Please see the most recent updates in the "Where did the .com name go?" thread. Posts number 16 and 17.
empty_weight_CG_position = -3.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
[airplane_geometry]
wing_area = 174.0 //Square feet
wing_span = 36.1 //Feet
wing_root_chord = 4.9 //Feet
wing_dihedral = 1.7 //Degrees
wing_incidence = 1.5 //Degrees
wing_twist = -3.0 //Degrees
oswald_efficiency_factor= 0.68 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 0 //Degrees, wing leading edge
wing_pos_apex_lon = -2.4 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
[fuel]
LeftMain = -3.9, -2.1, 2.5, 26.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -3.9, 2.1, 2.5, 26.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
. . . go into the aircraft.cfg file and under the flight tuning section, adjust the roll stability upward to decrease the tendency to roll back and downward to increase it. . . .