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{"ops":[{"insert":"Critique Bombardier\u2019s choice of Al-alloy 2198-T8 for the fuselage of the A220\/Cseries. In your answer you must: \u2022 explain the main design drivers for fuselage skin material selection, \u2022 state which of the alloys in Table Q1 would previously have been selected for this component and \u2022 suggest why Bombardier choose 2198-T8.\n"}]}
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