[fltsim.0] title=Airbus A380-800 White livery sim=A388 model=flex panel= sound= texture= checklists= description=Airbus A380-800 ui_manufacturer=Airbus ui_type=A380-800 ui_variation=White atc_heavy=1 atc_id=F-WXXL atc_type=Airbus atc_model=A380-800 atc_airline=Airbus atc_flight_number=380 [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=50 station_load.0=115500.000000,0.000000,0.000000,0.000000 // 550 pax @ 210lb each empty_weight=611729.000000 empty_weight_roll_MOI=21059579.000000 empty_weight_pitch_MOI=43557241.000000 empty_weight_yaw_MOI=40526900.000000 empty_weight_coupled_MOI=1300.000000 max_gross_weight=1234998.000000 [jet_engine] thrust_scalar=1.000 [flight_tuning] cruise_lift_scalar=1.00 pitch_stability=0.901 roll_stability=0.800 yaw_stability=0.800 parasite_drag_scalar=1.230 induced_drag_scalar=1.110 elevator_effectiveness=1.001 aileron_effectiveness=1.000 // keyboard = 2.301 rudder_effectiveness=1.000 // keyboard = 2.301 [Radios] Audio.1=1 Com.1=1, 0 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=500.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 use_no_default_bank=1 use_no_default_pitch=0 default_bank_mode=0 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=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [fuel] Center1= 0.000, 0.000, -4.000, 21893.000, 0.000 LeftMain=0.000000,0.000000,0.000000,18000.000000,0.000000 LeftAux=0.000000,-87.416667,0.000000,12000.000000,0.000000 RightMain=0.000000,0.000000,0.000000,18000.000000,0.000000 RightAux=0.000000,87.416667,0.000000,12000.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=8920.000000 wing_span=261.83 wing_root_chord=28.583333 wing_dihedral=8.497925 wing_incidence=0.000000 wing_twist=0.999756 oswald_efficiency_factor=23.358876 wing_winglets_flag=1 wing_sweep=33.330000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=1468.000000 htail_span=72.000000 htail_pos_lon=-128.416667 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=1050.000000 vtail_span=36.945906 vtail_sweep=0.000000 vtail_pos_lon=-116.000000 vtail_pos_vert=5.833333 elevator_area=188.250000 aileron_area=155.840000 rudder_area=84.150000 elevator_up_limit=27.501974 elevator_down_limit=20.626481 aileron_up_limit=19.480565 aileron_down_limit=14.896903 rudder_limit=23.491270 elevator_trim_limit=19.480565 spoiler_limit=59.988681 spoilerons_available=1 aileron_to_spoileron_gain=1.10 min_ailerons_for_spoilerons=11 min_flaps_for_spoilerons=0 //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) [contact_points] // Wheels point.0=1.000000,103.68,0.000000,-10.000,1574.803150,0.000000,5.724152,84.660000,0.9416,2.500000,0.567515,5.000000,7.000000,0.000000,0.000000,0.000000 point.1=1.000000,-8.916667,-19.666667,-12.183333,1574.803150,1.000000,5.724152,0.000000,0.983202,2.500000,0.420762,5.000000,5.000000,2.000000,0.000000,0.000000 point.2=1.000000,-8.916667,19.666667,-12.183333,1574.803150,2.000000,5.724152,0.000000,0.983202,2.500000,0.420762,5.000000,5.000000,3.000000,0.000000,0.000000 // Scrape points // Engine 2 & 3: point.3=2.000000,37.07,-50.48,-5.256,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,37.07,50.48,-5.256,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 // Wingtips: point.5=2.000000,-48.56,-130.9,21.53,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,-48.56,130.9,21.53,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 // Rear fuse: point.7=2.000000,-75.02,0.000,6.457,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 // Underside of the body: point.8=2.000000,-7.014,0.000,-3.504,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 point.8=2.000000,96.34,0.000,-0.935,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=-0.719605 static_cg_height=12.890305 gear_system_type=0 [Flaps.0] type=1 span-outboard=0.500000 extending-time=8.000000 damaging-speed = 230 blowout-speed = 250 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=6.665409,0.000000 flaps-position.2=13.330818,0.000000 flaps-position.3=19.996227,0.000000 flaps-position.4=26.661636,0.000000 flaps-position.5=33.327045,0.000000 flaps-position.6=39.992454,0.000000 [flaps.1] type=2 // 1 - tail, 2 - lead span-outboard = 0.85 extending-time = 4 flaps-position.0 = 0, 0 flaps-position.1 = 18, 230 //Conf. 1 Intermediate approach flaps-position.2 = 22, 215 //Conf. 1+F Take off flaps-position.3 = 22, 205 //Conf. 2 Take off and Approach flaps-position.4 = 22, 195 //Conf. 3 Take off, Approach, and Landing flaps-position.5 = 27, 190 //Conf "Full" Landing flaps-position.6 = 27, 190 //Conf "Full" Landing damaging-speed = 230 blowout-speed = 250 lift_scalar = 0.5 //0.55 drag_scalar = 0.4 pitch_scalar = 0.2 system_type = 0 //Hydraulic [GeneralEngineData] engine_type=1 Engine.0=-2.9,-85.570000,6.1 Engine.1=23.460000,-50.19,2.54 Engine.2=23.460000,50.19,2.54 Engine.3=-2.9,85.570000,6.1 fuel_flow_scalar=0.791748703 min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain=0.002170 inlet_area=79.738480 rated_N2_rpm=29920.000000 static_thrust=67890.000000 afterburner_available=0 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=185.000000 full_flaps_stall_speed=135 cruise_speed=488 max_indicated_speed=350 max_mach=0.89 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=108.8,-2.35,13.92 [General] performance=Airbus A380-800\nRobert Versluys [direction_indicators] direction_indicator.0=3,0 [brakes] toe_brakes_scale=1.00 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] electric_pumps=1 engine_map=1,1,1,1 normal_pressure=3000.000000 [stall_warning] type=1 [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=0,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 2, 30.669, 0.00, 26.371, fx_beaconb, //nav top light.1 = 1, 45.259, 0.00, -2.9167, fx_beaconh, //nav bot light.2 = 2, -109.7802, 0.00, 16.22375, fx_navwhih, //nav tail [TailHook] // #1 Door, upperdeck tailhook_length=1 tailhook_position = 0.0, 0.0, 0.0 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second