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I Review Due to an unequal distribution of fuel in the wing tanks, the centers of gravity for the airplane fuselage A and win

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Taking Moment about y Emy=0; 8000 llo 10 ,4300016 ND (8000X 4) +(43000) (4) +6000(4) - NF (27)=0 Nf=13.22222 kip Enzo; (8000

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