SEAL ASSEMBLY FOR A GAS TURBINE ENGINE

An assembly (60) for a gas turbine engine (20) comprising a component (66) that has a first interface portion (74), and a support (68) that has a mounting portion (76) and a second interface portion (78), the mounting portion (76) attachable to an engine static structure (36), a first retention feature (80) that releasably secures the first interface portion (74) to the support (68) in a first installed position of the gas turbine engine component (66), and a second retention feature (82) dimensioned to secure the first interface portion (74) to the second interface portion (78) in a second installed position of the gas turbine engine component (66). The first installed position differs from the second installed position, and one of first and second retention features is dimensioned to carry the gas turbine engine component (66) in response to release of another one of the first and second retention features.