An aircraft engine mounting system to retrofit an aircraft engine from one aircraft type to another in a manner suitable for approved flight. The system includes a circular member having longitudinal securement members extending therefrom to attach the circular member to an inner surface of the fuselage of an aircraft. The circular member in turn has mounting members configured to receive an aircraft engine to retrofit the engine from a first aircraft to a second aircraft.


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    Title :

    Aircraft Engine Adapter System


    Author / Creator :

    Type of media :

    Patent


    Type of material :

    Electronic Resource



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