[fltsim.0] title=IL-62M Cubana sim=IL62M model= panel=747 sound=737 texture= kb_checklists=IL62M_check kb_reference=IL62M_ref atc_id=CU-T1282 atc_airline=Cubana de Aviación atc_flight_number=1123 atc_heavy=0 ui_manufacturer=Ilyushin ui_type=IL-62M ui_variation=CU-T1284 description="EL Ilyushin IL-62M fué el más exitoso de los modelos derivados del IL-62 original diseñado para realizar vuelos intercontinetales sin escalas, pero el prototipo no pudo contar con los motores en planes y tuvo que hacer sus primeros vuelos con motores "Lyulka AL7" (75.0kN). Esta potencia era insuficiente para alcanzar el desempeño planificado pero sirvió como banco de pruebas volando por primera vez en Septiembre de 1962. \nSu primer vuelo comercial fué en Marzo de 1967 ya con motores Kuznetsov NK84 (103.0kN) y su primer vuelo intercontinental en Septiembre del mismo año (Moscú-Motreal). \nEn 1971, en la feria aérea de París se presentó el IL-62M con sus motores definitivos, Soloviev D30KU (107.9kN), que entró en servicio en 1974. \nLa producción del IL-62 cesó en 1994, tras la caida del campo socialista, aunque todavía quedan algunos aparatos en servicio. \nRuidoso y consumidor el IL-62M pasará a la historia como uno de los primeros y exitosos jets intercontinentales." visual_damage=1 [General] atc_type=Ilyushin atc_model=IL62 editable=0 performance=Velocidad crucero: \n0.80 Mach ~ 850 kph \nMotores: \nCuatro 107.9kN (24,250lb) Soloviev D30KU turbofans \nAutonomía: \n9,200km + 1h (10,000kg) / 6,700km + 1h (23,000) \nMáxima altitud operativa permitida: \n13000m \nCapacidad de combustible: \n1053000 l (x 0.825 kg/litro) ~ 86870 kg \nPeso Vacío: \n74500kg\nLargo: \n53.1 m / 174ft 3in \nEnvergadura: \n43.2 m / 141ft 9in\nAlto \n43.3 m / 142ft 9in\nConfiguración típica de dos clases: \n186 pax \nCarga util: \n23,000 kg visual_damage=1 [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI [WEIGHT_AND_BALANCE] max_gross_weight=372960 // (pounds) ~ 168000 kg empty_weight=162060 // (pounds) ~ 73000 kg reference_datum_position=0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=20 // Max. Payload 23t () // People station_load.0="0.0, 60.0, 0.0, 2.0, OA (Max 3696)" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) *** Passenger Unit x 148,5(67,5Kg America) ó 165(75,0Kg Europa) station_load.1="0.0, 43.0, 0.0, 2.0, OB (Max 4620)" station_load.2="0.0, 13.0, 0.0, 2.0, OC (Max 4620)" station_load.3="0.0, 0.0, 0.0, 2.0, OD (Max 5544)" station_load.4="0.0, -16.0, 0.0, 2.0, OE (Max 5544)" station_load.5="0.0, -36.0, 0.0, 2.0, WR (Max 616)" // Cargo station_load.6 ="0.0, 79.7, 0.0, -2.0, WB (Max 2000)" station_load.7 ="0.0, 43.3, 0.0, -2.0, C1 (Max 13640)" station_load.8 ="0.0, 43.3, 0.0, -2.0, C2 (Max 7260)" station_load.9 ="0.0, -19.3, 0.0, -2.0, C3 (Max 4400)" station_load.10="0.0, -33.9, 0.0, -2.0, C4 (Max 2948)" station_load.11="0.0, -54.0, 0.0, 0.0, C6 (Max 2948)" ;Moments of Inertia empty_weight_pitch_MOI=7000000 //Según fórmula: 6036656 empty_weight_roll_MOI=6000000 //Según fórmula: 1727840 empty_weight_yaw_MOI=6000000 //Según fórmula: 5215978 empty_weight_coupled_MOI=0.0 [contact_points] max_number_of_points=12 //0 Class <0=none,1=wheel, 2=scrape, 3=float, 4=?, 5=water_rudder> //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) //WHEELS point.0=1, 71.9, 0.0, -11.8, 600.0, 0, 1.5, 50.0, 0.3, 4.5, 0.6, 10.0, 11.0, 0, 0, 297 point.1=1, -4.3, -12.6, -12.0, 1200.0, 1, 2.6, 0.00, 0.6, 2.5, 0.9, 14.0, 15.0, 2, 0, 297 point.2=1, -4.3, 12.6, -12.0, 1200.0, 2, 2.6, 0.00, 0.6, 2.5, 0.9, 14.0, 15.0, 3, 0, 297 //SCRAPES point.3=2, -29.0, -71.0, 0.37, 500.