The present invention relates to a method for processing a TC11 material vane. The method can conveniently machine out a TC11 material aviation vane which has large torsional angle, large string width, large rough blank profile margin and uneven margins at all positions and is easy to machine. The method comprises the steps as follows: retesting a central forging hole, processing the back of a middle body, a technical reference of the air outlet side and a vane top axial reference face, rough machining a vane root and a vane root bottom surface technical button, processing for reverse adjustment, finish milling the profile, polishing the profile, processing the total length, removing a vane top central hole and removing the vane root bottom surface button. The present invention is characterized in that the vane top central hole during swaging processing is always kept until the total length is cut; a forging vane top central hole is considered as the reference; after the distressing treatment, the reverse adjustment is conducted, and the vane root and the surface of the vane root bottom surface technical button is fine finished; a vane root positioning area is increased, so the technical button is reserved at the vane root bottom surface, a vane root molding knife is used for processing the vane root and the surface of the vane root bottom surface technical button to ensure that the surface of the vane root bottom surface technical button is consistent with the vane root; and when milling comprehensively, the vane root and the surface of the vane root bottom surface technical button are used for positioning, and the vane profile is rough milled and fine milled.