Using both the LRFD methods, determine whether the connection shown in the figure is adequate to support the applied loads; consider the strength of the bolts in shear and bearing on the plate. The plates are ASTM A$36$ and the fasteners are $3/4-$in$-$diameter ASTM A$490$ A$325$ bolts in standard holes $($when threads are not excluded from shear planes$).$ The applied factored load is $Pu=60$ kips $($LRFD$).$ Assume deformation at the hole at service loads is a design consideration and all high$-$strength bolts in a slip$-$critical connection with a Class A faying surface.