Aircraft joint with a curable composite bushing

An aircraft joint comprising:

• a first structural component provided with an attachment hole configured to receive a corresponding attachment fastener provided by a second structural component;
• a curable composite bush compressed and cured between an outer diameter of the attachment fastener and the attachment hole when the first structural component is mounted to the second structural component,
• wherein the curable composite bush prevents radial displacement of the attachment fastener within the attachment hole,
• wherein the curable composite bush comprises a hollow cylindrical body formed from a matrix material pre-impregnated with reinforcement fibers, and
• wherein the reinforcement fibers of the curable composite bush are oriented in a circumferential direction about a longitudinal axis of the bush, wherein the hollow cylindrical body defines a plurality of corrugations extending between an inner and an outer diameter of the bush, and wherein the corrugations improve a compressibility of the bush in a direction collinear to a longitudinal axis of the bush.