The wind of an aircraft is subjected to a thrust force due to the engine of T = 8 kN. The resulting lift force is given as L = 45 kN. IF the mass of the wing is 2.1 Mg and the center is found to be at point G, determine the support reactions at point A where the wing is fixed to the fuselage. Remember to provide forces and reactions on a FBD for full credit. 2.5 m T=8KN L= 45 kN