Try to experiment a little bit (if you have'nt done so) with the axial movement parameters:
Line Num.5 Maximim Aileron Angle
Line Num.22 Roll Inertia Moment
Of course from what I've concluded the program is really good but it lack some fine details about realism in flight.
Anyway this is a pretty good (by my standards) .par file, just put those in your (low-wing) plane
Example of .par
0 1:Type(-) Type[0=Plane] ParDesigner Ver0.8
15 2:Tmax(N) Maximum Thrust
0.30 3:Drmax(rad) Maximun Rudder Angle
0.10 4:Demax(rad) Maxmim Elevator Angle
0.020 5:Damax(rad) Maximim Aileron Angle
1.0 6:CLmax(-) Maximum Lift Coefficient
-1.0 7:CLmin(-) Minimum Lift Coefficient
6.3 8:CLa(/rad) Lift Gradient
10 9:CLaSt(/rad) Lift Gradient in Stall
0.02 10:CDw(-) Drag Coefficient of Wing
0.04 11:CDb(-) Drag Coefficient of Fuselage
0.2 12:mug(-) Friction Coefficient of Wheels
0.69 13:dCDSt(-) Rise of Drag Coefficient in Stall
0.00 14:CM(-) Moment Coefficient
0.015 15:alpha0(rad) Wing Angle
1.48 16:b(m) Wing Span
0.23 17:c(m) Wing Chord
0.10 18:hce(m) Equivalent Center of Gravity
1.5 19:m(Kg) Mass
0.18 20:Izz(Kg*m^2) Yaw Inertia Moment
0.024 21:Iyy(Kg*m^2) Pitch Inertia Moment
0.010 22:Ixx(Kg*m^2) Roll Inertia Moment
0.05 23:She(m^2) Effective Area of Stab
0.06 24:Sfe(m^2) Effective Area of fin
0.70 25:Lt(m) Tail Moment Arm
0.001 26:VForm(-) Effect of Dihedral Angle
Regards,
Christos
