[fltsim.0] title=300CBi sim=Helicopter model= panel= sound= texture= panel_alias=bell206b\panel sound_alias=bell206b\sound kb_checklists= kb_reference= prop_anim_ratio=-1.76 atc_id_color=0xc6eff7ff atc_id=NHELI atc_model= ui_manufacturer=Schweizer ui_type=300CBi ui_variation= description=Schweizer Aircraft developed the Model 300CBi specifically for the commercial helicopter training market. The Model 300CBi retains all of the superb flight handling, reliability, and safety characteristics of the Schweizer Model 300C, but for many operators, at the lowest life cycle cost of any current production helicopter.\n atc_heavy=0 atc_airline= atc_flight_number= [General] atc_type=Schweizer 300CBi performance=VNE(Kias) SeaLevel 94 knots 174 km\/hr\nCruise Speed 80 knots 148 km\/hr\nMax Endurance (32 gal) 3.0 hrs 3.0 hrs\nMax Endurance (64 gal) 6.1 hrs 6.1 hrs\nMax Range (32 gal) 220 mi 353 km\nMax Range (64 gal) 430 mi 691 km\nHover Ceiling IGE 7000ft 2133 m\nHover Ceiling OGE 4800ft 1463 m\n(Hover Ceiling displayed at 1600ibs\nHeight (overall) 8.72 ft 2.65 m\nlength [overall) 30.83 ft 9.40 m\nFuselage length 22.19 ft 6.76 m\nLanding gear tread width 6.54 ft 1.99 m\n\n\nWeight\nEmpty weight 1088 lbs 493.5 kg\nGross weight 1750 lbs 793.8 kg\nUseful load 662 lbs 300.0 kg\n\n\nPowerplant \nTextron Lycoming HIO-360-G1A Engine\nMaximum Take Off 180 shp 134 kw\nMaximum Continuous 180 shp 134 kw\n\nRotor System\nMain rotor diameter 26.83 ft 8.18 m\nMain rotor disk areas 565 sq ft 52.49 sq m\nMain rotor RPM 471\nTail rotor diameter 4.25 ft 1.30 m\n\nFuel\nStandard capacity 32 gal 192 lbs 87 kg\nAuxiliary Fuel 32 gal \n\n\n atc_model= [WEIGHT_AND_BALANCE] max_gross_weight=1750.000 empty_weight=1088.000 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 station_load.1=0, 0.0, 0.0, 0.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=6000.000 empty_weight_roll_MOI=4000.000 empty_weight_yaw_MOI=10000.000 empty_weight_coupled_MOI=0.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [turboprop_engine] power_scalar=1.0 [propeller] thrust_scalar=1.0 [Helicopter] low_realism_stability_scale=1.0, 1.0, 1.0 //Pitch , Bank, Yaw Scalars on Stability in Low Realism Settings [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, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 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=3.000, 4.700, 3.000, -4.200, 1574.800, 0.000, 0.519, 0.000, 0.287, 2.500, 0.605, 0.000, 0.000, 0.000, 0.000, 0.000 point.1=3.000, -1.800, -3.000, -4.280, 1574.800, 0.000, 0.519, 0.000, 0.396, 2.500, 0.728, 0.000, 0.000, 2.000, 0.000, 0.000 point.2=3.000, -1.800, 3.000, -4.280, 1574.800, 0.000, 0.519, 0.000, 0.396, 2.500, 0.728, 0.000, 0.000, 3.000, 0.000, 0.000 point.3=3.000, 4.700, -3.000, -4.200, 1574.800, 0.000, 0.519, 0.000, 0.287, 2.500, 0.605, 0.000, 0.000, 1.000, 0.000, 0.000 point.4=2.000, 0.000, -16.670, 9.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.5=2.000, 0.000, 16.670, 9.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.6=2.000, -20.500, 0.000, 1.670, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.7=2.000, 0.000, 9.080, 2.580, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=0.198 static_cg_height=4.000 [Views] eyepoint=0.5, 1.35, 2.15 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -0.00, -2.9, -2.55, fx_navred , light.1=3, -0.00, 2.9, -2.55, fx_navgre , light.2=3, -14.6, 0.00, 1.5, fx_navwhi , light.3=1, -6.7, 0.04, 1.05, fx_beacon , light.4=2, -6.5, 0.04, 1.1, fx_strobe , light.5=4, 3.0, 0.00, 1.3, fx_vclight , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks [fuel] Center1=0.000, 0.000, 0.000, 91.000, 0.000 fuel_type=2 number_of_tank_selectors=1 [GeneralEngineData] engine_type=3 Engine.0=8.300, 0.000, 0.400 fuel_flow_scalar=1.000 [Reference Speeds] flaps_up_stall_speed=0.0 //Knots True (KTAS) full_flaps_stall_speed=0.0 //Knots True (KTAS) cruise_speed=115.0 //Knots True (KTAS) [autopilot] autopilot_available=0 flight_director_available=0