Abstract: The present invention is a portable engine powered horizontal action aircraft landing barrier arresting cable disc loading apparatus which includes an engine powered hydraulic pump; manual hydraulic pump; an elongated frame; a transverse axle having a reservoir for hydraulic fluid; a hydraulic cylinder and ram/piston secured to one end of the frame and a system of staves comprised partially of the elongated frame and slotted plates affixed at regular intervals along the longitudinal length opposite the hydraulic cylinder. The ram/piston is configured with a chain attachment hook which is movable toward and away from the staves and provides a longitudinal pulling force with respect to the staves. Multiple staves are provided to divide the pulling force between groups of the total number of discs to be loaded. The present invention has internal power redundancy and has a means of accessing external power for secondary redundancy.