A sealing arrangement to seal a gap between a first turbine component and a second turbine component in a gas turbine engine, the sealing arrangement comprising: a first arcuate feather seal comprising an anchored end segment and a free end segment , wherein the anchored end segment of the first arcuate feather seal is connected to an anchoring assembly of the sealing arrangement affixed to the first turbine component ; and a second arcuate feather seal comprising an anchored end segment and a free end segment , wherein the anchored end segment of the second arcuate feather seal is affixed to the second turbine component , wherein the first arcuate feather seal and the second arcuate feather seal are responsive to a pressure differential that develops across the gap to form a pressure-loaded sealing joint between respective sealing surfaces of the first arcuate feather seal and the second arcuate feather seal , to contactively engage the first arcuate feather seal and the second arcuate feather seal wherein the respective sealing surface of the first arcuate feather seal is disposed at the free end segment of the first arcuate feather seal , the free end segment disposed opposite the anchored end segment of the first arcuate feather seal , and wherein the respective sealing surface of the second arcuate feather seal is disposed at the free end segment of the second arcuate feather seal , the free end segment disposed opposite the anchored end segment of the second arcuate feather seal , wherein the free end segment of the second arcuate feather seal is disposed radially outward relative to the anchored end segment of the second arcuate feather seal . a first arcuate feather seal comprising an anchored end segment and a free end segment , wherein the anchored end segment of the first arcuate feather seal is connected to an anchoring assembly of the sealing arrangement affixed to the first turbine component ; and a second arcuate feather seal comprising an anchored end segment and a free end segment , wherein the anchored end segment of the second arcuate feather seal is affixed to the second turbine component , wherein the first arcuate feather seal and the second arcuate feather seal are responsive to a pressure differential that develops across the gap to form a pressure-loaded sealing joint between respective sealing surfaces of the first arcuate feather seal and the second arcuate feather seal , to contactively engage the first arcuate feather seal and the second arcuate feather seal wherein the respective sealing surface of the first arcuate feather seal is disposed at the free end segment of the first arcuate feather seal , the free end segment disposed opposite the anchored end segment of the first arcuate feather seal , and wherein the respective sealing surface of the second arcuate feather seal is disposed at the free end segment of the second arcuate feather seal , the free end segment disposed opposite the anchored end segment of the second arcuate feather seal , wherein the free end segment of the second arcuate feather seal is disposed radially outward relative to the anchored end segment of the second arcuate feather seal . <EOS>