A method of assembling and installing an underwing package to an underside of an aircraft wing is disclosed. In various embodiments, the method includes assembling the underwing package, comprising at least a pylon and an engine, using a build frame; attaching a transfer cart to the underwing package; lowering the underwing package and the transfer cart from the build frame; transporting the underwing package and the transfer cart to the underside of the aircraft wing; and transferring the underwing package from the transfer cart to the underside of the aircraft wing.


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    Titel :

    TOTAL UNDERWING NACELLE AND ENGINE INSTALLATION


    Beteiligte:
    GORMLEY TIMOTHY (Autor:in) / RAMLAOUI JIHAD (Autor:in) / VIGNOBOUL VINCENT (Autor:in) / REPP TIMOTHY (Autor:in) / MINER JASEN (Autor:in) / LOPEZ LUIS A (Autor:in) / RANDOLPH DUFFY ADAM (Autor:in) / LINDE ERIK N (Autor:in)

    Erscheinungsdatum :

    19.11.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT