A gas turbine engine comprising: an engine static structure; a rotating structure configured to rotate relative to the engine static structure, the rotating structure provides a first annular array of first radial scoops, and the rotating structure provides a second annular array of second radial scoops arranged axially with respect to the first annular array of first radial scoops; a first component arranged in an axially forward direction relative to the first annular array of first radial scoops, and a second component arranged in an axially aft direction relative to the second annular array of second radial scoops; and a lubrication system including at least one nozzle (68a, 68b) aimed at the first and second annular arrays of first and second radial scoops (78; 80), and a first lubrication delivery path fluidly connecting the first annular array of first radial scoops to the first component along the axially forward direction, and a second lubrication delivery path fluidly connecting the second annular array of second radial scoops to the second component along the axially aft direction, wherein the rotating structure includes a ring mounted to a shaft, the first annular array of first radial scoops and the second annular array of second radial scoops are provided on the ring; wherein a seal (100; 200) is provided radially between the ring and the shaft, the seal (100; 200) fluidly separating the first lubrication delivery path and the second lubrication delivery path, the seal (100; 200) positioned axially between the first annular array of first radial scoops and the second annular array of second radial scoops; wherein each of the first annular array of first radial scoops and the second annular array of second radial scoops includes an arcuate tapered surface leading to a window that is configured to fluidly communicate lubricant from an outer diameter of the ring to an inner diameter of the ring; and wherein the first annular array of first radial scoops are provided by first and second radially outwardly extending walls (82; 84), and the second annular array of second radial scoops are provided by the second radially outward extending wall and a third radially outwardly extending wall. an engine static structure; a rotating structure configured to rotate relative to the engine static structure, the rotating structure provides a first annular array of first radial scoops, and the rotating structure provides a second annular array of second radial scoops arranged axially with respect to the first annular array of first radial scoops; a first component arranged in an axially forward direction relative to the first annular array of first radial scoops, and a second component arranged in an axially aft direction relative to the second annular array of second radial scoops; and a lubrication system including at least one nozzle (68a, 68b) aimed at the first and second annular arrays of first and second radial scoops (78; 80), and a first lubrication delivery path fluidly connecting the first annular array of first radial scoops to the first component along the axially forward direction, and a second lubrication delivery path fluidly connecting the second annular array of second radial scoops to the second component along the axially aft direction, wherein the rotating structure includes a ring mounted to a shaft, the first annular array of first radial scoops and the second annular array of second radial scoops are provided on the ring; wherein a seal (100; 200) is provided radially between the ring and the shaft, the seal (100; 200) fluidly separating the first lubrication delivery path and the second lubrication delivery path, the seal (100; 200) positioned axially between the first annular array of first radial scoops and the second annular array of second radial scoops; wherein each of the first annular array of first radial scoops and the second annular array of second radial scoops includes an arcuate tapered surface leading to a window that is configured to fluidly communicate lubricant from an outer diameter of the ring to an inner diameter of the ring; and wherein the first annular array of first radial scoops are provided by first and second radially outwardly extending walls (82; 84), and the second annular array of second radial scoops are provided by the second radially outward extending wall and a third radially outwardly extending wall.