[fltsim.0] title=Ilyushin Il-18D White sim=il18 model= panel= sound= texture=template kb_checklists= kb_reference=notes atc_id=CU-T000 atc_id_color= atc_airline= atc_flight_number= ui_manufacturer=Ilyushin ui_type="Il-18D" ui_variation="White" atc_heavy=0 editable=0 description="El Il-18 es una aeronave de pasajeros de 4 motores turbohélice de medio-largo alcance. \nSu primer vuelo con motores NK4 fué el 4 de julio de 1957 y con motores AI-20, el 17 de septiembre de 1958. \nEste avión fué producido en serie por 12 años y alcanzó gran popularidad gracias a su capacidad para aumentar los asientos y su autonomía en cada una de las versiones que se sucedieron (A,B,V,D,E). \nEntre los años 1958-60 el Il-18 implantó 25 records mundiales incluyendo varios de alcance y altitud con diferentes payloads. \nPor sus méritos, en 1958, le fué otorgado el "Gran Premio" de la feria aerea de Bruselas y en 1979 fué develado un monumento, en el aeropuerto de Sheremetevo en su homenaje. \nCuba fué uno de los paises que más aeronaves de este tipo adquirió, Unión Soviética aparte, y desde sus inicios tuvieron un roll preponderante en el desarrollo aeronáutico de la isla." visual_damage=1 [fltsim.1] title=Ilyushin Il-18D Old Cubana sim=il18 model= panel= sound= texture=831 kb_checklists= kb_reference=notes atc_id=CU-T831 atc_id_color= atc_airline=Cubana de Aviación atc_flight_number= ui_manufacturer=Ilyushin ui_type="Il-18D" ui_variation="CU-T831" atc_heavy=0 editable=0 description="El Il-18 es una aeronave de pasajeros de 4 motores turbohélice de medio-largo alcance. \nSu primer vuelo con motores NK4 fué el 4 de julio de 1957 y con motores AI-20, el 17 de septiembre de 1958. \nEste avión fué producido en serie por 12 años y alcanzó gran popularidad gracias a su capacidad para aumentar los asientos y su autonomía en cada una de las versiones que se sucedieron (A,B,V,D,E). \nEntre los años 1958-60 el Il-18 implantó 25 records mundiales incluyendo varios de alcance y altitud con diferentes payloads. \nPor sus méritos, en 1958, le fué otorgado el "Gran Premio" de la feria aerea de Bruselas y en 1979 fué develado un monumento, en el aeropuerto de Sheremetevo en su homenaje. \nCuba fué uno de los paises que más aeronaves de este tipo adquirió, Unión Soviética aparte, y desde sus inicios tuvieron un roll preponderante en el desarrollo aeronáutico de la isla." visual_damage=1 [fltsim.2] title=Ilyushin Il-18D Classic Cubana sim=il18 model= panel= sound= texture=900 kb_checklists= kb_reference=notes atc_id=Cu-T900 atc_id_color= atc_airline=Cubana de Aviación atc_flight_number= ui_manufacturer=Ilyushin ui_type="Il-18D" ui_variation="CU-T900" atc_heavy=0 editable=0 description="El Il-18 es una aeronave de pasajeros de 4 motores turbohélice de medio-largo alcance. \nSu primer vuelo con motores NK4 fué el 4 de julio de 1957 y con motores AI-20, el 17 de septiembre de 1958. \nEste avión fué producido en serie por 12 años y alcanzó gran popularidad gracias a su capacidad para aumentar los asientos y su autonomía en cada una de las versiones que se sucedieron (A,B,V,D,E). \nEntre los años 1958-60 el Il-18 implantó 25 records mundiales incluyendo varios de alcance y altitud con diferentes payloads. \nPor sus méritos, en 1958, le fué otorgado el "Gran Premio" de la feria aerea de Bruselas y en 1979 fué develado un monumento, en el aeropuerto de Sheremetevo en su homenaje. \nCuba fué uno de los paises que más aeronaves de este tipo adquirió, Unión Soviética aparte, y desde sus inicios tuvieron un roll preponderante en el desarrollo aeronáutico de la isla." visual_damage=1 [fltsim.3] title=Ilyushin Il-18D AeroCaribbean sim=il18 model= panel= sound= texture=1517 