Abstract: A system including an extraction force transfer coupling link assembly is provided that extracts a cargo from an airborne aircraft with an extraction parachute and then deploys the cargo with a descent parachute. During a normal extraction the link assembly transfers a force from an extraction line to a deployment lanyard that deploys a descent parachute. In the event of a failed extraction, the assembly severs the deployment lanyard and jettisons the extraction parachute. The extraction force transfer coupling link assembly includes an ultra high molecular weight polyethylene rope that has one end of the deployment lanyard braided with the extraction line. The rope acts as both the extraction line for the cargo and the deployment lanyard for the descent parachute. By virtue of the ability to use a single rope, the link assembly is of simple construction and employs pyrotechnic cutters to effect the release of the extraction line and deployment lanyard rather than conventional mechanical interlocks.