An air seal assembly for a gas turbine engine , 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 leading edge side ; and a clip mounting flange extending from said trailing edge side ; a blade outer air seal 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 ; and a shelf formed from said lower region extending axially outward from said pocket on said trailing edge of said body ; and a clip configured to detachably couple with said clip mounting flange , characterised in that : the air seal assembly comprises a clip receiver communicating through said blade outer air seal control ring from said leading edge side to said trailing edge side , wherein said clip mounting flange is proximate said clip receiver ; said blade outer air seal comprises a notch being formed into said upper region ; said clip is insertable into said clip receiver and configured to engage said notch of the blade outer air seal ; and said blade outer air seal comprises a ceramic matrix composite material. 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 leading edge side ; and a clip mounting flange extending from said trailing edge side ; a leading edge side and a trailing edge side opposite said leading edge side ; a hook protruding axially from said leading edge side ; and a clip mounting flange extending from said trailing edge side ; a blade outer air seal 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 ; and a shelf formed from said lower region extending axially outward from said pocket on said trailing edge 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 ; and a shelf formed from said lower region extending axially outward from said pocket on said trailing edge of said body ; and a clip configured to detachably couple with said clip mounting flange , characterised in that : the air seal assembly comprises a clip receiver communicating through said blade outer air seal control ring from said leading edge side to said trailing edge side , wherein said clip mounting flange is proximate said clip receiver ; said blade outer air seal comprises a notch being formed into said upper region ; said clip is insertable into said clip receiver and configured to engage said notch of the blade outer air seal ; and said blade outer air seal comprises a ceramic matrix composite material. the air seal assembly comprises a clip receiver communicating through said blade outer air seal control ring from said leading edge side to said trailing edge side , wherein said clip mounting flange is proximate said clip receiver ; said blade outer air seal comprises a notch being formed into said upper region ; said clip is insertable into said clip receiver and configured to engage said notch of the blade outer air seal ; and said blade outer air seal comprises a ceramic matrix composite material. <EOS>