The second phase of the CH-47C airworthiness and flight characteristics (A and FC) test program consisted of the stability and control test of the production helicopter. The CH-47C was evaluated to determine compliance with the military specification, MIL-H-8501A, with deviations as defined in the detail specification. The helicopter was also evaluated with respect to its mission as a transport helicopter. The CH-47C stability and control characteristics are acceptable for the transport helicopter mission.


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    Title :

    Airworthiness and Flight Characteristics Test CH-47C Helicopter (Chinook) Stability and Control


    Contributors:
    J. I. Nagata (author) / G. L. Skinner (author) / P. J. Bohn (author) / A. R. Todd (author) / D. G. Broadhurst (author)

    Publication date :

    1972


    Size :

    89 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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