//iFDG A320-214 updated to V1.4 and optimized to FSx by Franco Baratti [fltsim.0] title=A320-214 Airone CFM sim=A320-200CFM model= panel= sound= texture=Airone kb_checklists= kb_reference= atc_id= atc_airline= atc_flight_number=1123 atc_heavy=0 ui_manufacturer=iFDG Airbus ui_type="A320-214" ui_variation=Airone description="The A320 was launched on March 2, 1984. It is the first subsonic commercial aircraft with fly-by-wire controls. First flight took place on February 22, 1987. The A320-100 was the initial version and was superseded by the A320-200 from the third quarter of 1988. The A320-200 differs from the A320-100 in having wingtip fences, a wing center-section fuel tank, and a higher MTOW. Model by Albaro Villegas and Ric Barker. Master Textures by Ben Jones. FDE by Pedro Oliveira. Textures by Franco Baratti" atc_id_color=0000000000 visual_damage=0 prop_anim_ratio=1.72 [General] atc_type=Airbus atc_model=A320 editable=0 performance=Engines\nCFM-56 5B rated at 26,500 lbs\n\nTypical Cruise Speed\n0.78 Mach at 35,000 ft\n\nMax Speed\nVmo 350 kts Mmo 0.82 Mach\n\nRange(150 pax)\n2,900 nm (5,374 km)\n\nMax Fuel\n42,230 lbs (6,303 US gal)\n\nMax Takeoff Weight\n162,040 lbs\n\nMax Gross Weight (taxi weight)\n162,900 lbs\n\nMax Payload\n42,370 lbs Category=airplane [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 [WEIGHT_AND_BALANCE] reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, 0.000 station_load.0=310.000, 43.000, 0.000, 0.000 //(crew) station_load.1=5920.000, 32.000, 0.000, 0.000 //frontmost cabin station_load.2=3150.000, 25.000, 0.000, 0.000 //front cargo bay station_load.3=6920.000, 15.000, 0.000, 0.000 //center cabin station_load.4=4400.000, -15.000, 0.000, 0.000 //rearmost cargo bay station_load.5=8840.000, -23.000, 0.000, 0.000 //rearmost cabin //total load=29,540lbs, empty wt. 98,500lbs (29,540+98,500= 128,040lbs/58.2T) empty_weight=98500.000 empty_weight_roll_MOI=1801400.000000 empty_weight_pitch_MOI=3580000.000000 empty_weight_yaw_MOI=2000000.000000 empty_weight_coupled_MOI=1200.000000 max_gross_weight=170270.099 //aircraft.cfg file by Peter Binamira. Must be used with the PA A320 aircrafts. 07/24/02 [General] performance=July 24, 2002 revision 008\n\n\n\n atc_type=Airbus atc_model=A320 [GeneralEngineData] engine_type=1 fuel_flow_scalar=1.12 Engine.0=10.000000,-18.833333,-3.933333 Engine.1=10.000000,18.833333,-3.933333 min_throttle_limit=-0.269958 [Reference Speeds] flaps_up_stall_speed=128.000 full_flaps_stall_speed=102.000 cruise_speed=455.020 max_indicated_speed=350.000000 max_mach=0.820020 [autopilot] autoland_available=0 autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=87.00000 pitch_takeoff_ga=8.000000 use_no_default_pitch=1 use_no_default_bank=1 default_pitch_mode=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 [direction_indicators] direction_indicator.0=3,0 [smokesystem] smoke.0 = 88.0,-17.3,-39.8, fx_contrail_320 smoke.1 = 88.0,-17.3,39.8, fx_contrail_320 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 [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 [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, 33.85, 0.0, -10.8, 1574.8, 0.0, 1.68, 75.0, 0.41, 2.5, 0.65, 9.0, 9.4, 0.0, 0.0, 0.0 point.1 = 1, -3.80, -12.417, -11.45, 1574.803, 1.0, 1.68, 0.0, 1.0, 2.5, 0.52, 13.0, 11.7, 2.0, 0.0, 0.0 point.2 = 1, -3.80, 12.417, -11.45, 1574.803, 2.0, 1.68, 0.0, 1.0, 2.5, 0.52, 13.1, 11.9, 3.0, 0.0, 0.0 point.3 = 2, -13.75, -54.58, -0.5, 750.925, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0 point.4 = 2, -13.75, 54.58, -0.5, 750.925, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0 point.5 = 2, -71.25, 0.0, 0.75, 750.925, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0 point.6 = 2, 51.67, 0.0, -8.17, 750.925, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0 point.7 = 5, -50.9, -19.25, -19.3, 1600, 0.0, 0.0, 70.0, 0.0, 0.0, 5.0, 3.0, 3.2, 0.0, 0.0, 0.0 point.8 = 5, -50.9, 19.25, -19.3, 1600, 0.0, 0.0, 70.0, 0.0, static_pitch=0 static_cg_height=10.9 gear_system_type=1 //Hydraulic [fuel] Center1=0.000, 0.000, -4.000, 2180.0, 8.000 LeftMain=-5.000, -15.000, 0.000, 1829.5, 5.000 RightMain=-5.000, 15.000, 0.000, 1829.5, 5.000 LeftAux=-8.5, -30.0, -3.0, 