The objective of the test is to verify, according to the FAA airworthiness regulations (FAR25.305), the static structural integrity of the elevator. In accordance with the certification regulations, the structural components must endure at least 150 percent (ultimate load) of a defined limit load without rupture. In addition to verify the performance of the intact structure, power control units disconnect situations, where important connecting elements have failed, must also be evaluated. Furthermore,Borescope inspection was performed for dimensional checks of pins,bushings, and lugs to confirm that no secondary damage occurs on elevator.