The invention belongs to the technical field of laser machining and relates to an ultrasonic-impact-assisted laser cladding repairing method for an ultra-high-strength steel member. The ultrasonic-impact-assisted laser cladding repairing method is mainly used for repairing damage such as surface corrosion and micro cracks of the ultra-high-strength steel member of an airplane. In the earlier stage, same metal powder for repairing is adopted for conducting a direct laser cladding repairing test and an ultrasonic-impact-assisted laser cladding repairing test on a 30CrMnSiNi2A ultra-high-strengthsteel undercarriage half-shaft base body, wherein according to the metal powder, the cladding metal impact toughness is larger than or equal to 420 KJ/m<2>, the room-temperature ductility is larger than or equal to 10.8%, and the room-temperature tensile strength is larger than or equal to 1400 MPa; and the room-temperature tensile performance, the room-temperature impact performance and the microhardness performance of two repairing areas are tested. The results are obtained as follows: according to direct laser cladding repairing, the average tensile strength is 1428.6 MPa, the average elongation rate is 11.8%, the average impact toughness is 471 KJ/m<2>, and the average microhardness of repairing metal is 474.3 HV; and according to ultrasonic-impact-assisted laser cladding repairing, the average tensile strength is 1436.2 MPa, the average elongation rate is 14.8%, the average impact toughness is 643 KJ/m<2>, and the average microhardness of the repairing metal is 490.7 HV.