Design, development and testing thrust reversers for a business jet airplane are described from program conception through Federal Aviation Administration (FAA) Certification. Mechanical design, reverser operation, failsafe features, actuation systems and aircraft integration are covered. Model tests, developmental taxi tests, static ground tests and flight tests required for configuration development and FAA type certification are discussed.


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    Title :

    Design, Development and Flight Test of the Cessna Citation Thrust Reverser


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    National Business Aircraft Meeting and Engineering Display ; 1976



    Publication date :

    1976-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





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