[fltsim.0] title=Airbus 340-500 Lisbon Sun sim=a345 model= panel= sound= texture= kb_checklists= kb_reference= atc_id= atc_airline=EMIRATES atc_flight_number= atc_heavy=1 ui_manufacturer=Airbus ui_type=340-500 ui_variation=Lisbon Sun visual_damage=1 description=The Airbus 340-500 is a new the second in the new breed of high technology designs from Airbus Industries. The Airbus A340-500, undisputably the longest range aircraft in the free world, boast an amzing range of 8,650NM (16,019 KM). With the smaller Trent 553 series, the aircraft has less power than its larger sibling, but can fly over 1,150NM* further, and nearly the same airspeed. There are a few differences between the two, but they share the commonality that all Airbus users have come to respect and appreciate. [General] atc_type=AIRBUS atc_model=A340 editable=1 performance=Maximum Cruise: Mach .86\nEngines: Four (4) RR Trent 553 Turbofans\nThrust: 53,000 lbs or 20,901 KG\nMaximum Range: 8650 NM or 16,019 KM\nPax Capacity: 313 Passengers\nSimuBuild Freeware Group\nDesigner: Herve Dongmo\nFlight Dynamics: SimuBuild FDX Engineering Department\nTextureing: SimuBuild Texture Department\nFlight Deck: SimuBuild Flightdeck Engineering.\n Visit us at simubuild.cjb.net\nV1B-3 [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=807452 // (pounds) empty_weight=375700 // (pounds) reference_datum_position=0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-2, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 //PASSENGER WEIGHT LOADOUT station_load.0=5263.2 , 78.0, 0, 15.00 //PAX SEC 1 (DEFAULT: 5263.2) station_load.1=13312.8 , -0.55, 0, 15.00 //PAX SEC 2 (DEFAULT: 13312.8) station_load.2=12384 , -55.0, 0, 15.00 //PAX SEC 3 (DEFAULT: 12384) //station_load.3=0,0,0,0 //AFT Galley Payload (MAX: MIN: DEFAULT:) UNUSED UNUSED UNUSED //CARGO AND FRIEGHT LOADOUT station_load.4=3371.2 , 77.00, 0, -4.26 //FORE CARGO COMPARTMENT (DEFAULT: 3371.2) station_load.5=2614.4 , -55.00, 0, -4.26 //AFT LARGE CARGO COMPARTMENT (DEFAULT: 2614.4) station_load.6=894.4 , -62.00, 0, -4.26 //AFT SMALL CARGO COMPARTMENT (DEFAULT: 894.4) //PILOT AND RELIEF WEIGHT station_load.7=180, 103.00, -1.6.1, 15.0 //CAPTAIN WEIGHT (DEFAULT: 180) station_load.8=180, 103.00, 1.6.1, 15.0 //FIRST OFFICER WEIGHT (DEFAULT: 180) station_load.9=220, 100.00, 114.8, 15.0 //JUMPSEAT/RELIEF PILOT(S) (DEFAULT: 220) ;Moments of Inertia empty_weight_roll_MOI=15352310 empty_weight_pitch_MOI=24223159 empty_weight_yaw_MOI=39531785 empty_weight_coupled_MOI=0 [fuel] Center1= 7.0, 0.0, 7.5, 14788.0, 7.0 //Wing Root Center Fuel Tank (CENTER 1) Center2= -15.0, 0.0, 7.5, 5625.0, 0.0 //Rear Center Tank (RCT) (CENTER 2) Center3= -85.0, 0.0, 20.0, 2177.0, 0.0 //Trim Tank (CENTER 3) LeftMain= 7.0, -40.5, 7.5, 15578.0, 9.0 //INNER 1 + INNER 2 (LEFT MAIN) LeftAux= 7.8, -60.5, 7.5, 1680.0, 0.0 //LEFT OUTTER (LEFT AUX) RightMain= 7.0, 40.5, 7.5, 15578.0, 9.0 //INNER 3 + INNER 4 (RIGHT MAIN) RightAux= 7.8, 60.5, 7.5, 1680.0, 0.0 //RIGHT OUTER (RIGHT AUX) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [airplane_geometry] wing_area=4729.0 //Square feet wing_span=208.2 //Feet wing_root_chord=45.3 //Feet wing_dihedral=7.0 //Degrees wing_incidence=2.0 //Degrees wing_twist=-1.0 //Degrees oswald_efficiency_factor=0.81 //Measure of lift effeciency of wing wing_winglets_flag=1 //Are winglets available? wing_sweep=31.1 //Degrees, wing leading edge wing_pos_apex_lon=-68.2 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0 //Feet, vertical distance from reference point, positive going up htail_area=1470 //Square feet htail_span=72.8 //Feet htail_pos_lon=-210.0 //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=0.0 //Degrees htail_sweep=37.5 //Degrees, horizontal tail leading edge vtail_area=1060 //Square feet vtail_span=37.1 //Feet, tip to body vtail_sweep=45.0 //Degrees, vertical tail leading edge vtail_pos_lon=-198.5 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=26.1 //Feet, vertical distance from reference point, positive going up elevator_area=327 //Square feet aileron_area=225 //Square feet rudder_area=230 //Square feet elevator_up_limit=30 //Degrees elevator_down_limit=17 //Degrees aileron_up_limit=30 //Degrees aileron_down_limit=20 //Degrees rudder_limit=35 //Degrees elevator_trim_limit=16 //Degrees spoiler_limit=35 //Degrees spoilerons_available=1 aileron_to_spoileron_gain=1.500000 min_ailerons_for_spoilerons=10 min_flaps_for_spoilerons=0.000000 [Reference Speeds] flaps_up_stall_speed=224.0 //Knots True (KTAS) full_flaps_stall_speed=155.0 //Knots True (KTAS) cruise_speed=500.0 //Knots True (KTAS) // [flaps.0] //Inboard Trailing Edge Flaps type=1 // 1 - tail, 2 - lead span-outboard=0.2 // 0.0 .. 