The combined cab and payload weight, amplified by the impact factor, is shared by the support brackets. The lower panel shows the bending-moment diagram (triangular) of a single bracket beam under central point load.
$$W_{\text{tot}} = (m_{\text{rated}} + m_{\text{cab}})\cdot g\cdot K_{\text{imp}}, \qquad P = \frac{W_{\text{tot}}}{n}$$
Total load W_tot and per-bracket load P. K_imp is the impact factor, n the number of brackets, g = 9.81 m/s².
$$M = \frac{P\,L}{4}, \qquad I = \frac{b\,h^{3}}{12}, \qquad Z = \frac{I}{h/2} = \frac{b\,h^{2}}{6}$$
Maximum bending moment M for a simply supported beam under central point load, second moment of area I, and section modulus Z. b is beam thickness, h is beam height.
$$\sigma_{\max} = \frac{M}{Z}, \qquad \mathrm{SF} = \frac{f_y}{\sigma_{\max}}, \qquad \delta = \frac{P\,L^{3}}{48\,E\,I}, \qquad \delta_a = \frac{L}{360}$$
Maximum bending stress σ_max, safety factor SF against yield, midspan deflection δ, and allowable deflection δ_a. E_steel = 200 GPa fixed.