[fltsim.0] title=Wright's Flyer sim=03flyer model= panel= sound= texture= checklists= atc_id=W1 ui_manufacturer=Wright Bros ui_type=Flyer description=Orville and Wilber Wright were the first to demonstrate powered (and controlled) flight to the world. ui_variation= atc_heavy=0 atc_airline= atc_flight_number= [forcefeedback] gear_bump_nose_magnitude=6000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=6000 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=6000 gear_bump_right_direction=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [fltsim.1] title= sim= panel= sound= texture= model= [fltsim.2] title= sim= panel= sound= texture= model= [fltsim.3] title= sim= panel= sound= texture= model= [fltsim.4] title= sim= panel= sound= texture= model= [fltsim.5] title= sim= panel= sound= texture= model= [fltsim.6] title= sim= panel= sound= texture= model= [fltsim.7] title= sim= panel= sound= texture= model= [fltsim.8] title= sim= panel= sound= texture= model= [fltsim.9] title= sim= panel= sound= texture= model= [General] performance=Length: 19 ft 9 in\nSpan: 40 ft 4 in\nWeight: 750 lbs\nPower: 12 hp @ 400 rpm\nRange: not very far\nDate: December 1903\nDetails:\nDesigner: Orville and Wilber Wright (model by Paul B. KSMS\/KSSC) atc_type= atc_model= [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight= 600.000 empty_weight_roll_MOI= 5000.000 empty_weight_pitch_MOI= 6000.000 empty_weight_yaw_MOI= 9000.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 750.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] Center1= -1.667, 0.000, 0.000, 1.000, 0.000 fuel_type=1.000000 number_of_tank_selectors=1 [airplane_geometry] wing_area= 510.000 wing_span= 40.000 wing_root_chord= 6.500 wing_dihedral= 2.999 wing_incidence= 0.000 wing_twist= -1.000 oswald_efficiency_factor= 0.250 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 48.000 htail_span= 12.000 htail_pos_lon= -10.000 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 20.000 vtail_span= 6.270 vtail_sweep= 0.000 vtail_pos_lon= -11.220 vtail_pos_vert= 0.000 elevator_area= 48.000 aileron_area= 18.300 rudder_area= 20.000 elevator_up_limit= 20.000 elevator_down_limit= 20.000 aileron_up_limit= 15.000 aileron_down_limit= 15.000 rudder_limit= 20.000 elevator_trim_limit= 20.000 spoiler_limit= 0.000 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [contact_points] point.0= 1.000, -9.500, 0.000, -5.300, 1574.803, 0.000, 0.507, 36.840, 0.571, 2.500, 0.834, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, 4.167, -2.250, -5.000, 1574.803, 1.000, 0.507, 0.000, 0.293, 2.500, 0.786, 0.000, 0.000, 2.000, 0.000, 0.000 point.2= 1.000, 4.167, 2.250, -5.000, 1574.803, 2.000, 0.507, 0.000, 0.293, 2.500, 0.786, 0.000, 0.000, 3.000, 0.000, 0.000 point.3= 2.000, 0.000, -20.000, -5.000, 787.402, 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, 0.000, 20.000, -5.000, 787.402, 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, -13.000, 0.000, 0.000, 787.402, 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, 2.417, 0.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= 0.000 static_cg_height= 4.900 [GeneralEngineData] engine_type= 0 Engine.0= -4.000, -2.000, 0.000 Engine.1= -4.000, 2.000, 0.000 fuel_flow_scalar= 1.000 [piston_engine] max_rpm_mechanical_efficiency_scalar=0.842 idle_rpm_mechanical_efficiency_scalar=0.640 max_rpm_friction_scalar=1.262 idle_rpm_friction_scalar=0.610 cylinder_displacement= 81.800 compression_ratio= 8.000 number_of_cylinders= 4 max_rated_hp= 12.000 max_rated_rpm= 1025.000 fuel_metering_type= 1 cooling_type= 1 normalized_starter_torque= 0.300 turbocharged= 0 max_design_mp= 0.000 min_design_mp= 0.000 critical_altitude= 0.000 emergency_boost_type= 0 emergency_boost_mp_offset= 0.000 emergency_boost_gain_offset= 0.000 fuel_air_auto_mixture= 0 auto_ignition= 0 power_scalar=0.780 [propeller] propeller_type= 1 propeller_diameter= 8.000 propeller_blades= 2 propeller_moi= 4.003 beta_max= 5.565 beta_min= 15.000 min_gov_rpm= 100.000 prop_tc= 0.100 gear_reduction_ratio= 1.750 fixed_pitch_beta= 20.000 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 0 prop_feathering_available= 0 prop_auto_feathering_available= 0 min_rpm_for_feather= 0.000 beta_feather= 0.000 power_absorbed_cf= 0.000 defeathering_accumulators_available= 0 prop_reverse_available= 0 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 thrust_scalar=1.000 [flight_tuning] cruise_lift_scalar=0.920 parasite_drag_scalar=1.500 induced_drag_scalar=0.958 elevator_effectiveness=1.849 aileron_effectiveness=1.000 rudder_effectiveness=4.000 pitch_stability=1.318 roll_stability=0.958 yaw_stability=0.920 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [Reference Speeds] flaps_up_stall_speed= 24.000 full_flaps_stall_speed= 24.000 cruise_speed= 45.000 [keyboard_response] elevator=200.000000,1000.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 [Views] eyepoint=-1, -1, 1.6 [autopilot] autopilot_available=0 flight_director_available=0 [direction_indicators] direction_indicator.0=1,0 [SMOKESYSTEM] smoke.0=-0.5,-2.333,-3.833, fx_smoke_r smoke.1=-0.5,-2.333,3.833, fx_smoke_w smoke.2=-0.5,-2.333,-8.833, fx_smoke_w smoke.3=-0.5,-2.333,8.833, fx_smoke_r smoke.4=-0.5,-2.333,-14.833, fx_smoke_r smoke.5=-0.5,-2.333,14.833, fx_smoke_w smoke.6=-0.5,-2.333,-22.833, fx_smoke_w smoke.7=-0.5,-2.333,22.833, fx_smoke_r [Flaps.0] type= 0 span-outboard= 0.500 extending-time= 0.100 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= 0.000, 0.000