A method and apparatus for operating an aircraft. The aircraft is flown. A skin panel is held on a support structure. The support structure has flanges on a number of edges of the support structure, the flanges being substantially orthogonal to the edges. The support structure also has openings into the support structure substantially orthogonal to the flanges. First connecting structures on clips are connected to the flanges and positioned such that an opening in each clip is aligned with one of the openings in the support structure. The skin panel is positioned such that the clips are received in holes in the skin panel. Fasteners are attached to the second connecting structures such that the support structure holds the skin panel.


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    Titel :

    Aircraft skin attachment system


    Beteiligte:

    Erscheinungsdatum :

    13.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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