kb_checklists= kb_reference=notes atc_id=Cu-T1517 atc_id_color= atc_airline=AeroCaribbean atc_flight_number= ui_manufacturer=Ilyushin ui_type="Il-18D" ui_variation="CU-T1517" atc_heavy=0 editable=0 description="El Il-18 es una aeronave de pasajeros de 4 motores turbohélice de medio-largo alcance. \nSu primer vuelo con motores NK4 fué el 4 de julio de 1957 y con motores AI-20, el 17 de septiembre de 1958. \nEste avión fué producido en serie por 12 años y alcanzó gran popularidad gracias a su capacidad para aumentar los asientos y su autonomía en cada una de las versiones que se sucedieron (A,B,V,D,E). \nEntre los años 1958-60 el Il-18 implantó 25 records mundiales incluyendo varios de alcance y altitud con diferentes payloads. \nPor sus méritos, en 1958, le fué otorgado el "Gran Premio" de la feria aerea de Bruselas y en 1979 fué develado un monumento, en el aeropuerto de Sheremetevo en su homenaje. \nCuba fué uno de los paises que más aeronaves de este tipo adquirió, Unión Soviética aparte, y desde sus inicios tuvieron un roll preponderante en el desarrollo aeronáutico de la isla." visual_damage=1 [General] atc_type=Ilyushin atc_model=Il-18 editable=0 performance=Velocidad máxima: \n675 km/h (True) \nVelocidad Crucero: \n650 km/h (True) \nMotores: \n4x Ivchenko AI-20M 3,169 kW (4,250 hp) \nAlcance con máxima carga de pago: \n4,300 km (2,322 nm, 2,650 mi) \nAlcance máximo: \n6,500 km (3,510 nm, 4,010 mi) \nTecho de vuelo: \n10,000 m (32,800 ft) \nCapacidad de combustible: \n23,700 L \nPeso vacio: \n35,000 kg (77,000 lb) \nMáximo peso de despegue: \n64,000 kg (140,800 lb) \nLargo: \n37.40 m (122 ft 8 in)\nEnvergadura: \n37.90 m (124 ft 4 in) \nAltura: \n10.17 m (33 ft 4 in) \nAsientos: \n100-120 \nSuperficie alar: \n140 m² (1,506.4 ft²) [WEIGHT_AND_BALANCE] max_gross_weight=140800 // (pounds) empty_weight=77660 // (pounds) reference_datum_position=0.0, 0.0, 0.0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_cg_position=0.0, 0.0, 0.0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) // Passenger load zone. Unit x 148,5 (67,5Kg America) ó 165 (75,0Kg Europa) station_load.0 = "0.0, 29.0, 0.0, 0.0, 1Pass (Max 3300)" station_load.1 = "0.0, -2.6, 0.0, 0.0, 2Pass (Max 11550)" station_load.2 = "0.0, -36.8, 0.0, 0.0, 3Pass (Max 2475)" // Cargo load zone. station_load.3 = "0.0, 17.6, 0.0,-5.0, 1Bagg (Max 4500)" station_load.4 = "0.0, 27.6, 0.0,-5.0, 2Bagg (Max 4500)" station_load.5 = "0.0, -21.1, 0.0,-5.0, 3Bagg (Max 4500)" station_load.6 = "0.0, -31.1, 0.0,-5.0, 4Bagg (Max 4500)" ;Moments of Inertia empty_weight_pitch_MOI=1427026 empty_weight_roll_MOI=1000000 //638556 empty_weight_yaw_MOI=1525867 empty_weight_coupled_MOI=0 [flight_tuning] cruise_lift_scalar=1.0 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 p_factor_on_yaw=0.01 torque_on_roll=0.01 gyro_precession_on_yaw=0.3 gyro_precession_on_pitch=0.3 [GeneralEngineData] engine_type=5 Engine.0=13.1, -29.9, -1.1 Engine.1=16.1, -14.3, -1.7 Engine.2=16.1, 14.3, -1.7 Engine.3=13.1, 29.9, -1.1 max_contrail_temperature = -45 min_throttle_limit=-0.01 fuel_flow_scalar=1.0 [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=14.76 //Propeller Diameter, (feet) propeller_blades=4 //Number of propeller blades propeller_moi=130 //Propeller moment of inertia beta_max=50.0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=8.0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=1700.0 //Miminum governed RPM prop_tc=0.004 //Prop time-constant gear_reduction_ratio=17.0 //Propeller gear reduction ratio fixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=600 //Minimum RPM for prop feathering beta_feather=93.3 //Feathering pitch angle (degrees) power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta=0.