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What is the designed structural loading for the wings and fuselage?

April 26, 2017designed fuselage loading structural wings

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What is the designed structural loading for the wings and fuselage?

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The wing was built to design loads of 4.5g/-3g with +9g/-6g safety factor. It is in utility category at gross weight of 1,250lbs. The fuselage and tail are well beyond that simply due to the minimum number of exterior layers needed for impact resistance.