[fltsim.0] title=Piper Cub AI 1 sim=Cubai model= panel= sound= texture= kb_checklists= kb_reference= atc_type=Piper atc_model=j3 atc_id=N-3477L ui_manufacturer=PIPER ui_type=Cub AI 1 ui_variation= description=\n [fltsim.1] title=Piper Cub AI 2 sim=Cubai model= panel= sound= texture=1 kb_checklists= kb_reference= atc_type=Piper atc_model=j3 atc_id=N-3477L ui_manufacturer=PIPER ui_type=Cub AI 2 ui_variation= description=\n [General] atc_type=Piper atc_model=j3 atc_id=N-2255L performance=\n\n [forcefeedback] gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [WEIGHT_AND_BALANCE] empty_weight=950 // (pounds) reference_datum_position=3.6, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-4.0, 0, 0.0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=170, -3.0, -1.5, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170, 0.0, 1.5, 0.0 //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=0, -8.0, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=2672.0 empty_weight_roll_MOI=1037.0 empty_weight_yaw_MOI=1760.0 CG_forward_limit=0.000000 CG_aft_limit=-3.000000 empty_weight_coupled_MOI=0.000000 max_gross_weight=935.000000 [flight_tuning] cruise_lift_scalar=1.1 parasite_drag_scalar=2.35 induced_drag_scalar=1.0 elevator_effectiveness=1.4 aileron_effectiveness=1.4 rudder_effectiveness=1.4 pitch_stability=1.3 roll_stability=1.1 yaw_stability=2.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [piston_engine] power_scalar = 1.0 //Piston power scalar cylinder_displacement= 44.0 //Cubic inches per cylinder compression_ratio= 7.5 //Compression ratio number_of_cylinders=4 //Number of cylinders max_rated_rpm= 2300 //Max rated RPM max_rated_hp= 65 //Max rated HP fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque= 0.3 //Starter torque factor turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp= 0 //Max design manifold pressure, (inHg) min_design_mp= 0 //Min design manifold pressure, (inHg) critical_altitude= 0 //Altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar= 0.2 //Scalar on idle RPM friction [propeller] thrust_scalar = 2.0 //Propeller thrust scalar propeller_type= 1 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 6.0 //Propeller Diameter, (feet) propeller_blades= 2 //Number of propeller blades propeller_moi= 0.80 //Propeller moment of inertia beta_max= 0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm= 0 //Miminum governed RPM prop_tc= 0.1 //Prop time-constant gear_reduction_ratio= 1.0 //Propeller gear reduction ratio fixed_pitch_beta= 13.75 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit= 80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available= 0 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available= 0 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available= 0 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather= 0 //Minimum RPM for prop feathering beta_feather= 0 //Feathering pitch angle (degrees) power_absorbed_cf= 0 //Coefficient of friction for power absorbed by propeller in feather defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta= 0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta= 0 //Minimum pitch angle in reverse, (degrees) [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus=0, 1, 3.0 avionics=1, 1 , 3.