Cold working — or cold hole expansion — consists of pulling through a fastener hole a mandrel of slightly larger diameter, creating a controlled radial plastic deformation (typically 3% to 6% of the nominal diameter). This deformation introduces a high-intensity, deep residual compressive stress field around the hole (several millimetres radially).
Hole edges are the classic fatigue-crack initiation site on aerospace structures. By installing a compressive field there, cold working significantly delays crack initiation and propagation: fatigue life is multiplied by 3 to 10 depending on the alloy and loading mode. The process is specified by Boeing (BACC 5060) and adopted across the civil aerospace industry.
Two techniques coexist: split sleeve (Fatigue Technology — disposable split sleeve between mandrel and hole, preserves surface finish) and split mandrel (West Coast Industries — split mandrel expanding inside the hole, faster in production).