/ This aircraft configuration file is made for the FS 2002 Airbus A320-200 // made by Holger Ellerbrock and developed for "Eurowings professional" by Aerosoft. / Flight dynamics developed by Alexander M. Metzger [fltsim.0] title=Iberia Airbus A320-200 sim=A320_2k2v4.6n model=cfm panel= sound= texture=ib kb_checklists=A320_check kb_reference=A320_ref atc_id=ECHTC atc_id_color=0xffffffff atc_airline=IBERIA atc_flight_number=IB6163 ui_manufacturer=Airbus ui_type=A320-200 ui_variation=Iberia A320-231 EC-HTC "Alpujarra" description=Este avión es uno de los últimos A320 que se han incorporado a la numerosa flota de este modelo que posee Iberia.\nDesign: Holger Ellerbrock & Andrew Richards 09\/2001\nBase textures: Frank Di Candia 09\/2001\nLivery: Manolo Machuca Medina 01\/2002\nFDX: Alexander M. Metzger 2k2V4.6n [fltsim.1] title=Condor Airbus A320-200 sim=A320_2k2v4.6n model=cfm panel= sound= texture=de kb_checklists=A320_check kb_reference=A320_ref atc_id=DAICI atc_id_color=0xffffffff atc_airline=Condor atc_flight_number=DE100 ui_manufacturer=Airbus ui_type=A320-200 ui_variation=Condor D-AICI description=FS2002 Airbus A320-200\nDesign: Holger Ellerbrock &\nAndrew Richards 09\/2001\nBase textures: Frank Di Candia 09\/2001\nLivery: Holger Ellerbrock 12\/2002\nFDX: Alexander M. Metzger 2k2V4.6n [General] atc_type=Airbus atc_model=A320 editable=1 performance=Airbus A320-200\nWing span: 34.09 m \/ 111.8 ft\nLength: 37.57 m \/ 123.2 ft\nHeight: 11.76 m \/ 38.6 ft\nWing Area: 122.6 m2 \/ 1319 sqft\n\nDry Operating Weight: 41,000 kg \/ 90,390 lb\nMax. Fuel: 18,870 kg \/ 6,300 gal\nMax. Take Off Weight: 73,500 kg \/ 162,040 lb\nZero Fuel Weight FDX: 54,350 kg \/ 119,820 lb\nEngine: CFM 56-5 120.1 kN \/ 27,000 lb\nPassengers: 147 max. 150\nMax. speed: mach 0.82 at FL350\nCruise speed: mach 0.78 at FL350 [WEIGHT_AND_BALANCE] // You may modify below the Zero Fuel Weight of the aircraft you want to fly. // Otherwise enter the Dry Operating Weight and add Payload Weight and addjust MOIs below. // !!WARNING!!: // To maintain operational flight model, the following values of weight need to be checked: // Empty operational weight: 90389 lbs // Maximum fuel weight: 41600 lbs // Maximum take off weight: 162040 lbs empty_weight=90389 // Empty weight of aircraft DOW (lbs) reference_datum_position=0,0,0 // (feet) distance from FS Reference: (1/4 chord, centerline, waterline) empty_weight_CG_position=0,0,0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 // Payload weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.0=353,42.7,0,0 // Weight Pilots (lbs) station_load.1=353,37.3,0,0 // Weight stewards in front (lbs) station_load.3=353,-47.7,0,0 // Weight stewards in rear (lbs) station_load.4=6614,22,0,0 // Weight cargo 1 (lbs) station_load.5=1830,-20,0,0 // Weight cargo 2 (lbs) station_load.6=705,27.6,0,0 // Weight passengers row 1 (lbs) station_load.7=705,24.8,0,0 station_load.8=705,22.1,0,0 station_load.9=529,19.3,0,0 station_load.10=882,16.5,0,0 station_load.11=1058,13.7,0,0 station_load.12=705,10.9,0,0 station_load.13=705,8.1,0,0 station_load.14=1058,5.3,0,0 station_load.15=705,2.5,0,0 station_load.16=705,-0.3,0,0 station_load.17=882,-3.1,0,0 station_load.18=882,-5.9,0,0 station_load.19=1058,-8.7,0,0 station_load.20=882,-11.4,0,0 station_load.21=882,-14.2,0,0 station_load.22=705,-17,0,0 station_load.23=705,-19.8,0,0 station_load.24=882,-22.6,0,0 station_load.25=705,-25.4,0,0 station_load.26=1058,-28.2,0,0 