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 1 , 2.0 light_panel=0, 1 , 2.0 //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 [contact_points] point.0=1, -19.30, 0.00, -0.50, 5000.0, 0, 0.5124, 67.0, 0.4, 2.5, 0.6, 0.0, 0.0, 0.0, 0.0,0.0 point.1=1, -2.8, -3.0, -5.2, 1968.50, 1, 0.5124, 0.0, 0.7, 2.5, 0.7, 0.0, 0.0, 1.0, 0.0, 0.0 point.2=1, -2.8, 3.0, -5.2, 1968.50, 2, 0.5124, 0.0, 0.7, 2.5, 0.7, 0.0, 0.0, 2.0, 0.0, 0.0 point.3=2, -4.80, -16.25, 0.20, 1787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0 point.4=2, -4.80, 16.25, 0.20, 1787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0 point.5=2, -19.30, 0.00, 3.8, 2787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0 point.6=2, 1.67, 0.00, -1.83, 1787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0 point.7=2, -19.30, 0.25, -0.48, 2900, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0 point.8=2, -19.30, -0.25, -0.48, 2900, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0 //[contact_points] //point.0=1, -19.30, 0.00, -0.6, 2977.95, 0, 0.0124, 67.0, 0.03, 2.5, 1.77, 0.0, 0.0, 0.0, 0.0,0.0 //point.1=1, -2.8, -3.0, -5.1, 1968.50, 1, 0.5124, 0.0, 0.7, 2.5, 0.7, 0.0, 0.0, 1.0, 0.0, 0.0 //point.2=1, -2.8, 3.0, -5.1, 1968.50, 2, 0.5124, 0.0, 0.7, 2.5, 0.7, 0.0, 0.0, 2.0, 0.0, 0.0 //point.3=2, -4.80, -16.25, 0.20, 1787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0 //point.4=2, -4.80, 16.25, 0.20, 1787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0 //point.5=2, -19.30, 0.00, -0.8, 2787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0 //point.6=2, 1.67, 0.00, -1.83, 1787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0 //point.7=2, -19.30, 0.3, -0.25, 2900, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0 //point.8=2, -19.30, -0.3, -0.25, 2900, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0 //static_pitch=13.54 //static_cg_height=4.2 static_pitch=13.54 static_cg_height=4.1 [Views] eyepoint=-5.9, 0.1, 1.2 //(feet) longitudinal, lateral, vertical distance from reference datum [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 0 Com.1 = 1, 0 Nav.1 = 0, 0, 0 Adf.1 = 0 Transponder.1 = 1 Marker.1 = 0 [LIGHTS] light.0=4, -4.8,0.0,-0.6 , fx_vclitecub.fx [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_dustrun concrete=fx_sparksx touchdown=fx_tchdwn_s, 1 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator=100, 180 aileron=200, 1000 rudder=200, 3000 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type=4 direction_indicator.0=1,0 [fuel] Center1=3.000000,0.000000,0.000000,12.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=184.000000 wing_span=36.083333 wing_root_chord=4.916670 wing_tip_chord=4.916670 wing_dihedral=30.0 //Degrees wing_incidence=1.0 //Degrees wing_twist=1.0 //Degrees oswald_efficiency_factor=0.9 //Measure of lift effeciency of wing wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=-2.371000 wing_pos_apex_vert=0.000000 htail_area=39.000000 htail_span=11.666667 htail_pos_lon=-18.266667 htail_pos_vert=0.000000 htail_incidence=3.246460 htail_sweep=0.000000 vtail_area=15.8 //Square feet vtail_span=1.8 //Feet, tip to body vtail_pos_vert=-16.00000 elevator_area=16.610000 aileron_area=18.300000 rudder_area=23.20000 elevator_up_limit=28.000447 elevator_down_limit=20.998903 aileron_up_limit=19.996227 aileron_down_limit=15.000035 rudder_limit=33.995472 elevator_trim_limit=19.497754 spoiler_limit=45.000000 vtail_span=4.837355 vtail_sweep=0.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 P_factor_scaler=0.1 vtail_pos_lon=-12.183333 [Reference Speeds] flaps_up_stall_speed=24.0 cruise_speed=62.0 never_exceed_speed=125.0 full_flaps_stall_speed=19.200000 max_indicated_speed=180.000000 [GeneralEngineData] engine_type=0 Engine.0=1.400000,0.000000,-1.500000 fuel_flow_scalar=0.350000 min_throttle_limit=0.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 autoland_available=0 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [brakes] parking_brake = 0 //Parking brake available toe_brakes_scale = 0.35 //Brake scalar differential_braking_scale = 9.0 //Delta on the amount of brake when the rudder pedals deflected [Flaps.0] type=0 span-outboard=0.500000 extending-time=0.000000 system_type=0 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000
