Fan outlet guide vane shroud insert repair

摘要

A method of repairing a turbine engine component that contains a series of lined apertures (50). The component is removed from the engine (10), and then at least one of the aperture liners (38) is also removed. The area adjacent the aperture (50) is machined to remove a portion of the parent material of the component. An insert (72) which replaces the material removed by machining is secured adjacent the aperture (50). The liner (38,82) about the aperture (50) is then replaced.