Arrangement for avoiding clashing between an actuation assembly and an upper cover of a folding wing tip

An aircraft wing, the aircraft wing comprising a fixed wing and a wing tip device rotatable about a hinge axis of a hinge at the tip of the fixed wing between:

• (i) a flight configuration for use during flight and (ii) a ground configuration for use during ground-based operations, in which ground configuration the wing tip device is moved away from the flight configuration such that the span of the aircraft wing is reduced,
• wherein the wing further comprises an actuation assembly for rotating the wing tip device about the hinge, and wherein in the flight configuration the actuation assembly is in a first configuration occupying a first space, and in the ground configuration the actuation assembly is in a second configuration occupying a second space;
• wherein the upper cover of the wing tip device comprises an offset region extending inboard of the hinge axis,
• the offset region and the actuation assembly being arranged such that when the wing tip device is rotated to the ground configuration, the offset region extends into the first space, but is outside the second space.