Three design considerations have been investigated.
1. Based on the allowable normal stress in member $\left(1\right)$:

$\mathrm{w} = 34.08 \mathrm{kN/}\mathrm{m}$

2. Based on the allowable shear stress in bolts $\mathrm{A}$ and $\mathrm{B}$:

$\mathrm{w} = 24.92 \mathrm{kN/}\mathrm{m}$

3. Based on the allowable shear stress in bolt $\mathrm{C}$:

$\mathrm{w} = 19.05 \mathrm{kN/}\mathrm{m}$