At section A-A, Sy=0 and Txy=0

	Sx=(P/A) + ((M1*c)/I)
	Tmax = Sx/2

Normal stress Sx = 158.4 MPa
Shear stress Tmax = 79.2 MPa

At section B-B, Sy=0 and Txy=0

	Sx=((M1*c)/I)

Normal stress Sx = 194.4 MPa
Shear stress Tmax = 97.2 MPa