[fltsim.0] title=P-51D Duchess Arlene sim=FDG-P51D V11b model= panel= sound= texture= [WEIGHT_AND_BALANCE] empty_weight=7635 // (lbs.) 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, -2.09, 0.0, 0.5 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=11442.32 empty_weight_roll_MOI=8056.44 empty_weight_yaw_MOI=15600.73 [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 [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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) point.0=1, -12.986, 0.00, -3.325, 5000, 0, 0.577, 90.0, 0.30, 2.5, 0.90, 5, 5, 0, 0, 150 //Tail Wheel point.1=1, 3.7, -5.855, -7.4, 3600, 1, 1.66, 0.0, 0.45, 2.5, 0.83, 12.5, 15, 2, 0, 150 //Left Wheel point.2=1, 3.7, 5.855, -7.4, 3600, 2, 1.66, 0.0, 0.45, 2.5, 0.83, 12.5, 15, 2, 0, 150 //Right Wheel point.3=2, 1.3,-17.856, -1, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5 //Left Wing Tip point.4=2, 1.3, 17.856, -1, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6 //Right Wing Tip point.5=2, -17.5, 0.00, -3, 2400, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9 //Tail Contact Point point.6=2, 8.9, 0.00, -5, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4 //Nose Contact Point static_cg_height = 6.17 //(feet) altitude of CG when at rest (altitude when loaded on ground) static_pitch = 13.38 //degrees (pitch when loaded on ground) [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.125 // 0.0 .. 1.0 extending-time=12 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=11 // degrees, KIAS flaps-position.2=22 // degrees, KIAS flaps-position.3=32 // degrees, KIAS flaps-position.4=43 // degrees, KIAS damaging-speed=185 // KIAS blowout-speed=250 // KIAS [Views] eyepoint=-1.2, 0.000000, 2.25 //(feet) longitudinal, lateral, vertical distance from reference datum [LIGHTS] panel=0.00, -1.5, 3.15, fx_vclight