A method of manufacturing a toothed component for a gas turbine engine, the method comprising: forming a first tooth (238; 338a) in the component, the first tooth having a top land, a bottom land (246, 346a), a side wall (240, 340a, 440a, 540a, 640a) extending from the top land to the bottom land, a fillet radius transitioning between the side wall and the bottom land, wherein the bottom land has a minimum adjacent the fillet radius and a maximum away from the fillet radius; forming a second tooth (238, 338b) in the component adjacent the first tooth, the second tooth having a top land, a bottom land, a side wall (340b, 440b, 540b, 640b) extending from the top land to the bottom land and facing the first tooth, and a fillet radius transitioning between the side wall and the bottom land, the bottom land of the second tooth extending from a respective minimum adjacent the respective fillet radius toward the maximum of the bottom land of the first tooth, wherein the maximum of the bottom land of the first tooth and the maximum of the bottom land of the second tooth define a gable area (362; 462; 562; 662) of the component that peaks where the maximum of the bottom land of the first tooth and the maximum of the bottom of the second land join, wherein the gable area of the component has a primary stress driver concentration factor; and characterized by forming a stress relief feature (464; 466; 468; 572; 672), after formation of the first tooth and the second tooth, by removing material at the peak of the joined maximums in the gable area such that the stress relief feature reduces the primary stress driver concentration factor in the gable area during operation of the toothed component, as compared to the primary stress driver concentration factor in a gable area of a toothed component without such stress relief feature, wherein the removal of material removes the peak of the joined maximums and causes formation of two separate peaks in the form of a first inflection feature (574a, 674a) and a second inflection feature (574b, 674b), and wherein the stress relief feature forms the first inflection feature (574a, 674a) between the stress relief feature and the side wall of the first tooth and the second inflection feature (574b, 674b) between the stress relief feature and the side wall of the second tooth. forming a first tooth (238; 338a) in the component, the first tooth having a top land, a bottom land (246, 346a), a side wall (240, 340a, 440a, 540a, 640a) extending from the top land to the bottom land, a fillet radius transitioning between the side wall and the bottom land, wherein the bottom land has a minimum adjacent the fillet radius and a maximum away from the fillet radius; forming a second tooth (238, 338b) in the component adjacent the first tooth, the second tooth having a top land, a bottom land, a side wall (340b, 440b, 540b, 640b) extending from the top land to the bottom land and facing the first tooth, and a fillet radius transitioning between the side wall and the bottom land, the bottom land of the second tooth extending from a respective minimum adjacent the respective fillet radius toward the maximum of the bottom land of the first tooth, wherein the maximum of the bottom land of the first tooth and the maximum of the bottom land of the second tooth define a gable area (362; 462; 562; 662) of the component that peaks where the maximum of the bottom land of the first tooth and the maximum of the bottom of the second land join, wherein the gable area of the component has a primary stress driver concentration factor; and characterized by forming a stress relief feature (464; 466; 468; 572; 672), after formation of the first tooth and the second tooth, by removing material at the peak of the joined maximums in the gable area such that the stress relief feature reduces the primary stress driver concentration factor in the gable area during operation of the toothed component, as compared to the primary stress driver concentration factor in a gable area of a toothed component without such stress relief feature, wherein the removal of material removes the peak of the joined maximums and causes formation of two separate peaks in the form of a first inflection feature (574a, 674a) and a second inflection feature (574b, 674b), and wherein the stress relief feature forms the first inflection feature (574a, 674a) between the stress relief feature and the side wall of the first tooth and the second inflection feature (574b, 674b) between the stress relief feature and the side wall of the second tooth.