[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
