Patent ID: 8328142

Claim:
An aircraft wing comprising: a trailing edge cove extending in a span-wise direction along a trailing edge of the wing, the trailing edge cove having a front face, a top face and a bottom face; an actuator bracket which is mounted to the front and top faces of the trailing edge cove but not to its bottom face; an aileron actuator coupled at one end to an aileron and at the other end to the actuator bracket, the aileron actuator being adjustable from a retracted position to a deployed position to deploy the aileron; and a channel extending in a span-wise direction along the wing and positioned below the actuator bracket; wherein the actuator bracket comprises a front web which is mounted to the front face of the trailing edge cove; a top web which is mounted to the top face of the trailing edge cove; and a lug which extends from said front web and said top web.