[fltsim.0] title=Schweizer 300 utility sim=S300 model= panel=1 sound= texture= kb_checklists=S300_check kb_reference=S300_ref prop_anim_ratio=-1.76 visual_damage=1 atc_id_color=0xc6eff7ff atc_id=HC0001 atc_model= ui_manufacturer=Schweizer ui_type=300C Electrical Utility ui_variation=Hovercontrol description=The Schweizer 300 series of helicopters boast the lowest operating costs of any commercially oriented helicopter airframe. Making the line a favorite for small operators and training businesses worldwide. atc_flight_number= [fltsim.1] title=Schweizer 300 utility paint 1 sim=S300 model= panel=1 sound= texture=mba kb_checklists=S300_check kb_reference=S300_ref prop_anim_ratio=-1.76 visual_damage=1 atc_id_color=0xc6eff7ff atc_id=HC0001 atc_model= ui_manufacturer=Schweizer ui_type=300C Electrical Utility ui_variation=Munch Bros. description=The Schweizer 300 series of helicopters boast the lowest operating costs of any commercially oriented helicopter airframe. Making the line a favorite for small operators and training businesses worldwide. atc_flight_number= [General] atc_type=Schweizer 300 performance=Cruise Speed \t\n95 kts 110 mph 213 km\/h\n\nEngine\nAllison 250-C20J 420 shp\n\nMaximum Range\n435 nm \t 500 m 805 km\n\nService Ceiling\n20,000 ft 6,096 m\n\nHovering Ceiling\n19,600 5,974 m\n\nFuel Capacity\n91 U.S. gal 344 L\n\nEmpty Weight\n1,640 lb 744 kg\n\nMaximum Gross Weight\n3,200 lb 1,451 kg\n\nMaximum Gross Weight (External Loading)\n3,350 lb 1,519 kg\n\nLength\t\n31.2 ft\t 9.51 m\n\nRotor Span\n33.3 ft\t 10.15 m\n\nHeight\n11.7 ft\t 3.51 m\n\nSeating \t\nUp to 5 \n\nUseful Load\t\n1,498 lb\t 679 kg\n editable=0 [WEIGHT_AND_BALANCE] max_gross_weight = 1370 // (pounds) empty_weight = 862.4 // (pounds) reference_datum_position = 8.33, 0.0, 0.0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -8.37, 0.0, 0.0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = "160, -6.6, 0.89, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "160, -6.6, -0.78, 0.0, Passenger" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 6000 empty_weight_roll_MOI = 4000 empty_weight_yaw_MOI = 10000 empty_weight_coupled_MOI = 0 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor = 0, 5 , 17.0 gear_motor = 0, 5 , 17.0 autopilot = 0, 5 , 17.0 avionics_bus = 0, 5 , 17.0 avionics = 1, 5 , 17.0 pitot_heat = 0, 2 , 17.0 additional_system = 0, 2 , 17.0 marker_beacon = 1, 2 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 17.0 starter1 = 0, 20, 17.0 light_nav = 0, 5 , 17.0 light_beacon = 0, 5 , 17.0 light_landing = 0, 5 , 17.0 light_taxi = 0, 5 , 17.0 light_strobe = 0, 5 , 17.0 light_panel = 0, 5 , 17.0 //0 Class <0=none,1=wheel, 2=scrape, 3=skid> //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) [contact_points] point.0=3, -2.52, 3.33, -5.08, 1574.8, 0, 0.5187, 0.0, 0.286975, 2.5, 0.605067, 0.0, 0.0, 0.0, 0.0, 0.0 point.1=3, -11.85, -3.33, -5.16, 1574.8, 0, 0.5187, 0.0, 0.396299, 2.5, 0.728164, 0.0, 0.0, 2.0, 0.0, 0.0 point.2=3, -11.85, 3.33, -5.16, 1574.8, 0, 0.5187, 0.0, 0.396299, 2.5, 0.728164, 0.0, 0.0, 3.0, 0.0, 0.0 point.3=3, -2.52, -3.33, -5.08, 1574.8, 0, 0.5187, 0.0, 0.286975, 2.5, 0.605067, 0.0, 0.0, 1.0, 0.0, 0.0 point.4=2, -8.35, -16.67, 9.00, 0.0, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 5.0, 0.0, 0.0 point.5=2, -8.35, 16.67, 9.00, 0.0, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 6.0, 0.0, 0.0 point.6=2, -28.85, 0.00, -1.0, 787.4, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 9.0, 0.0, 0.0 point.7=2, -8.35, 9.08, 2.58, 787.4, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 4.0, 0.0, 0.0 point.8=4.000, -3.03, 4.188, -3.580, 1600.000, 