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If these components have weights wa 45 000 1b wb 8000 1b

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Reference no: EM13628632

Due to an unequal distribution of fuel in the wing tanks the centers of gravity for the airplane fuselage A and wings B and C are located as shown. If these components have weights WA = 45 000 1b. WB = 8000 1b, and WC = 6000 lb, determine the normal reactions of the wheels D, E and F on the ground.

Reference no: EM13628632

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