[fltsim.0] title=PZL P-37A Los sim=pzlp37A model= panel= sound= texture= checklists= [WEIGHT_AND_BALANCE] empty_weight = 19480 // (pounds) reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = 170, 12.0, -4.0, 2.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.0 = 170, 12.0, 4.0, 2.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 61203.47 //slug-ft^2 empty_weight_roll_MOI = 43209.89 //slug-ft^2 empty_weight_yaw_MOI = 83573.24 //slug-ft^2 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.0 aileron_effectiveness = 1.0 rudder_effectiveness = 1.0 pitch_stability = 1.0 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [piston_engine] power_scalar = 1.0 [propeller] thrust_scalar=1.0 rotation= -1,1 //Engine 1,2,3,... Rotation direction. 1 = CW, -1 = CCW [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second [electrical] max_battery_voltage = 24.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps = 60.0 [contact_points] //0 Class //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type point.0= 1.000, -38.417, 0.000, 1.50, 1574.803, 0.000, 0.666, 57.660, 0.195, 2.500, 0.916, 33.000, 33.000, 0.000, 0.000, 0.000 point.1= 1.000, 3.417, -9.917, -7.850, 1574.803, 1.000, 0.666, 0.000, 0.366, 2.500, 0.773, 5.000, 5.000, 2.000, 0.000, 0.000 point.2= 1.000, 3.417, 9.917, -7.850, 1574.803, 2.000, 0.666, 0.000, 0.366, 2.500, 0.773, 5.000, 5.000, 3.000, 0.000, 0.000 point.3= 2.000, -8.500, -47.500, 0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -8.500, 47.500, 0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -27.333, 0.000, 0.750, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 18.833, 0.000, -1.667, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= 12.90 static_cg_height= 7.40 [Views] eyepoint=12.1, -0.25, 4.25 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 5.000 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 15.000, 0.000 flaps-position.2= 30.000, 0.000 flaps-position.3= 45.000, 0.000 [Flaps.1] type= 2 span-outboard= 0.200 extending-time= 5.000 system_type= 0 damaging-speed= 0.000 blowout-speed= 0.000 lift_scalar= 0.100 drag_scalar= 0.100 pitch_scalar= 0.100 flaps-position.0= 0.000, 0.000 flaps-position.1= 5.000, 0.000 flaps-position.2= 10.000, 0.000 flaps-position.3= 15.000, 0.000