The present application relates to an aircraft assembly. The aircraft assembly has a wing tip device connected to a wing tip of a wing by a first connector, a second connector and a third connector. The wing tip device includes a front device spar and a rear device spar. The first connector is associated with the rear device spar. The second connector is spaced apart in a chordwise direction forward of the first connector, and the third connector is spaced apart in a chordwise direction rearward of the first connector. The third connector comprises a spigot mounting formation.


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    Title :

    An aircraft assembly including a wingtip device


    Publication date :

    2017-12-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English



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