An aircraft wing (308) including a fuel tank (314) located in the wing (308), a channel (336) defining a cavity (313) in the fuel tank (314), the channel (336) including at least two channel ends terminating at an upper or lower wing surface (340, 342), a driveshaft (316) located in the cavity (313); and an access panel (390) located on the wing surface (340, 342) and being movable between an open position so that access to the cavity (313) is permitted, and a closed position so that the cavity (313) is at least partially covered by the access panel (390) to inhibit access to the cavity (313).


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    Title :

    CROSS-WING DRIVESHAFT CHANNEL


    Additional title:

    ANTRIEBSKANAL IN FLÜGELLÄNGSRICHTUNG
    CANAL TRANSVERSAL AILAIRE POUR ARBRE DE TRANSMISSION


    Contributors:

    Publication date :

    2018-11-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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