Be sure to draw the free-body diagrams, show calculation steps, use the right symbols, and highlight final answers including units. 1. 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 = 45000 lb, We = 8000 lb, and We = 6000 lb, determine the normal reactions of the wheels D, E, and F on the ground. D bE 8 ft 4 ft 6 ff 8 ft 20 ft 3 it 6 ft (Optional: The time I spent on this problem was minutes.)Be sure to draw the free-body diagrams, show calculation steps, use the right symbols, and highlight final answers including units. 1. 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 = 45000 lb, We = 8000 lb, and We = 6000 lb, determine the normal reactions of the wheels D, E, and F on the ground. D bE 8 ft 4 ft 6 ff 8 ft 20 ft 3 it 6 ft (Optional: The time I spent on this problem was minutes.)