[fltsim.0] title=Virgin ilyushin -il-96 sim=il96 model= panel= sound= texture= panel_alias = sound_alias = kb_checklists= kb_reference= atc_id=N700MS atc_airline=virgin atc_flight_number=0001 atc_heavy=1 ui_manufacturer=Ilyushin ui_type=Ilyushin Il-96-300 ui_variation=Virgin Atlantic description=Enter your description here. [General] atc_type= atc_model= editable=1 performance=Enter your performance information here. [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 = 476000.000 empty_weight = 258000.000 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 = 28000.000, 0.000, 0.000, 0.000 ;Moments of Inertia empty_weight_roll_MOI = 11200000.000 empty_weight_pitch_MOI = 88000000.000 empty_weight_yaw_MOI = 37000000.000 empty_weight_coupled_MOI = 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] Center1 = 0.000, 0.000, -2.000, 32600.000, 3.000 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 [airplane_geometry] wing_area = 3400.000 wing_span = 190.000 wing_root_chord = 35.000 wing_dihedral = 7.000 wing_incidence = 2.000 wing_twist = -1.000 oswald_efficiency_factor= 0.700 wing_winglets_flag = 1 wing_sweep = 40.000 wing_pos_apex_lon = 12.000 wing_pos_apex_vert = 0.000 htail_area = 600.000 htail_span = 66.000 htail_pos_lon = -70.000 htail_pos_vert = 8.000 htail_incidence = 0.000 htail_sweep = 40.000 vtail_area = 560.000 vtail_span = 28.000 vtail_sweep = 45.000 vtail_pos_lon = -65.000 vtail_pos_vert = 15.000 elevator_area = 190.000 aileron_area = 100.000 rudder_area = 133.000 elevator_up_limit = 25.000 elevator_down_limit = 15.000 aileron_up_limit = 25.000 aileron_down_limit = 15.000 rudder_limit = 31.500 elevator_trim_limit = 20.000 spoiler_limit = 45.000 spoilerons_available = 1 aileron_to_spoileron_gain = 3.000 min_ailerons_for_spoilerons = 10.000 min_flaps_for_spoilerons = 0.000 [Reference Speeds] flaps_up_stall_speed = 140.000 full_flaps_stall_speed = 112.000 cruise_speed = 505.000 [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =1.000 induced_drag_scalar =1.000 elevator_effectiveness =1.000 aileron_effectiveness =1.000 rudder_effectiveness =1.000 pitch_stability =1.000 roll_stability =1.000 yaw_stability =1.000 elevator_trim_effectiveness =1.000 aileron_trim_effectiveness =1.000 rudder_trim_effectiveness =1.000 [GeneralEngineData] engine_type = 1 Engine.0 = -10.000, -57.000, -4.000 Engine.1 = 3.000, -34.000, -6.000 Engine.2 = 3.000, 34.000, -6.000 Engine.3 = -10.000, 57.000, -4.000 fuel_flow_scalar = 1.000 [TurbineEngineData] fuel_flow_gain = 0.002 inlet_area = 30.000 rated_N2_rpm = 29920.000 static_thrust = 35275.000 afterburner_available = 0 reverser_available = 1 [jet_engine] thrust_scalar =1.000 [autopilot] autopilot_available = 1 flight_director_available = 1 default_vertical_speed = 1800.0 autothrottle_available = 1 autothrottle_arming_required = 1 autothrottle_max_rpm = 90 autothrottle_takeoff_ga = 1 pitch_takeoff_ga = 8; [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 = 1.000, 45.000, 0.000, -12.000, 1000.000, 0.000, 2.000, 70.000, 0.500, 3.500, 0.900, 6.000, 6.000, 0.000, 0.000, 0.000 point.1 = 1.000, -12.500, -16.000, -14.500, 2000.000, 1.000, 2.000, 0.000, 3.000, 2.500, 0.900, 5.000, 5.000, 2.000, 0.000, 0.000 point.2 = 1.000, -12.500, 16.000, -14.500, 2000.000, 2.000, 2.000, 0.000, 3.000, 2.500, 0.900, 5.000, 5.000, 3.000, 0.000, 0.000 point.3 = 2.000, -46.000, -95.000, 7.000, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4 = 2.000, -46.000, 95.000, 7.000, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5 = 2.000, -80.000, 0.000, 0.000, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6 = 2.000, 65.000, 0.000, 0.000, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch = 0.000 static_cg_height = 12.000 [Views] eyepoint = -19.4, -1.97, 9.27 ; Longitude, Latitude and Vertical position from Reference Point, (FEET) [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot = 0, 5 , 17.0 avionics_bus = 0, 10, 17.0 avionics = 1, 5 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 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 [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 Transponder.1 = 1 Marker.1 = 1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -38.92, -94.07, 6.83, fx_navredh , light.1 = 3, -38.92, 94.07, 6.83, fx_navgreh , light.2 = 3, -94.80, 0.00, 11.42, fx_navwhih , light.3 = 2, -39.32, -94.20, 6.83, fx_strobeh , light.4 = 2, -39.32, 94.20, 6.83, fx_strobeh , light.5 = 1, 29.71, 0.00, 13.73, fx_beaconh , light.6 = 1, 2.78, 0.00, -6.83, fx_beaconb , light.7 = 4, 61.56, 0.00, 8.48, fx_vclighth, [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 [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 [exits] number_of_exits = 3 exit_rate.0 = 1.0 ;Percent per second exit_rate.1 = 1.0 ;Percent per second exit_rate.2 = 1.0 ;Percent per second [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 [Flaps.0] type= 1 span-outboard= 0.900 extending-time= 7.000 system_type= 1 damaging-speed= 200.000 blowout-speed= 250.000 lift_scalar= 0.700 drag_scalar= 0.900 pitch_scalar= 0.900 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000 flaps-position.2= 5.000, 0.000 flaps-position.3= 10.000, 0.000 flaps-position.4= 20.000, 0.000 flaps-position.5= 25.000, 0.000 flaps-position.6= 30.000, 0.000 [Flaps.1] type= 2 span-outboard= 0.900 extending-time= 3.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 0.300 drag_scalar= 0.100 pitch_scalar= 0.100 flaps-position.0= 0.000, 0.000 flaps-position.1= 1.000, 0.000