to these deficiencies. (Author)


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    Titel :

    U. S. Army AC-1 de Havilland 'Caribou' Evaluation, Ft. Rucker, Alabama, 21 January 1960


    Beteiligte:
    G. M. Bruggink (Autor:in) / J. Carroll (Autor:in) / W. R. Knowles (Autor:in)

    Erscheinungsdatum :

    1960


    Format / Umfang :

    65 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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