The invention discloses a combined lifting tool for an aircraft. The combined lifting tool for the aircraft comprises a lifting beam assembly, a front connection assembly, a back connection assembly, a back lifting shaft assembly and a sling assembly. The lifting beam assembly is provided with two first lifting beams and two second lifting beams, wherein the two first lifting beams are used for horizontal lifting, and the two second lifting beams are used for vertical lifting. The front connection assembly comprises an arch-shaped fixing frame and a lower support plate. The two ends of the lower support plate are connected with the fixing frame through bolts. The two sides of the fixing frame are provided with first connection shafts correspondingly. Auxiliary supporting devices are arranged on the two sides of the fixing frame and located on the upper sides of the first connection shafts. The back connection assembly comprises an adapter plate. The two sides of the adapter plate are provided with second connection shafts. The adapter plate is provided with multiple bolt passing holes used for connection with an aircraft. The back lifting shaft assembly comprises two back lifting shafts. The sling assembly comprises a triangular lifting rack and slings. The combined lifting tool for the aircraft has the advantages of being stable and firm in connection, good in barycenter adaptability and wide in use range and achieving safe and reliable lifting. The combined lifting tool for the aircraft can meet the two working conditions of horizontal lifting and vertical lifting.