I did a quick look and am almost done. Make a back-up copy of the aircraft cfg then just copy and paste the sections below over the relevant cfg sections. Note that some sections are partial so be careful to only replace the lines given.
I consulted videos, specs, and my own limited flight experience to arrive at what I have but anyone with real time in these should speak up so I can make it as real as I can. Performance is with sliders 3/4 towards realistic. The extra wheel points are an experiment to prevent pitching over on braking while keeping a good settled attitude while otherwise on the ground.
[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= -1.000, 0.000, 0.100
max_number_of_stations=50
station_load.0= 300, 18.0, 0.0, 3.0
station_load.1= 0, 0.0, 0.0, 0.0
station_load.2= 0, 0.0, 0.0, 0.0
empty_weight= 2000.000
empty_weight_roll_MOI= 2037.000
empty_weight_pitch_MOI= 5000.000
empty_weight_yaw_MOI= 2800.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 2780.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[airplane_geometry]
wing_area= 190.000
wing_root_chord= 4.917
wing_dihedral= 1.736
wing_twist= -2.999
[GeneralEngineData]
engine_type= 0
Engine.0= 6.000, 0.000, 0.900
fuel_flow_scalar= 1.000
min_throttle_limit=0.000000
[piston_engine]
power_scalar=1.000
[propeller]
thrust_scalar=1.000
[Reference Speeds]
flaps_up_stall_speed= 54.000
full_flaps_stall_speed= 43.200
cruise_speed= 133.831
max_indicated_speed=170.000000
[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.000
roll_stability=0.500
yaw_stability=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=0.800
rudder_effectiveness=0.800
elevator_trim_effectiveness=0.800
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
[contact_points]
point.0= 1, -17.91, 0.00, -1.40, 3500, 0, 0.51, 42, 0.19, 2.50, 1.08, 0.00, 0.000, 0.000, 0.000, 0.000
point.1= 1, 3.30, -4.00, -6.10, 3500, 0, 0.51, 0, 0.26, 2.50, 0.62, 0.00, 0.000, 2.000, 0.000, 0.000
point.2= 1, 3.30, 4.00, -6.10, 3500, 0, 0.51, 0, 0.26, 2.50, 0.62, 0.00, 0.000, 3.000, 0.000, 0.000
point.3= 1, 2.00, -4.00, -6.00, 3500, 1, 0.51, 0, 0.26, 2.50, 0.62, 0.00, 0.000, 2.000, 0.000, 0.000
point.4= 1, 2.00, 4.00, -6.00, 3500, 2, 0.51, 0, 0.26, 2.50, 0.62, 0.00, 0.000, 3.000, 0.000, 0.000
static_pitch= 11.630
static_cg_height= 4.820
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 7.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.200
pitch_scalar= -0.500
flaps-position.0= 0.000, 0.000
flaps-position.1= 12.666, 0.000
flaps-position.2= 25.332, 0.000
flaps-position.3= 37.999, 0.000
[brakes]
toe_brakes_scale=0.5
parking_brake=1