[fltsim.0] title=Airbus A340-600 Iberia sim=a340 model= panel= sound= texture=iberia kb_checklists= kb_reference= atc_id=EC-IOB atc_airline=Iberia atc_flight_number=301 atc_heavy=1 ui_manufacturer=Airbus ui_type=A340-600 ui_variation=Iberia visual_damage=1 description=The Airbus 340-600 is Airbus' newest production from the vernerable A340 family. This aircraft comes standard with common Airbus features all of pilots have come to respect (Fly by Wire controls, Next Generation Cockpit design, ETC.,), while maintaining a standard adapatation/familiarization environment which provides a comfortable working and learning setting for flight crew and general crew alike. [General] atc_type=AIRBUS atc_model=A340 editable=1 performance=Maximum Cruise: Mach .86\nEngines: Four (4) RR Trent 556 Turbofans\nThrust: 56,000 lbs or 20,901 KG\nMaximum Range: 7480 NM or 13,853 KM\nPax Capacity: 380 - 475 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\nV1K-2 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [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= 804675 // (pounds)920000 empty_weight=391000 // (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=10620, 0.0, 0.0,0.0 //PAX SEC 1 (DEFAULT:10620)78, 0,0.98 / station_load.1=18360, 0.0, 0.0,0.0 //PAX SEC 2 (DEFAULT:18360)-0.55, 0,0.98 station_load.2=8100, 0.0, 0.0,0.0 //PAX SEC 3 (DEFAULT:8100)-55.7, 0,0.98 //station_load.3=139074,0,0,0 //AFT Galley Payload (MAX: MIN: DEFAULT:) Rick added //CARGO AND FRIEGHT LOADOUT station_load.4=4037, 0.0, 0.0,0.0 //FORE CARGO COMPARTMENT (DEFAULT: 4037) 96.03,0,-4.26 station_load.5=3131, 0.0, 0.0,0.0 //AFT LARGE CARGO COMPARTMENT(DEFAULT:3131)-69.16,0,-4.26 station_load.6=1071, 0.0, 0.0,0.0 //AFT SMALL CARGO COMPARTMENT(DEFAULT:1071)-76.96,0,-4.26 //PILOT AND RELIEF WEIGHT station_load.7=180, 0.0, 0.0,0.0 //CAPTAIN WEIGHT (DEFAULT: 180)-1.6,118.1,1.6 station_load.8=180, 0.0, 0.0,0.0 //FIRST OFFICER WEIGHT (DEFAULT: 180)1.6,118.1,1.6 station_load.9=220, 0.0, 0.0,0.0 //JUMPSEAT/RELIEF PILOT(S) (DEFAULT: 220)2.2,114.8,1.6 ;Moments of Inertia empty_weight_roll_MOI=15352310 empty_weight_pitch_MOI=24223159 empty_weight_yaw_MOI=39531785 empty_weight_coupled_MOI=0 ;2142 [fuel] Center1=21.3, 0.0, -7.0, 18786.0, 7.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center1=21.3, 0.0, -7.0, 14788.0, 7.0 Center2=-37.0, 0.0, 6.5, 2177.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center2=-107.0, LeftMain=20, -50.1, -4.0, 15588.0, 9.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux=-2.3, -63.0, -3.0, 1680.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=20, 50.1, -4.0, 15588.0, 9.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux=-2.3, 63.0, -3.0, 1680.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=4729.16 //Square feet wing_span=208.5 //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=37.5 //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 //1470 Square feet, Rick htail_span=72.8 //72.8 Feet, Rick htail_pos_lon=-210.0 //-210.0 long, Rick htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_incidence=-6.0 //0.0 Degrees, Rick -6.0 worked but a bit too "down" htail_sweep=37.5 //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 //30 Degrees Rick elevator_down_limit=17 //17 Degrees Rick 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 //Spoilerons Available? aileron_to_spoileron_gain=2 //Aileron to spoileron gain min_ailerons_for_spoilerons=15 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate [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) max_indicated_speed=370.671875 max_mach=0.904980 // [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=1.1 //2.1 Rick induced_drag_scalar=1.8 //1.8 Rick elevator_effectivenes=2.0 //1.0 Rick aileron_effectiveness=2.0 //0.7 rick rudder_effectiveness=1.0 pitch_stability=1.15 //1.0 Rick roll_stability=1.0 //1.0 Rick yaw_stability=1.0 //1.0 Rick elevator_trim_effectiveness=2.0 //1.0 Rick 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=1.05 //Scalar for fuel flow efficiency min_throttle_limit=-0.250000 max_contrail_temperature = -27 [TurbineEngineData] fuel_flow_gain=0.002 //Gain on fuel flow inlet_area=56.2 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=56000 //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=1000.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=99 //96 Rick autothrottle_takeoff_ga=1 pitch_takeoff_ga=8; 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 [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, 102.5, 0.0, -17.1, 1500.0, 0, 1.584, 85, 0.6, 3, 2.100, 9.0, 8.0, 0, 220, 262 point.1=1, -9, 0.0, -18.90, 2000.0, 0, 1.837, 0, 1, 1, 0.900, 11.0, 9.0, 2, 220, 262 point.2=1, -9, -17.536, -18.90, 2000.0, 1, 1.837, 0, 1, 1, 0.900, 11.0, 9.0, 3, 220, 262 point.3=1, -9, 17.536, -18.90, 2000.0, 2, 1.837, 0, 1, 1, 0.900, 11.0, 9.0, 3, 220, 262 //Tail Scrape Points point.4=2, -72.178, 0.0, -9.51, 430.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 0, 0 //Crest point.5=2, -131.23, 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=16.7 gear_system_type=0 [Views] eyepoint=42.00, -7.30, 3.00 //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] [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, -123.839, -0.151, 6.819, fx_navwhih , light.3 =2, -123.839, 0.151, 6.819, fx_strobeh , light.4 =5, 18, 27.464, -4, A340_wingscan, light.5=5, -1.933, 60.827, -0.368, A340_wingscan, light.6=5, 18, -27.464, -4, A340_wingscan, light.7=5, -1.933, -60.827, -0.368, A340_wingscan, light.8 =4, 117.038, 0, 2.812, A340_cockpit, light.9=6, 97.0, 0.00, -10.0, noselight , light.10 = 3, -115.94, -6.58, 30.36, Newll , light.11 = 3, -115.94, 6.58, 30.36, Newll , light.12 = 3, 40.94, -15.58, -3.36, Newll , light.13 = 3, 40.94, 15.58, -3.36, Newll , //longitudinal, lateral, vertical distance from reference datum [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 //contrail=fx_A_I_Contrail //Rick removed [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second ;1660 [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 [brakes] toe_brakes_scale=0.91 //1.241798 parking_brake=1 differential_braking_scale = 1.0 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
