Due to an unequal distribution of fuel in the wing tanks, the centers of gravity for the a...

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 lb. wB = 8000 lb, and WC = 6000 lb. determine the normal reactions of the wheels d, E, and F on the ground.