[fltsim.0] title=Balkan IL-18V sim=Il18d model= panel= sound= texture= kb_checklists= kb_reference= atc_id=LZ-BEU atc_airline= atc_flight_number= ui_manufacturer=Ilyushin ui_type=IL-18V ui_variation=Balkan (90s) editable=0 description=Long range passenger aircraft, first flight July 4, 1957 \n\nFS2002 only \n\nApr.8.2002 atc_heavy=0 [General] atc_type=Ilyushin atc_model=Il-18 editable=0 performance=Cruise Speed\n625km/h \n\nEngines\n4 Ivchenko AI-20M \n\nMaximum Range\n7'100km \n\nService Ceiling\n9,000 m \n\nFuel Capacity\n23,700 L \n\nEmpty Weight-Standard\n33,760 kg \n\nMaximum Takeoff Weight\n64,000kg \n\nLength\n35.9m \n\nWingspan\n37.42 m \n\nHeight\n10.17m \n\nSeating\nSeats 100 to 120 [pitot_static] vertical_speed_time_constant=10 //Increasing this value will cause a more instantaneous reaction in the VSI [WEIGHT_AND_BALANCE] max_gross_weight=142200 // (pounds) empty_weight=88900 // (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 station_load.0=0.000000,0.000000,0.000000,0.000000 ;Moments of Inertia empty_weight_pitch_MOI=1636600 empty_weight_roll_MOI=1659435 empty_weight_yaw_MOI=231380 empty_weight_coupled_MOI=0 [flight_tuning] cruise_lift_scalar=1.6 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 [GeneralEngineData] engine_type=5 Engine.0=13.5, -30.5, 2.8 Engine.1=16.2, -14.1, 2.1 Engine.2=16.2, 14.1, 2.1 Engine.3=13.5, 30.5, 2.8 fuel_flow_scalar=0.700 [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=75 //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=700.0 //Miminum governed RPM prop_tc=0.004 //Prop time-constant gear_reduction_ratio=12.100 //Propeller gear reduction ratio fixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit=180.000 //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=500 //Minimum RPM for prop feathering beta_feather=93.320 //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=1.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=-14.0 //Minimum pitch angle in reverse, (degrees) [TurbineEngineData] fuel_flow_gain=0.015 inlet_area=3.5 rated_N2_rpm=22400.0 static_thrust=1150.0 [turboprop_engine] power_scalar=1.3 maximum_torque=13600.0 [electrical] ;BusType, MaxAmpLoad, MinVoltage ;BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) max_battery_voltage=24.0 generator_alternator_voltate=28.0 max_generator_alternator_amps=200.0 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, 15, 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 starter2=0, 20, 17.0 light_nav=0, 0 , 10.0 light_beacon=0, 5 , 10.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 10.0 light_panel=0, 5 , 10.0 [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, 47.5, 0.000, -8.60, 1200, 0, 1.0, 55.0, 0.21, 1.0, 1.5, 9.0, 7.0, 0, 189.0, 194.0 point.1=1, -1.3, -15.445, -9.44, 1900, 1, 1.6, 0.0, 1.00, 1.0, 0.1, 15.0, 14.0, 2, 189.0, 194.0 point.2=1, -1.3, 15.445, -9.44, 1900, 2, 1.6, 0.0, 1.00, 1.0, 0.1, 14.0, 12.0, 3, 189.0, 194.0 point.3=2, -1.35, -61.80, 2.8, 415, 0, 0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -1.35, 61.80, 2.8, 415, 0, 0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -53.20, 0.00, -0.5, 820, 0, 0.0, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 40.15, 0.00, -2.6, 680, 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=8.54 [Views] eyepoint=42.8, -1.7, 5.4 [Flaps.0] type=1 span-outboard=0.57 extending-time=17 system_type=1 damaging-speed=173 blowout-speed=179 lift_scalar=1.9 drag_scalar=1.2 pitch_scalar=1.0 flaps-position.0=0 flaps-position.1=15 flaps-position.2=30 [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, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1, 1 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=1900 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=93 autothrottle_takeoff_ga=1 pitch_takeoff_ga=9 use_no_default_bank=1 use_no_default_pitch=1 [exits] number_of_exits=3 exit_rate.0=0.3 exit_rate.0=0.4 exit_rate.1=0.7 [fuel] LeftMain=0.0, -20.6, 0.0, 1100.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux=0.0, -30.0, 0.0, 1100.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=0.0, 20.6, 0.0, 1100.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux=0.0, 30.0, 0.0, 1100.0, 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=2 [airplane_geometry] wing_area=1502.2 //Square feet wing_span=122.73 //Feet wing_root_chord=17.166 //Feet wing_dihedral=4.500 //Degrees wing_incidence=0.999756 //Degrees wing_twist=-1.499634 //Degrees oswald_efficiency_factor=0.99 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=0.0 //Degrees, wing leading edge wing_pos_apex_lon=0.0 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_area=67.0 //Square feet htail_span=17.17 //Feet htail_pos_lon=-24.6 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=0.0 /Feet, vertical distance from reference point, positive going up htail_incidence=0.5 //Degrees htail_sweep=0.0 //Degrees, vertical tail leading edge vtail_area=42.0 //Square feet vtail_span=7.4 //Feet, tip to body vtail_sweep=0.0 //Degrees, vertical tail leading edge vtail_pos_lon=-52.3 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=22.3 //Feet, vertical distance from reference point, positive going up elevator_area=75.0 //Square feet aileron_area=58.0 //Square feet rudder_area=370.0 //Square feet elevator_up_limit=20.0 //Degrees elevator_down_limit=17.5 //Degrees aileron_up_limit=18.0 //Degrees aileron_down_limit=18.0 //Degrees rudder_limit=30.0 //Degrees elevator_trim_limit=25.0 //Degrees spoiler_limit=50.0 //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=83.8 //Knots True (KTAS) cruise_speed=351.0 //Knots True (KTAS) [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, 0.50, -61.90, 2.90, fx_navredh , light.1=3, 0.50, 61.90, 2.90, fx_navgreh , light.2=3, -3.00, -61.90, 2.70, fx_navredm , light.3=3, -3.00, 61.90, 2.70, fx_navgrem , light.4=1, -59.7, 0.00, 26.55, fx_beaconh , light.5=1, -45.4, 0.00, -2.10, fx_beaconb , light.6=4, 43.0, 0.00, 5.20, fx_vclighth , light.7=4, 21.0, -1.10, 7.00, fx_vclighth , light.8=4, -27.0, -1.10, 7.00, fx_vclighth , [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds 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=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 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
