The present disclosure provides a tooling for handling a nacelle of an aircraft turbojet engine. The tooling includes a gantry having at least one upper support bar which is hinged about at least a first upper axis of rotation (A) by a first upper hinge. The upper support bar is hinged between at least a first support position in which the upper bar has a first attachment which is adapted to be fastened on a first type of nacelle, and at least a second support position in which the upper support bar has a second attachment which is adapted to be fastened on a second type of nacelle.


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    Title :

    TOOLING FOR HANDLING A NACELLE OF AN AIRCRAFT TURBOJET ENGINE


    Contributors:

    Publication date :

    2018-08-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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