A turbocharger assembly comprising: a shaft including a turbine wheel that includes a hub portion; a rolling element bearing rotatably supporting the shaft, wherein the rolling element bearing comprises an inner race; a housing that comprises a bearing bore that receives the rolling element bearing; and a turbine side bore that extends from an interior of the housing to an exterior of the housing and wherein the turbine side bore comprises an interior side overhang, wherein an edge forms the overhang as a lip portion, wherein the overhang is defined by an axial length and an arc angle about a central axis of the turbine side bore, and wherein the edge defines in part a first surface that forms an undercut and a second surface that overhangs the first surface to form the overhang, wherein the second surface comprises an annular width defined between an outer edge and an inner edge; and a sub-assembly disposed axially between the inner race and the hub portion, wherein the sub-assembly comprises: a lubricant slinger comprising a diameter which exceeds a diameter of the turbine side bore, a front face and a back face, wherein the inner race extends axially to contact the front face of the slinger; and a bushing configured to be received within the turbine side bore, the bushing comprising a front face, a back face, and a slinger feature that extends axially past the first surface. a shaft including a turbine wheel that includes a hub portion; a rolling element bearing rotatably supporting the shaft, wherein the rolling element bearing comprises an inner race; a housing that comprises a bearing bore that receives the rolling element bearing; and a turbine side bore that extends from an interior of the housing to an exterior of the housing and wherein the turbine side bore comprises an interior side overhang, wherein an edge forms the overhang as a lip portion, wherein the overhang is defined by an axial length and an arc angle about a central axis of the turbine side bore, and wherein the edge defines in part a first surface that forms an undercut and a second surface that overhangs the first surface to form the overhang, wherein the second surface comprises an annular width defined between an outer edge and an inner edge; and a sub-assembly disposed axially between the inner race and the hub portion, wherein the sub-assembly comprises: a lubricant slinger comprising a diameter which exceeds a diameter of the turbine side bore, a front face and a back face, wherein the inner race extends axially to contact the front face of the slinger; and a bushing configured to be received within the turbine side bore, the bushing comprising a front face, a back face, and a slinger feature that extends axially past the first surface. a bearing bore that receives the rolling element bearing; and a turbine side bore that extends from an interior of the housing to an exterior of the housing and wherein the turbine side bore comprises an interior side overhang, wherein an edge forms the overhang as a lip portion, wherein the overhang is defined by an axial length and an arc angle about a central axis of the turbine side bore, and wherein the edge defines in part a first surface that forms an undercut and a second surface that overhangs the first surface to form the overhang, wherein the second surface comprises an annular width defined between an outer edge and an inner edge; and a sub-assembly disposed axially between the inner race and the hub portion, wherein the sub-assembly comprises: a lubricant slinger comprising a diameter which exceeds a diameter of the turbine side bore, a front face and a back face, wherein the inner race extends axially to contact the front face of the slinger; and a bushing configured to be received within the turbine side bore, the bushing comprising a front face, a back face, and a slinger feature that extends axially past the first surface. a lubricant slinger comprising a diameter which exceeds a diameter of the turbine side bore, a front face and a back face, wherein the inner race extends axially to contact the front face of the slinger; and a bushing configured to be received within the turbine side bore, the bushing comprising a front face, a back face, and a slinger feature that extends axially past the first surface.