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 0, 0 point.4=2, -29.0, 71.0, 0.37, 500.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 6, 0, 0 point.5=2, 80.2, 0.0, -4.3, 500.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 9, 0, 0 point.6=2, -31.0, 0.0, -4.3, 500.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 //TAILWHEEL point.7=5, -42.4, 0.0, -12.6, 120, 0, 0.00, 0.0, 0.0, 0.0, 1.0, 12, 12, 0, 0.0, 13.4 static_pitch=0.0 static_cg_height=12.0 gear_system_type=1 [Views] eyepoint=80.0, -1.6, 3.7 ; Longitude, Latitude and Vertical position from Reference Point, (feet) [fuel] Center1=12.0, 0.0, -1.5, 5554.2, 4.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain=6.2, -12.0, -1.5, 4876.8, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=6.2, 12.0, -1.0, 4876.8, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux=-5.5, -20.0, -1.0, 4876.8, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux=-5.5, 20.0, -1.0, 4876.8, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Righttip=-19.0, -27.0, 0.5, 1056.4, 1.0 Lefttip=-19.0, 27.0, 0.5, 1056.4, 1.0 Center2=-51.4, 0.0, 13.3, 1354.7, 1.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=4 electric_pump=1 [Reference Speeds] flaps_up_stall_speed=135 //Knots True (KTAS) full_flaps_stall_speed=110 //Knots True (KTAS) cruise_speed=380 //Knots True (KTAS) max_indicated_speed=329 //Knots True (KIAS) max_mach=0.83 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.5 // 0.0 .. 1.0 extending-time=20 // seconds flaps-position.0=0 // degrees flaps-position.1=15 // degrees flaps-position.2=30 // degrees damaging-speed=174 // KIAS blowout-speed=194 // KIAS lift_scalar=1.0 drag_scalar=1.0 pitch_scalar=0.0 system_type=1 //Hydraulic [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [GeneralEngineData] engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-47.0, -16.1, 2.8 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-47.0, -9.9, 2.8 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.2=-47.0, 9.9, 2.8 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.3=-47.0, 16.1, 2.8 //(feet) longitudinal, lateral, vertical distance from reference datum min_throttle_limit=-0.30 //Minimum percent throttle. Generally negative for turbine reverser max_contrail_temperature=-30 //Temperature (deg C) below which contrails may appear fuel_flow_scalar=1.2 //Scalar for fuel flow efficiency [TurbineEngineData] fuel_flow_gain=0.002 //Gain on fuel flow inlet_area=11.0 //Square Feet, engine nacelle inlet area (11) rated_N2_rpm=15800 //RPM, second stage compressor rated value (15.8 real) static_thrust=24200 //Lbs, max rated static thrust at Sea Level (24200 teorico) afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar = 0.8 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 40.0 flap_motor=0, 5 , 0.0 gear_motor=0, 5 , 0.0 autopilot=0, 5 , 0.0 avionics_bus=0, 5, 0.0 avionics=1, 5 , 0.0 pitot_heat=0, 2 , 0.0 additional_system=0, 2, 0.0 marker_beacon=1, 2 , 0.0 gear_warning=0, 2 , 0.0 fuel_pump=0, 5 , 0.0 starter1=0, 20, 0.0 light_nav=0, 5 , 0.0 light_beacon=0, 5 , 0.0 light_landing=0, 5 , 0.0 light_taxi=0, 5 , 0.0 light_strobe=0, 5 , 0.0 light_panel=0, 5 , 0.0 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Adf.2=1 Transponder.1=1 Marker.1=1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -25.90, -70.90, 0.00, fx_navwhih light.1=3, -25.90, 