A turbine shroud assembly (20,322) for a gas turbine engine, the turbine shroud assembly comprising: a carrier (24, 224, 324) comprising metallic materials and arranged to extend circumferentially at least partway about a central axis; a blade track segment (26, 226, 326) comprising ceramic matrix composite materials, the blade track segment formed to include a runner shaped to extend circumferentially partway around the axis, a first mount post (70, 270, 370) that extends radially outward from the runner, and a second mount post (72, 272, 372) that extends radially outward from the runner, the second mount post spaced apart axially from the first mount post to define a channel (71,371) therebetween, the first mount post and the second mount post being shaped to include pin holes (67, 69), characterized in that the carrier (24, 224, 324) includes a carrier body (38, 338) extending at least partway about the central axis and forming an attachment-receiving space and a plurality of locating pads (40, 42, 240, 340, 342) that each extend radially inward from the carrier body into contact with a radially-outwardly facing surface (74, 274, 374) of at least one of the first mount post (70, 270, 370) and the second mount post (72, 272, 372) of the blade track segment (26, 226, 326) to radially locate the blade track segment relative to the carrier; and an intermediate carrier (28, 228, 328) configured to couple the blade track segment to the carrier, the intermediate carrier including an intermediate carrier body (30, 230, 330) arranged in the channel (71, 371) axially between the first mount post and the second mount post, the intermediate carrier body shaped to include pin holes (81, 83), at least one pin (32, 232, 332) that extends axially into the first mount post, the intermediate carrier body, and the second mount post to couple the intermediate carrier body to the blade track segment, and at least one retainer (36, 236, 336) that extends radially outward from the intermediate carrier body through the carrier to couple the intermediate carrier and the blade track segment with the carrier, wherein the at least one retainer includes a threaded coupling formed integrally with the intermediate carrier body (30, 230, 330) that extends radially outward from the intermediate carrier body and a threaded fastener (86, 286, 386) that extends radially inward through the carrier (24, 224, 324) into the coupling to couple the intermediate carrier (28, 228, 328) with the carrier (24, 224, 324). a carrier (24, 224, 324) comprising metallic materials and arranged to extend circumferentially at least partway about a central axis; a blade track segment (26, 226, 326) comprising ceramic matrix composite materials, the blade track segment formed to include a runner shaped to extend circumferentially partway around the axis, a first mount post (70, 270, 370) that extends radially outward from the runner, and a second mount post (72, 272, 372) that extends radially outward from the runner, the second mount post spaced apart axially from the first mount post to define a channel (71,371) therebetween, the first mount post and the second mount post being shaped to include pin holes (67, 69), characterized in that the carrier (24, 224, 324) includes a carrier body (38, 338) extending at least partway about the central axis and forming an attachment-receiving space and a plurality of locating pads (40, 42, 240, 340, 342) that each extend radially inward from the carrier body into contact with a radially-outwardly facing surface (74, 274, 374) of at least one of the first mount post (70, 270, 370) and the second mount post (72, 272, 372) of the blade track segment (26, 226, 326) to radially locate the blade track segment relative to the carrier; and an intermediate carrier (28, 228, 328) configured to couple the blade track segment to the carrier, the intermediate carrier including an intermediate carrier body (30, 230, 330) arranged in the channel (71, 371) axially between the first mount post and the second mount post, the intermediate carrier body shaped to include pin holes (81, 83), at least one pin (32, 232, 332) that extends axially into the first mount post, the intermediate carrier body, and the second mount post to couple the intermediate carrier body to the blade track segment, and at least one retainer (36, 236, 336) that extends radially outward from the intermediate carrier body through the carrier to couple the intermediate carrier and the blade track segment with the carrier, wherein the at least one retainer includes a threaded coupling formed integrally with the intermediate carrier body (30, 230, 330) that extends radially outward from the intermediate carrier body and a threaded fastener (86, 286, 386) that extends radially inward through the carrier (24, 224, 324) into the coupling to couple the intermediate carrier (28, 228, 328) with the carrier (24, 224, 324).