Well, 3" at the tip of a 168" wing (per DE Left wing drawing / 3" tilt is listed) boils down to a measly 1 deg. dihedral per side.
The restoring rolling moment will be 1.8% of the lift generated. At a DE AUW of 900 lbf, that equates to 16 lbf.
Did not calculate but I suspect that the pendulum effect of engine, fuselage and pilot weight - forget fuse drag for the moment - will be more relevant.
Mr. DErwin, as said above, look at left wing drawing and in the text below it is stated dihedral to be provided by a 3" tilt upwards.
Cheers,
azevedoflyer😎