70.90, 0.00, fx_navwhih light.2=8, -68.88, 0.00, 5.15, fx_navwhih light.3=8, -29.74, -70.23, -0.36, fx_navwhih light.4=8, -29.74, 70.23, -0.36, fx_navwhih light.5=1, -68.93, 0.00, 29.13, fx_beaconb light.6=1, 28.10, 0.00, -4.9, fx_beaconb light.7=4, 84.20, 0.00, 4.0, fx_vclighth light.8=6, 85.00, -4.00, -2.00, fx_landing light.9=6, 85.00, 3.10, -3.20, fx_landing light.10=5, -3.30, -39.65, -1.65, fx_landing light.11=5, -3.30, 39.65, -1.65, fx_landing light.12=5, 77.10, -0.40, -6.4, fx_landing light.13=5, 77.10, 0.40, -6.4, fx_landing light.14=3, -26.70, -71.30, 0.00, fx_navredh light.15=3, -26.70, 71.30, 0.00, fx_navgreh [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=150, 250 aileron=150, 250 rudder=150, 250 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [SMOKESYSTEM] Smoke.0=0.0, -47.0, -16.7, ILYUSHIN_SMOKE // vertical (no funciona), longitudinal, lateral, efecto Smoke.1=0.0, -47.0, -10.6, ILYUSHIN_SMOKE Smoke.2=0.0, -47.0, 10.6, ILYUSHIN_SMOKE Smoke.3=0.0, -47.0, 16.7, ILYUSHIN_SMOKE [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [brakes] parking_brake=1 //Parking brake available toe_brakes_scale=0.6 //Brake scalar [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] normal_pressure=3000.0 //PSI electric_pumps=0 //no electric pumps engine_map=1,1,1,1 //pumps on Eng1,2,3,4 [stall_warning] type=1 [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=1,0 [airplane_geometry] wing_area=3009.0 //Square feet wing_span=141.2 // Feet wing_root_chord=33.0 //Feet wing_dihedral=3.0 //Degrees wing_incidence=4.0 //Degrees wing_twist=-4.0 //Degrees oswald_efficiency_factor=0.7 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=35.0 //Degrees, wing leading edge wing_pos_apex_lon=26.6 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=-1.5 //Feet, vertical distance from reference point, positive going up htail_area=480 //Square feet htail_span=40.8 //Feet htail_pos_lon=-59.5 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=26.6 //Feet, vertical distance from reference point, positive going up htail_incidence=0.0 //Degrees htail_sweep=40.0 //Degrees, horizontal tail leading edge vtail_area=361 //Square feet vtail_span=18.3 //Feet, tip to body vtail_sweep=42.0 //Degrees, vertical tail leading edge vtail_pos_lon=-48.7 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=8.1 //Feet, vertical distance from reference point, positive going up elevator_area=190 //Square feet aileron_area=156 //Square feet rudder_area=144 //Square feet elevator_up_limit=26 //Degrees elevator_down_limit=14 //Degrees aileron_up_limit=27 //Degrees aileron_down_limit=15 //Degrees rudder_limit=30.0 //Degrees elevator_trim_limit=20 //Degrees spoiler_limit=60 //Degrees spoilerons_available=1 //Spoilerons Available? aileron_to_spoileron_gain=3 //Aileron to spoileron gain min_ailerons_for_spoilerons=5 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=0 autothrottle_max_rpm=97.000000 pitch_takeoff_ga=8.000000 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=20.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=16.000000 nav_integrator_control=0.170000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=18.0000 gs_integrator_control=0.330000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=1.000000 [TailHook] tailhook_length=0 ;(feet) tailhook_position=0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=0 [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 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
