Shroud pin for gas turbine engine shroud

A shroud assembly for a gas turbine engine, the shroud assembly comprising:

• a shroud segment extending substantially along a circumferential direction and comprising a shroud wall, the shroud wall defining a shroud attachment opening;
• a hanger assembly comprising a hanger wall defining a hanger attachment opening;
• and an attachment pin assembly, comprising
• a first member comprising a first body defining a hollow core and having a first portion provided within the hanger attachment opening and defining an interference fit between the first portion and the hanger wall, the first body further comprising a shoulder abutting the hanger wall, the first body further extending through the shroud attachment opening;
• a second member comprising a second body extending between a first end and a second end and including a rim at the first end, the second body extending through the hollow core of the first member;
• and
• a secondary attachment member provided with the second body and adapted to retain the second body within the first body.