Fairing for folding wing tip

An aircraft wing comprising a main fixed wing portion and a wing tip device at a tip thereof, wherein the wing tip device is configurable between a flight configuration and a ground configuration, 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,

• the aircraft wing further comprising:
• a hinge arrangement connecting the main fixed wing portion and the wing tip device and for enabling the wing tip device to rotate between the ground configuration and the flight configuration, wherein the hinge arrangement protrudes beyond an outer surface of the main fixed wing portion and wing tip device;
• a fairing covering at least part of the hinge arrangement on at least a suction side of the wing, wherein the hinge arrangement has a hinge line, and wherein the fairing is shaped to be asymmetric in planform view with respect to the hinge line;
• and,
• wherein the fairing asymmetry comprises a larger volume enclosed by a fairing outer surface on the wing tip device side of the fairing than on the main fixed wing portion side of the fairing.