0.000, 0.000, 0.000, 0.200, 2.500, 0.800, 0.000, 0.000, 0.000, 0.000, 0.000 point.9=4.000, -3.03, -4.188, -3.580, 1600.000, 0.000, 0.000, 0.000, 0.200, 2.500, 0.800, 0.000, 0.000, 0.000, 0.000, 0.000 point.10=4.000, -13.3500, 4.188, -3.320, 1600.000, 0.000, 0.000, 0.000, 0.200, 2.500, 0.800, 0.000, 0.000, 0.000, 0.000, 0.000 point.11=4.000, -13.3500, -4.188, -3.320, 1600.000, 0.000, 0.000, 0.000, 0.200, 2.500, 0.800, 0.000, 0.000, 0.000, 0.000, 0.000 static_pitch = 0.2 static_cg_height = 3.58 [brakes] parking_brake = 0 //Parking brake available toe_brakes_scale = 0.0 //Brake scalar [hydraulic_system] normal_pressure = 0.0 //PSI [Views] eyepoint=-6.95, -1.1, 2.2 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -15.85, 0.00, 1.40, fx_navred , light.1=3, -5.65, -0.90, -2.67, fx_navwhi , light.2=1, -15.85, 0.00, 1.40, fx_beacon , light.3=4, -5.35, 0.00, 3.00, fx_vclight , [SMOKESYSTEM] //?,long,lat from ref datum smoke.0=-20.35, -6.00, 6.0, fx_smoke_w smoke.1=-20.35, -6.00, -6.0, fx_smoke_w smoke.2=-20.35, -6.00, 12.0, fx_smoke_w smoke.3=-20.35, -6.00, -12.0, fx_smoke_w [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 1 Com.2 = 1, 1 Nav.1 = 1, 1, 1 Nav.2 = 1, 1, 0 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 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. //NOTE: These map to cyclic (fore/aft), cyclic (left/right), and anti-torque elevator = 100, 180 aileron = 200, 1000 rudder = 200, 1000 [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=3,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks startup=fx_engstrt [fuel] LeftMain = -8.85, -0.5, 0.0, 32.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -8.85, 0.5, 0.0, 32.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=0 [GeneralEngineData] engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = -8.5, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar= 1.0 //Fuel flow scalar min_throttle_limit = 0.0; //Minimum percent throttle. Generally negative for turbine reverser [piston_engine] power_scalar = 1.0 //Piston power scalar cylinder_displacement= 90.0 //Cubic inches per cylinder compression_ratio= 8.5 //Compression ratio number_of_cylinders=4 //Number of cylinders max_rated_rpm= 2700 //Max rated RPM max_rated_hp= 180 //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= 1.0 //Scalar on idle RPM friction [Reference Speeds] cruise_speed = 90.0 //Knots True (KTAS) max_indicated_speed = 102 //Red line (KIAS) [autopilot] autopilot_available= 0 flight_director_available= 0 [yaw_string] yaw_string_available=1 [Helicopter] reference_length = 21.58 reference_frontal_area = 17.7 reference_side_area = 44.5 side_aero_center = -12.5 right_trim_scalar = 1.0 correlator_available = 1 governed_pct_rpm_ref = 1.04 governor_pid = 0.4, 0, 0.1, 0, 0.2 rotor_brake_scalar = 1.0 torque_scalar = 1.0 //cyclic_roll_control_scalar =1.0 //cyclic_pitch_control_scalar =1.0 //pedal_control_scalar =1.0 cyclic_roll_control_scalar =1.5 cyclic_pitch_control_scalar =1.5 pedal_control_scalar =1.0 collective_on_rotor_torque_scalar = 1.0 [fuselage_aerodynamics] drag_force_cf = 0.55 side_drag_force_cf = 10.0 pitch_damp_cf = -2.0 roll_damp_cf = -2.0 yaw_damp_cf = -0.1 yaw_stability_cf = 0.27 [MainRotor] Position = -8.5, 0, 4.91 //Longitudinal, Lateral, Vertical feet from datum Radius = 12.583 //feet max_disc_angle = 5.0 RatedRpm = 510 Number_of_blades = 2 Weight_per_blade = 26.0 Weight_to_moi_factor = 0.58 inflow_vel_reference = 34.0 [SecondaryRotor] Position = -22.8, -0.74, 1.8 //Longitudinal, Lateral, Vertical feet from datum TailRotor = 1 Radius = 1.75 //feet [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=1.5