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=-12.0 //Minimum pitch angle in reverse, (degrees) [TurbineEngineData] fuel_flow_gain=0.001 //Gain on fuel flow inlet_area=1.0 //Square Feet, engine nacelle inlet area rated_N2_rpm=22800.0 //RPM, second stage compressor rated value static_thrust=1000.0 //Lbs, max rated static thrust at Sea Level [turboprop_engine] power_scalar=1.0 //Scalar on Turboprop power maximum_torque=13000.0 //Maximum torque available (ft-lbs) [electrical] ;BusType, MaxAmpLoad, MinVoltage ;BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) electric_always_available = 0 max_battery_voltage =24.0 generator_alternator_voltate =28.0 max_generator_alternator_amps =200.0 flap_motor = 0, 0 , 17.0 gear_motor = 0, 0 , 17.0 autopilot = 0, 0 , 17.0 avionics_bus = 0, 0 , 17.0 avionics = 1, 0 , 17.0 pitot_heat = 0, 0 , 17.0 additional_system = 0, 0 , 17.0 marker_beacon = 1, 0 , 17.0 gear_warning = 0, 0 , 17.0 fuel_pump = 0, 0 , 17.0 starter1 = 0, 0 , 17.0 starter2 = 0, 0 , 17.0 starter3 = 0, 0 , 17.0 starter4 = 0, 0 , 17.0 light_nav = 0, 0 , 17.0 light_beacon = 0, 0 , 17.0 light_strobe = 0, 0 , 17.0 light_landing = 0, 0 , 17.0 light_taxi = 0, 0 , 17.0 light_panel = 0, 0 , 17.0 prop_sync = 0, 0 , 17.0 auto_feather = 0, 0 , 17.0 auto_brakes = 0, 0 , 17.0 standby_vacuum = 0, 0 , 17.0 hydraulic_pump = 0, 0 , 17.0 fuel_transfer_pump = 0, 0 , 17.0 propeller_deice = 0, 0 , 17.0 directional_gyro = 0, 0 , 17.0 directional_gyro_slaving = 0, 0 , 17.0 //Engines smokes light_cabin = 0, 0 , 17.0 light_recognition = 0, 0 , 17.0 light_wing = 0, 0 , 17.0 light_logo = 0, 0 , 17.0 [contact_points] //0 Class <0=none,1=wheel, 2=scrape, 3=float> //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) point.0=1, 39.3, 0.0, -11.2, 1000, 0, 1.2, 50.0, 0.3, 3.0, 0.3, 9.0, 7.0, 0, 189.0, 194.0 point.1=1, -3.0, -14.5, -11.6, 1800, 1, 1.6, 0.0, 0.5, 1.5, 0.5, 15.0, 14.0, 1, 189.0, 194.0 point.2=1, -3.0, 14.5, -11.6, 1800, 2, 1.6, 0.0, 0.5, 1.5, 0.5, 14.0, 12.0, 2, 189.0, 194.0 // Hard countach point.3 = 4, -3.00, -14.00, -6.00, 1600, 0, 0.00, 0.0, 0.3, 2.5, 0.8, 0.0, 0.0, 7, 0.0, 0.0 point.4 = 4, -3.00, 14.00, -6.00, 1600, 0, 0.00, 0.0, 0.3, 2.5, 0.8, 0.0, 0.0, 7, 0.0, 0.0 point.5 = 4, 40.00, 0.00, -5.00, 1600, 0, 0.00, 0.0, 0.5, 2.5, 0.7, 0.0, 0.0, 7, 0.0, 0.0 point.6 = 4, -40.00, 0.00, -5.00, 1600, 0, 0.00, 0.0, 0.5, 2.5, 0.7, 0.0, 0.0, 7, 0.0, 0.0 // crash points point.7 =2, 0.00, -60.66, -0.50, 515, 0, 0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0 point.8 =2, 0.00, 60.66, -0.50, 515, 0, 0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0 point.9 =2, 50.00, 0.00, -3.00, 920, 0, 0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 point.10=2, -60.00, 0.00, 0.00, 920, 0, 0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0 static_pitch=0.0 static_cg_height=11.0 gear_system_type=0 //0-electric, 1-hidraulic [Views] eyepoint=42.1, -1.6, 1.6 [Flaps.0] type=1 system_type=1 span-outboard=0.6 extending-time=17 damaging-speed=173 blowout-speed=180 flaps-position.0=0 flaps-position.1=15 flaps-position.2=30 pitch_scalar=1.0 lift_scalar=1.0 drag_scalar=1.0 [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 [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, 1 Adf.1=1, 0 Adf.2=1, 0 Transponder.1=1 Marker.1=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 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=0 autothrottle_available=0 autothrottle_arming_required=1 autothrottle_max_rpm=93 autothrottle_takeoff_ga=0 pitch_takeoff_ga=9 use_no_default_bank=1 use_no_default_pitch=1 default_pitch_mode=0 default_bank_mode=0 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=20.0 max_bank_acceleration=1.8 max_bank_velocity=3.0 max_throttle_rate=0.1 nav_proportional_control=12.