Abstract: A method for manufacturing a part selected from a plurality of part types is disclosed. The method involves the step of selecting, from a supply of workpieces, a workpiece of a type that is associated with the type of part selected, the workpiece having a void and a substantially annular outer surface. Using a lathe, the selected workpiece is machined into the selected part. The workpiece, during the machining step, is mounted to the lathe by a collet associated with the type of part selected. The collet is an expanding collet which, during machining, is received by the void and engages the workpiece in gripping relation. The part can be a bushing for an aircraft landing gear and the workpiece can be an oversized bushing. The method can be carried out at an aircraft repair facility and the oversized bushings can be procured from specialist fabricators.

Abstract: This invention relates to an improved method of manufacturing injection molding manifolds for multicavity molding. The method includes gun drilling a longitudinal duct through a steel manifold body, drilling a transverse inlet duct to connect to an inlet on one surface of the manifold, and drilling diagonal outlet ducts to connect to spaced outlets on the opposite surface of the manifold. The outlet ducts are smaller in diameter than the longitudinal duct to match the rest of the system. Before the outlet ducts are drilled, end portions of the longitudinal duct are drilled out to a larger diameter and steel plugs having a tapered well are securely welded into them with the mouth of the well in alignment with the longitudinal duct. The plugs are larger in diameter than the central portion of the longitudinal duct to avoid the formation of thin knife edge portions where the outlet ducts join the longitudinal duct which often break down during use.