232.0, 0.0 RightAux=-8.5, 30.0, -3.0, 232.0, 0.0 fuel_type=2.000000 number_of_tank_selectors=1 fuel_type=2.000000 electric_pump=0 [keyboard_response] aileron=180.000000,130.000000 [pitot_static] vertical_speed_time_constant=1 pitot_heat=1.000000 [Views] eyepoint=43.22074,-1.723061,4.355627 [Flaps.0] type=1 span-outboard=0.800 extending-time=21.000 system_type=1 damaging-speed=233.000 blowout-speed=250.000 flaps-position.0=0.000, flaps-position.1=7.000, flaps-position.2=14.000, flaps-position.3=21.000, flaps-position.4=28.000, flaps-position.5=35.000, lift_scalar=0.85 drag_scalar=0.8 pitch_scalar=7.0 [flaps.1] type=2 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=18 // seconds flaps-position.0=0 flaps-position.1=0, flaps-position.2=5, flaps-position.3=10, flaps-position.4=10, flaps-position.5=27, blowout-speed=260 // KIAS lift_scalar=0.4 drag_scalar=0.3 system_type=1 [jet_engine] thrust_scalar=1.000 [GROUND_REACTION] MAX_STEERING_ANGLE=75 [TurbineEngineData] fuel_flow_gain=0.002380 inlet_area=31.000000 rated_N2_rpm=29920.000000 static_thrust=26500.000000 afterburner_available=0 reverser_available=1 [exits] number_of_exits=3 exit.0=0.2, 35.00, -6.0, 7.0, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) exit.1=0.2, -25.00, 5.85, -3.0, 1 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency) exit.2=0.2, 35.00, 6.0, 7.0, 2 [airplane_geometry] fly_by_wire=1 wing_area=1320.000000 wing_span=111.833333 wing_root_chord=16.666667 wing_dihedral=4.498901 wing_incidence=-0.783823 wing_twist=0.000000 oswald_efficiency_factor=0.650 wing_winglets_flag=1 wing_sweep=25.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=337.000000 htail_span=41.666667 htail_pos_lon=-50.000000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=249.000000 vtail_span=17.991665 vtail_sweep=0.000000 vtail_pos_lon=-35.833333 vtail_pos_vert=5.833333 elevator_area=70.500000 aileron_area=26.800000 rudder_area=56.200000 elevator_up_limit=28.0 elevator_down_limit=20.0 aileron_up_limit=26.0 aileron_down_limit=26.0 rudder_limit=25.0 elevator_trim_limit=18.5 spoiler_limit=35.0 spoilerons_available=1 aileron_to_spoileron_gain=1.10 min_ailerons_for_spoilerons=11 min_flaps_for_spoilerons=0 auto_spoiler_available=1 spoiler_extension_time=1.200000 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=3.000000 negative_g_limit_flaps_up=-3.000000 negative_g_limit_flaps_down=-2.000000 [flight_tuning] parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=0.95 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.2 aileron_trim_effectiveness=0.9 rudder_trim_effectiveness=1.1 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing //Tail Lights light.0 = 3, -72.26, 0, 5.08, iFDG_A320_whitenav light.1 = 2, -72.26, 0, 5.08, iFDG_A320_whitestrobe_tail //Wing strobes light.2 = 2, -17.00, -55.44, 4.41, iFDG_A320_whitestrobe light.3 = 2, -17.00, 55.44, 4.41, iFDG_A320_whitestrobe //Beacon lights light.4 = 1, 3.070, 0, 9.00, iFDG_A320_redbeacon_top light.5 = 1, 6.381, 0, -4.862, iFDG_A320_redbeacon_bottom //Logo lights light.6 = 5, -64.257, 11.41, 5.866, iFDG_A320_logo light.7 = 5, -64.257, -11.41, 5.866, iFDG_A320_logo //Inspection lights light.8 = 5, 21.777, 6.463, 1.791, iFDG_A320_inspection light.9 = 5, 21.777, -6.463, 1.791, iFDG_A320_inspection [ground_reaction] main_gear_static_compression=1.5 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression=0.9 // (feet), The distance the center gear strut is compressed when at rest on the ground [TailHook] tailhook_length=4 ;(feet) tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=0.9 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) electric_always_available=1 flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 0, 17.0 avionics=1, 0 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 0, 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 0 , 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, 0 , 17.0 [brakes] toe_brakes_scale=0.503555 parking_brake=1 auto_brakes=4 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [airspeed_indicators] airspeed_indicator.0=1 airspeed_indicator.1=1 [altimeters] altimeter.0=1 altimeter.1=1 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=0