Given:
\( d = 250 \) mm, \( S = 5 \) mm, \( t = 10 \) mm, Thickness of flat plate = \( 5 \) mm,
\( f_u = 410 \) N/mm², \( \gamma_{{mw}} = 1.25 \)
Step 1: Throat thickness of the weld (\( t_t \))
\[
t_t = 0.75 \times 5 = 3.5 \text{ mm}
\]
Step 2: Calculation of Section Modulus (\( Z_p \))
\[
Z_p = \frac{J}{r} = \frac{A r^2}{r} = A r
\]
Using geometry for a circular section:
\[
Z_p = \left(\pi \times t \times \frac{d}{2}\right) \times \frac{d^2 t}{2}
\]
\[
Z_p = \left(\pi \times 10 \times \frac{250}{2}\right) \times \frac{250^2 \times 3.5}{2}
\]
Step 3: Torque that can be applied on the plate
The maximum torque is given by:
\[
T = (f_s \times Z_p) = \left(\frac{f_u}{\sqrt{3} \gamma_{{mw}}}\right) \times \left(\pi \times \left(\frac{d^2 t}{2}\right)\right)
\]
Substituting the known values:
\[
T = \left(\frac{410}{\sqrt{3} \times 1.25}\right) \times \pi \times \frac{250^2 \times 3.5}{2}
\]
\[
T = 65.07 \text{ kN.m} \approx 65.1 \text{ kN.m}
\]
Thus, the torque that can be resisted by the weld is \( \boxed{65.1} \) kN.m.