A seal assembly for a gas turbine engine, the seal assembly comprising: a blade outer air seal control ring comprising: a leading edge side and a trailing edge side opposite said leading edge side; a hook protruding axially from said trailing edge side; a clip receiver communicating through said blade outer air seal control ring from said leading edge side to said trailing edge side; and a clip mounting flange extending from said trailing edge side proximate said clip receiver; a blade outer air seal comprising a ceramic matrix composite material and coupled to said blade outer air seal control ring, said blade outer air seal comprising: a body having a leading edge and a trailing edge opposite thereof; a pocket formed into said body having an upper region and a lower region, said pocket configured to receive and engage with said hook; a notch being formed into said upper region; and a shelf formed from said lower region extending axially outward from said pocket on said trailing edge side of said body; and a clip comprising: a clip base having a control ring interface; and a biasing element coupled to said clip base opposite said control ring interface, wherein said clip is insertable into the clip receiver and configured to engage the notch of the blade outer air seal and configured to detachably couple with the clip mounting flange. a blade outer air seal control ring comprising: a leading edge side and a trailing edge side opposite said leading edge side; a hook protruding axially from said trailing edge side; a clip receiver communicating through said blade outer air seal control ring from said leading edge side to said trailing edge side; and a clip mounting flange extending from said trailing edge side proximate said clip receiver; a leading edge side and a trailing edge side opposite said leading edge side; a hook protruding axially from said trailing edge side; a clip receiver communicating through said blade outer air seal control ring from said leading edge side to said trailing edge side; and a clip mounting flange extending from said trailing edge side proximate said clip receiver; a blade outer air seal comprising a ceramic matrix composite material and coupled to said blade outer air seal control ring, said blade outer air seal comprising: a body having a leading edge and a trailing edge opposite thereof; a pocket formed into said body having an upper region and a lower region, said pocket configured to receive and engage with said hook; a notch being formed into said upper region; and a shelf formed from said lower region extending axially outward from said pocket on said trailing edge side of said body; and a body having a leading edge and a trailing edge opposite thereof; a pocket formed into said body having an upper region and a lower region, said pocket configured to receive and engage with said hook; a notch being formed into said upper region; and a shelf formed from said lower region extending axially outward from said pocket on said trailing edge side of said body; and a clip comprising: a clip base having a control ring interface; and a biasing element coupled to said clip base opposite said control ring interface, wherein said clip is insertable into the clip receiver and configured to engage the notch of the blade outer air seal and configured to detachably couple with the clip mounting flange. a clip base having a control ring interface; and a biasing element coupled to said clip base opposite said control ring interface, wherein said clip is insertable into the clip receiver and configured to engage the notch of the blade outer air seal and configured to detachably couple with the clip mounting flange.