Given the loading shown, determine the internal loading (Fx.FX, F., Mx, My, Mz) at the cross section. Identify the stress component (Ox, Oy, Oz, txy, tyz, Txx) at location A (on y-axis) Draw a volurpe element of the material at this point, and stow the results on the elemerh Draw 3D Mohr's circles and determine the principal stresses (01,02,03). Given the diameter is 1.25 in, and the brittle material Su = 60 ksi, Sue 80 ksi, determine the factor of safety, N, based on CMT