station_load.27=705,-31,0,0 station_load.28=705,-33.8,0,0 station_load.29=705,-36.6,0,0 station_load.30=705,-39.4,0,0 //The Zero Fuel Weight of this aircraft is 54350 kg equal 119820 pounds // Moment of Inertia empty_weight_roll_MOI= 1298961 empty_weight_pitch_MOI= 1694567 empty_weight_yaw_MOI= 1621303 empty_weight_coupled_MOI= 0 [Reference Speeds] flaps_up_stall_speed=130 // (Knots) KTAS full_flaps_stall_speed=105 // (Knots) KTAS cruise_speed=465 // (Knots) KTAS [pitot_static] vertical_speed_time_constant=1.0 // Increasing this value will cause a faster reaction in the VSI [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.05 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.0 roll_stability=1.0 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= 6.1, -19.0, -4.9 // (feet) longitudinal, lateral, vertical distance from reference datum Engine.1= 6.1, 19.0, -4.9 // (feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0 [TurbineEngineData] fuel_flow_scalar=1.0 // Scalar for fuel flow efficiency fuel_flow_gain=0.002 // Gain on fuel flow inlet_area=19.6 // Square Feet, engine nacelle inlet area rated_N2_rpm=29920 // (RPM) second stage compressor rated value static_thrust=27000 // (Lbs) max rated static thrust at Sea Level afterburner_available=0 reverser_available=1 [jet_engine] thrust_scalar=1.0 // Scalar for thrust efficiency [fuel] // Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center1= 1.8, 0.0, -1.8, 2179, 5 LeftMain= -1.8, -15.3, 0.6, 1829, 5 RightMain= -1.8, 15.3, 0.6, 1829, 5 LeftAux= -15.9, -44.0, 4.9, 232, 2 RightAux= -15.9, 44.0, 4.9, 232, 2 fuel_type=2 // Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [airplane_geometry] wing_area=1319 // (square feet) wing_span=112.0 // (feet) wing_root_chord=13.5 // (feet) (AMM mean chord) wing_dihedral=7.0 // (degrees) wing_incidence=0.0 // (degrees) wing_twist=-0.5 // (degrees) oswald_efficiency_factor=0.75 // Measure of lift effeciency of wing wing_winglets_flag=1 // Are winglets available? wing_sweep=31.0 // (degrees) wing leading edge wing_pos_apex_lon=10.4 // (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=358 // (feet) htail_span=44.7 // (feet) htail_pos_lon=-54.4 // (feet) longitudinal distance from reference point, negative going aft htail_pos_vert=5.5 // (feet) vertical distance from reference point, positive going up htail_incidence=0.0 // (degrees) htail_sweep=35.0 // (degrees) horizontal tail leading edge vtail_area=316 // (square feet) vtail_span=22.7 // (feet) tip to body vtail_sweep=40.0 // (degrees) vertical tail leading edge vtail_pos_lon=-417.7 // (feet) longitudinal distance from reference point, negative going aft vtail_pos_vert=9.8 // (feet) vertical distance from reference point, positive going up elevator_area=127.8 // (square feet) aileron_area=75.2 // (square feet) rudder_area=85.7 // (square feet) elevator_up_limit=20 // (degrees) elevator_down_limit=30 // (degrees) aileron_up_limit=25 // (degrees) aileron_down_limit=25 // (degrees) rudder_limit=30 // (degrees) elevator_trim_limit=15 // (degrees) spoiler_limit=45 // (degrees) spoilerons_available=0 // Spoilerons Available? aileron_to_spoileron_gain=3.0 // Aileron to spoileron gain min_ailerons_for_spoilerons=10 // (degrees) min_flaps_for_spoilerons=0 // Minimum flap handle position when spoilerons activate [Views] eyepoint=42.6, -2.2, 5.8 // (feet) longitudinal, lateral, vertical distance from reference datum [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) // 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0= 1, 34.0, 0.0, -9.7, 1800, 0, 1.24, 80, 0.70, 1.5, 0.80, 6.0, 8.0, 0, 250, 250 point.1= 1, -7.1, -12.6, -9.7, 2400, 1, 1.88, 0, 0.70, 1.5, 0.60, 8.0, 10.0, 2, 250, 250 point.2= 1, -7.1, 12.6, -9.7, 2400, 2, 1.88, 0, 0.70, 1.5, 0.60, 8.0, 10.0, 3, 250, 250 point.3= 2, -24.0, -57.2, 6.0, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, point.4= 2, -24.0, 57.2, 6.0, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, point.5= 2, -72.7, 0.0, 7.4, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, point.6= 2, 50.5, 0.0, 1.2, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, max_number_of_points=21 static_pitch=0.0 // (degrees) pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=9.0 // (feet) altitude of CG when at rest on the ground [LIGHTS] // type, longitudinal, lateral, vertical distance (feet) from reference datum, filename // Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -20.2, -56.45, 6.00, fx_navred light.1=3, -20.2, 56.45, 6.00, fx_navgre light.2=2, -21.0, -56.45, 6.00, fx_strobeh light.3=2, -21.0, 56.45, 6.00, fx_strobeh light.4=2, -73.2, 0.10, 6.80, fx_strobeh light.5=1, 0.0, 0.00, 10.00, fx_beaconb light.7=1, 2.8, 0.00, -3.75, fx_beaconh light.8=3, -73.2, -0.10, 6.80, fx_navwhi [Flaps.0] // Trailing Edge Flaps type=1 // 1 - tail, 2 - lead span-outboard=0.75 // 0.0...1.0 extending-time=12.0 // (seconds) flaps-position.0=0 // (degrees) flaps-position.1=7 // (degrees) flaps-position.2=15 // (degrees) flaps-position.3=20 // (degrees) flaps-position.4=35 // (degrees) flaps-position.5=40 // (degrees) damaging-speed=230 // (Knots) KTAS blowout-speed=250 // (Knots) KTAS lift_scalar=1.0 drag_scalar=1.0 pitch_scalar=1.0 system_type=1 // Hydraulic [flaps.1] // Inboard Leading Edge Flaps type=2 // 1 - tail, 2 - lead span-outboard=0.9 // 0.0 .. 1.0 extending-time=3 // (seconds) flaps-position.0=0 // flaps-position.1=0.5 // flaps-position.3=1.0 // damaging-speed=230 // (Knots) KTAS blowout-speed=250 // (Knots) KTAS lift_scalar=1.0 drag_scalar=1.0 pitch_scalar=1.0 system_type=1 // Hydraulic [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=500 use_no_default_pitch=1 // 0 = Default to current pitch mode, 1 = No default pitch mode. use_no_default_bank=1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode. autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=96 pitch_takeoff_ga=8.0 autoland_available=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 [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 Transponder.1 = 1 Marker.1 = 1 [electrical] // BusType, MaxAmpLoad, MinVoltage // BusTypes: 0=MainBus, 1=AvionicsBus, 2=BatteryBus, 3=HotBatteryBus, 4-7=Generator/AlternatorBus(1-4) 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, 2 , 17.0 additional_system= 0, 20, 17.0 marker_beacon= 1, 2 , 17.0 gear_warning= 0, 2 , 17.0 fuel_pump= 0, 5 , 17.0 fuel_transfer_pump= 0, 5 , 17.0 starter1= 0, 20, 17.0 starter2= 0, 20, 17.0 auto_brake= 0, 0, 17.0 standby_vacuum= 0, 0, 17.0 hydraulic_pump= 0, 0, 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 light_recognition= 0, 5 , 17.0 light_wing= 0, 5 , 17.0 light_logo= 0, 5 , 17.0 max_battery_voltage= 28.0 generator_alternator_voltage= 28.0 max_generator_alternator_amps= 40.0 [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, 200 aileron= 150, 200 rudder= 150, 200 [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
