FST_Model 1
airframe_weight 20000
airframe_drag 7.00
uc_drag 2.50
airbrake_drag 4.00
dihedral 5.50
incidence 1.00
stall_angle 30.00
wing_efficiency 1.00
control_power 0.95
roll_inertia 4.00
pitch_inertia 4.00
retracts 1
flaps 1
airbrakes 1
biplane 0
tail_dragger 0
ejector 1
thrust 8050
fuel_weight 10000
num_engines 4
jet_engine 0
units_per_meter 5
grid_space 5
x_centre 204
33 0
12 6
-14 6
12 -6
-14 -6
-45 0
-57 0
12 85
-3 83
12 -85
-3 -83
-45 22
-56 22
-45 -22
-56 -22
-124 179
-147 179
-124 200
-147 200