1.0 extending-time=25 // seconds flaps-position.0=0 // degrees flaps-position.1=0 // degrees flaps-position.2=17.5 // degrees flaps-position.3=22.5 // degrees flaps-position.4=26.5 // degrees flaps-position.5=32 // degrees damaging-speed=269 // KIAS blowout-speed=327 // KIAS lift_scalar=0.38 drag_scalar=0.25 pitch_scalar=0.17 system_type=1 //Hydraulic [flaps.1] //Outboard Trailing Edge Flaps type=1 // 1 - tail, 2 - lead span-outboard=0.2 // 0.0 .. 1.0 extending-time=25 // seconds flaps-position.0=0 // degrees flaps-position.1=0 // degrees flaps-position.2=17.5 // degrees flaps-position.3=22.5 // degrees flaps-position.4=26.5 // degrees flaps-position.5=32 // degrees damaging-speed=269 // KIAS blowout-speed=327 // KIAS lift_scalar=0.38 drag_scalar=0.25 pitch_scalar=0.17 system_type=1 //Hydraulic [flaps.2] //Leading Edge Slats type=2 // 1 - tail, 2 - lead span-outboard=0.2 // 0.0 .. 1.0 extending-time=11 // seconds flaps-position.0=0 // degrees flaps-position.1=21 // degrees flaps-position.2=21 // degrees flaps-position.3=24 // degrees damaging-speed=260 // KIAS blowout-speed=300 // KIAS lift_scalar=0.33 drag_scalar=0.11 pitch_scalar=0.35 system_type=1 //Hydraulic [flight_tuning] cruise_lift_scalar=1.1 parasite_drag_scalar=1.3 induced_drag_scalar=1.3 elevator_effectivenes=1.1 aileron_effectiveness=1.35 rudder_effectiveness=1.10 pitch_stability=1.3 roll_stability=1.6 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=-107.5, -73.0, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-76.0, -38.9, -10.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.2=-76.0, 38.9, -10.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.3=-107.5, 73.5, -6.9 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=0.815 //Scalar for fuel flow efficiency [TurbineEngineData] fuel_flow_gain=0.002 //Gain on fuel flow inlet_area=60.0 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=53000 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar=0.9 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=93.3200 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) //Main and Nose Gear Contact Points point.0=1, 93.0, 0.0, -17.4, 1500.0, 0, 1.584, 85, 0.6, 3, 2.100, 9.0, 8.0, 0, 220, 262 point.1=1, -9, 0.0, -18.9, 2000.0, 0, 1.837, 0, 1, 1, 0.900, 11.0, 9.0, 2, 220, 262 point.2=1, -9, -17.536, -18.9, 2000.0, 1, 1.837, 0, 1, 1, 0.900, 11.0, 9.0, 3, 220, 262 point.3=1, -9, 17.536, -18.9, 2000.0, 2, 1.837, 0, 1, 1, 0.900, 11.0, 9.0, 3, 220, 262 //Tail Scrape Points point.4=2, -65.00, 0.0, -9.42, 430.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 0, 0 //Crest point.5=2, -107.00, 0.0, 6.8, 430.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 6, 0, 0 //Peak //Nose Scrape Points point.6=2, 112.762, 0.0, 7.217, 430.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 9, 0, 0 //Break for NG Door //Fairing Scrape Points point.7=2, 0.75, 0.0, 10.465, 430.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 //Center Faring Bottom //Wing Scrape Points point.8=2, 40.48, -103.83, 4.845, 430.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 //Left Wing point.9=2, 40.48, 103.83, 4.845, 430.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 //Right Wing static_pitch=-0.2 static_cg_height=18.9 [Views] eyepoint=96.00, -2.18, 4.25 //Pilots View [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=1, 18.207, 0, 9.4, fx_beaconb, light.1=1, 18.225, 0, -10.8, fx_beaconh, light.2=3, -111.70, -0.151, 6.819, fx_navwhih , light.3=2, -111.70, 0.151, 6.819, fx_strobeh , light.4=5, 18, 27.0, -4, A340_wingscan, light.5=5, -1.933, 60.827, -0.368, A340_wingscan, light.6=5, 18, -27.0, -4, A340_wingscan, light.7=5, -1.933, -60.827, -0.368, A340_wingscan, light.8=4, 95.038, 0, 2.812, A340_cockpit, light.9=4 41.833, 4, 3.2, A340_cabine, light.10=4, -7.533, 0, 3.2, A340_cabine, light.11=4 45.833, 0, 3.2, A340_cabine, light.12=4 34.833, -4, 3.2, A340_cabine, light.13=4 54.00, 0, 3.2, A340_cabine, [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] 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=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;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
