A turbine engine that extends along an axis, the turbine engine comprising: a compressor; a combustor in fluid communication with the compressor; a first turbine section in fluid communication with the combustor; a second turbine section in fluid communication with the first turbine section; a fan; a first shaft interconnecting the compressor and the first turbine section; a second shaft interconnecting the fan and the second turbine section, the second shaft being connected to the fan through a geared architecture and a portion of the second shaft extending through a center of the first shaft; a mid-turbine frame located axially between the first turbine section and the second turbine section, the mid-turbine frame having an outer frame case connected to an inner frame case via a plurality of cooled spokes, wherein each of the plurality of cooled spokes has a radially outer end, a radially inner end, and a hollow center for supplying cooling airflow from outside the outer frame case to the inner frame case, wherein the inner frame case includes a manifold defined by an outer diameter annular portion with a first cylindrical face oriented towards the axis, an inner diameter annular portion with a second cylindrical face oriented away from the axis, and first and second radial portions (82, 86) of the inner frame case that extend radially from the outer diameter annular portion to the inner diameter annular portion and each of the plurality of cooled spokes terminates radially between a radially outer surface of the outer diameter annular portion and a radially inner surface of the outer diameter annular portion to thereby allow the manifold to receive and combine airflow from the plurality of cooled spokes; a first bearing connected to the first shaft and supported by the mid-turbine frame; and a second bearing connected to the second shaft and supported by the mid-turbine frame, wherein the second bearing is positioned axially aft of and radially outward of the first bearing. a compressor; a combustor in fluid communication with the compressor; a first turbine section in fluid communication with the combustor; a second turbine section in fluid communication with the first turbine section; a fan; a first shaft interconnecting the compressor and the first turbine section; a second shaft interconnecting the fan and the second turbine section, the second shaft being connected to the fan through a geared architecture and a portion of the second shaft extending through a center of the first shaft; a mid-turbine frame located axially between the first turbine section and the second turbine section, the mid-turbine frame having an outer frame case connected to an inner frame case via a plurality of cooled spokes, wherein each of the plurality of cooled spokes has a radially outer end, a radially inner end, and a hollow center for supplying cooling airflow from outside the outer frame case to the inner frame case, wherein the inner frame case includes a manifold defined by an outer diameter annular portion with a first cylindrical face oriented towards the axis, an inner diameter annular portion with a second cylindrical face oriented away from the axis, and first and second radial portions (82, 86) of the inner frame case that extend radially from the outer diameter annular portion to the inner diameter annular portion and each of the plurality of cooled spokes terminates radially between a radially outer surface of the outer diameter annular portion and a radially inner surface of the outer diameter annular portion to thereby allow the manifold to receive and combine airflow from the plurality of cooled spokes; a first bearing connected to the first shaft and supported by the mid-turbine frame; and a second bearing connected to the second shaft and supported by the mid-turbine frame, wherein the second bearing is positioned axially aft of and radially outward of the first bearing.