[fltsim.0] title=Hughes 500D Teletica sim=hughes500 model= panel= sound= texture= kb_checklists= kb_reference= prop_anim_ratio=-1.76 atc_id_color=0xc6eff7ff atc_id=TI-TNT atc_model= ui_manufacturer=Hughes ui_type=500D ui_variation=Hughes500 Teletica description=The Hughes 500 is one of the world's most popular light turbine helicopters. It's rugged construction, operational performance and reliability combined with crisp handling and manoeuvrability make it the favourite of many helicopter pilots.\n\nSeveral different civilian and military versions have been built. Civilian versions include, amongst others, the 500C and 500D (1000 examples built since 1975), 500E (with longer fuselage, in production since 1982), 530E (new 485 kW engine built since 1983). atc_heavy=0 atc_airline= atc_flight_number= [General] atc_type= performance=Main Rotor Diameter: 8.1 m\nLength Overall: 7.5 m\nEmpty Weight: 675 kg\nMaximum Takeoff Weight: 1,350 kg \nNever Exceed Speed-VNE1: 152 kts\/281 kmh\nMaximum Cruise Speed: 134 kts\/248 kmh\nService Ceiling: 15,000 ft\nHover Ceiling-HIGE2: 8,500 ft\nHover Ceiling-HOGE3: 6,000 ft\nStandard Range: 261 nm\/302 km\nVertical Rate of Climb: 1,760 fpm \nPowerplant: 1 Allison 250-C20B \nMaximum Takeoff Power: 375 shp4 \n\nAuthor : Björn Büchner (March 2002)\n(bjornbuchner@hotmail.com) \n (bjornbuchner@hotmail.com) \n atc_model=H500 [WEIGHT_AND_BALANCE] max_gross_weight = 3000.000 empty_weight = 1500.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = 0.000, 0.000, 2.000 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, -2.930, -4.188, -4.491, 3000.000, 0.000, 0.519, 0.000, 0.150, 2.500, 0.728, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 3.000, -2.930, 4.188, -4.491, 3000.000, 0.000, 0.519, 0.000, 0.150, 2.500, 0.728, 0.000, 0.000, 0.000, 0.000, 0.000 static_pitch = 0.198 static_cg_height = 4.600 point.2= 3.000, 5.320, -4.188, -4.762, 3000.000, 0.000, 0.519, 0.000, 0.120, 2.500, 0.605, 0.000, 0.000, 0.000, 0.000, 0.000 point.3= 3.000, 5.320, 4.188, -4.762, 3000.000, 0.000, 0.519, 0.000, 0.120, 2.500, 0.605, 0.000, 0.000, 0.000, 0.000, 0.000 point.4= 2.000, -16.830, 0.254, -1.082, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000 point.5= 2.000, 13.200, 0.000, 4.950, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000 point.6= 2.000, 0.000, 13.200, 4.950, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000 point.7= 2.000, 0.000, -13.200, 4.950, 100.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000 [Views] eyepoint = 1.69, 1.23, 1.95 [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, 6.27, -4.23, -4.33, fx_navred , light.1 = 3, 6.27, 4.23, -4.33, fx_navgre , light.2 = 3, -18.45, 0.264, 6.27, fx_navwhi , light.3 = 1, 1.26, 0.00, -2.74, fx_beacon , light.4 = 2, -17.12, 0.264, 2.93, fx_beacon , light.5 = 4, 2.00, 0.00, 0.00, 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 //Fuel type: 1 = Avgas, 2 = JetA 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 = 134.0 //Knots True (KTAS) [autopilot] autopilot_available= 0 flight_director_available= 0