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=25.0 gs_integrator_control=0.53 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain=0.0 [exits] number_of_exits=1 exit_rate.0=0.3 [fuel] LeftTip= -1.6, -29.9, -2.4, 1981.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux= -1.6, -14.3, -3.2, 1981.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux= -1.6, 14.3, -3.2, 1981.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightTip= -1.6, 29.9, -2.4, 1981.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2.0 //Fuel type: 1=Avgas, 2=JetA number_of_tank_selectors=4 electric_pump=1 [airplane_geometry] wing_area=1603.0 //Square feet 1506.4 + wingbulb wing_span=124.4 //Feet wing_root_chord=18.2 //Feet wing_dihedral=3.0 //Degrees wing_incidence=6.0 //Degrees wing_twist=-3.0 //Degrees oswald_efficiency_factor=0.8 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=5.0 //Degrees, wing leading edge wing_pos_apex_lon=4.6 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=-3.7 //Feet, vertical distance from reference point, positive going up htail_area=302.7 //Square feet htail_span=38.9 //Feet htail_incidence=0.0 //Degrees htail_sweep=14.0 //Degrees, vertical tail leading edge htail_pos_lon=-54.6 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=1.0 /Feet, vertical distance from reference point, positive going up vtail_area=194.9 //Square feet vtail_span=22.4 //Feet, tip to body vtail_sweep=26.0 //Degrees, vertical tail leading edge vtail_pos_lon=-49.4 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up elevator_area=104 //Square feet aileron_area=100 //Square feet rudder_area=72 //Square feet elevator_up_limit=24.0 //Degrees elevator_down_limit=15.0 //Degrees aileron_up_limit=18.0 //Degrees aileron_down_limit=20.0 //Degrees rudder_limit=25.0 //Degrees elevator_trim_limit=20.0 //Degrees spoiler_limit=90.0 //Degrees spoilerons_available=0 //Spoilerons Available? aileron_to_spoileron_gain=0 //Aileron to spoileron gain min_ailerons_for_spoilerons=0 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed=100.0 //Knots True (KTAS) full_flaps_stall_speed=85.0 //Knots True (KTAS) cruise_speed=351.0 //Knots True (KTAS) max_indicated_speed=310.0 //Red Line (KIAS) max_mach=0.65 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, 0.42, -60.66, -0.50, fx_navredh , light.1=3, 0.42, 60.66, -0.50, fx_navgreh , light.2=3, -2.92, -60.66, -0.54, fx_navredm , light.3=3, -2.92, 60.66, -0.54, fx_navgrem , light.4=1,-59.77, 0.00, 22.12, fx_beaconh , light.5=1,-45.04, 0.00, -4.89, fx_beaconb , light.6=4, 40.00, 0.00, 3.00, fx_vclighth , light.7=5, -0.33, -59.80, -1.20, fx_landing , light.8=5, -0.33, 59.80, -1.20, fx_landing , light.9=6, 43.30, -3.93, -3.36, fx_landing , light.10=6, 43.30, 3.93, -3.36, fx_landing , light.11=3,-66.00, 0.00, 1.35, fx_navwhih , //Engines smokes light.12=7, -13.0, -29.9, -0.1, Ilyushin_smoke , light.13=8, -17.0, -14.3, -0.7, Ilyushin_smoke , light.14=9, -17.0, 14.3, -0.7, Ilyushin_smoke , light.15=10,-13.0, 29.9, -0.1, Ilyushin_smoke , [SMOKESYSTEM] smoke.0=0.0, 0.0, 0.0, fx_smoke_r [brakes] toe_brakes_scale=0.7 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.1 flap_limit_power=30.0 flap_limit_idle=15.0 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=3000.0 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=1,0 [pitot_static] vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI [TailHook] tailhook_length=1 ;(feet) tailhook_position=0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=0 [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.10,0.10 ;Percent per second
