The invention discloses a chute machining method for the inner wall face of a case of an aero-engine. The method comprises the following steps that a, a five-axis numerical control machine tool is selected as machining equipment; b, the tool assembly manner is improved, a through-connection angle head is used for carrying out through connection on a tool on a machine tool spindle, and the machine tool spindle stretching into the case in the axial direction of the case and the tool for machining the inner wall face of the case in the radial direction of the case are formed; c, the tool is selected, the diameter of a handle of the tool ranges from phi6 to phi10, the diameter of a cutting part ranges from phi4 to phi7, the length-diameter ratio of the tool ranges from 1:7 to 1:10, and therefore tool vibration brought by through connection of the tool in the machining process is reduced; d, a chute machining process path is selected, and a circulation machining manner is adopted so as to guarantee the surface roughness of chutes and improve the machining efficiency; and e, all chute design positions on the inner wall face of the case are machined, and the formed case is obtained. The requirements for the sizes and the roughness of the chutes are guaranteed; and tool consumption is greatly reduced, and the machining cost is reduced.