Abstract: An aircraft skin alignment system includes a support structure to support one or more aircraft skins, a puller tool, and a clamp tool; the puller tool having a base, the base supporting a holding mechanism to releasably engage with a first aircraft skin and a pulling mechanism to apply a pulling force to the first aircraft skin when the first aircraft skin is engaged with the holding mechanism; and the clamp tool having a body supporting an edge locator; the puller tool is to pull the first aircraft skin such that a first edge of the aircraft skin abuts the edge locator, the edge locator preventing the first edge from being pulled past the edge locator; and tool holes can be drilled into the first aircraft skin such that the tool holes are aligned based on an edge index due to a position of the edge locator.

Abstract: A barge lid lifter system having a frame, a plurality of vertical beams adjustably mounted to the frame, a plurality of cross bracing beams, and a plurality of load engagement mechanisms mounted to the vertical beams. Each load engagement mechanism may include a frame including a dagger plate, and a linear actuator configured to position an arm is configured an arm over a dagger point to retain a lifting assembly of a barge lid. The brackets of the vertical beams are configured to mount onto plates disposed on the frame such that the position of the load engagement mechanisms can be adjusted to fit barge lids of varying lengths and widths.

Abstract: A barge lid lifter system having a horizontal frame, a plurality of vertical beams, a plurality of cross bracing beams, and a plurality of load engagement mechanisms is provided. Each load engagement mechanism may include a frame, wherein each load engagement mechanism frame may have a first side plate, a second side plate, a top plate, a dagger plate, a horizontal pivot pin, and a horizontal pivot pin sleeve. The load engagement mechanism includes a linear actuator, a rotation plate, a rotation elbow, an arm, and a dagger point. The linear actuator is connected to the first side plate and the rotation elbow, and the rotation plate is connected to the rotation elbow and the arm. The arm is configured to close over the dagger point and retain a lifting eye of a barge lid lifting assembly.

Abstract: A barge lid lifter system having a horizontal frame, a plurality of vertical beams, a plurality of cross bracing beams, and a plurality of load engagement mechanisms is provided. Each load engagement mechanism may include a frame, wherein each load engagement mechanism frame may have a first side plate, a second side plate, a top plate, a dagger plate, a horizontal pivot pin, and a horizontal pivot pin sleeve. The load engagement mechanism includes a linear actuator, a rotation plate, a rotation elbow, an arm, and a dagger point. The linear actuator is connected to the first side plate and the rotation elbow, and the rotation plate is connected to the rotation elbow and the arm. The arm is configured to close over the dagger point and retain a lifting eye of a barge lid lifting assembly.