A fan assembly of a gas turbine engine, comprising: a fan rotor including: a fan rotor hub; and a plurality of fan blades extending radially outwardly from the fan rotor hub; a fan case including: an inner case portion; an outer case portion surrounding the plurality of fan blades; and a plurality of struts extending between the inner case portion and the outer case portion; and a bearing assembly configured to support the fan rotor at the inner case portion, the bearing assembly including: a bearing inner race secured to the fan rotor; a bearing outer race secured to the inner case portion; and a plurality of bearing elements located radially between the bearing inner race and the bearing outer race; and an oil return feature located at a first strut of the plurality of struts, configured to collect used lubricant and direct the used lubricant away from the bearing assembly; wherein the oil return feature includes a plurality of oil return ports (100a, 100b) located at an inner surface of the inner case portion of the fan case; wherein a first oil return port of the plurality of oil return ports is located axially forward of the plurality of bearing elements, and at least a second oil return port of the plurality of oil return ports is located axially aft of the plurality of bearing elements; and the first oil return port has a smaller cross-sectional area than the second oil return port. a fan rotor hub; and a plurality of fan blades extending radially outwardly from the fan rotor hub; a fan case including: an inner case portion; an outer case portion surrounding the plurality of fan blades; and a plurality of struts extending between the inner case portion and the outer case portion; and a bearing assembly configured to support the fan rotor at the inner case portion, the bearing assembly including: a bearing inner race secured to the fan rotor; a bearing outer race secured to the inner case portion; and a plurality of bearing elements located radially between the bearing inner race and the bearing outer race; and an oil return feature located at a first strut of the plurality of struts, configured to collect used lubricant and direct the used lubricant away from the bearing assembly; wherein the oil return feature includes a plurality of oil return ports (100a, 100b) located at an inner surface of the inner case portion of the fan case; wherein a first oil return port of the plurality of oil return ports is located axially forward of the plurality of bearing elements, and at least a second oil return port of the plurality of oil return ports is located axially aft of the plurality of bearing elements; and the first oil return port has a smaller cross-sectional area than the second oil return port. an inner case portion; an outer case portion surrounding the plurality of fan blades; and a plurality of struts extending between the inner case portion and the outer case portion; and a bearing assembly configured to support the fan rotor at the inner case portion, the bearing assembly including: a bearing inner race secured to the fan rotor; a bearing outer race secured to the inner case portion; and a plurality of bearing elements located radially between the bearing inner race and the bearing outer race; and an oil return feature located at a first strut of the plurality of struts, configured to collect used lubricant and direct the used lubricant away from the bearing assembly; wherein the oil return feature includes a plurality of oil return ports (100a, 100b) located at an inner surface of the inner case portion of the fan case; wherein a first oil return port of the plurality of oil return ports is located axially forward of the plurality of bearing elements, and at least a second oil return port of the plurality of oil return ports is located axially aft of the plurality of bearing elements; and the first oil return port has a smaller cross-sectional area than the second oil return port. a bearing inner race secured to the fan rotor; a bearing outer race secured to the inner case portion; and a plurality of bearing elements located radially between the bearing inner race and the bearing outer race; and an oil return feature located at a first strut of the plurality of struts, configured to collect used lubricant and direct the used lubricant away from the bearing assembly; wherein the oil return feature includes a plurality of oil return ports (100a, 100b) located at an inner surface of the inner case portion of the fan case; wherein a first oil return port of the plurality of oil return ports is located axially forward of the plurality of bearing elements, and at least a second oil return port of the plurality of oil return ports is located axially aft of the plurality of bearing elements; and the first oil return port has a smaller cross-sectional area than the second oil return port.