Ceramic matrix composite seal segment for a gas turbine engine

A segmented turbine shroud radially encasing a turbine in a gas turbine engine, said shroud comprising:

• a carrier comprising at least one carrier member defining a carrier bore;
• a ceramic matrix composite (CMC) seal segment comprising a flange having:
• a flange comprising opposing major surfaces, one major surface facing radially inward and the other major surface facing radially outward relative to an axis of rotation of the turbine;
• a portion extending radially outward from the major surface facing radially outward, said portion at least partially defining a pin-receiving seal segment bore for receiving an elongated pin, wherein said pin-receiving seal segment bore is aligned with said axis of rotation;
• and
• one or more elongated pins, wherein said CMC seal segment is carried by said carrier by at least one of said elongated pins being received with said carrier bore and said seal segment bore.