[fltsim.0] title=Airbus A319 EasyJet sim=3xx_AIIS model=319 panel= sound= texture=319_EASY atc_id=319 atc_airline=Easy atc_flight_number=1123 ui_manufacturer=AI ui_type=Airbus A319 ui_variation=EasyJet atc_id_color=000000ff80 visual_damage=0 atc_heavy=1 [fltsim.1] title=Airbus A321 AlItaia sim=3xx_AIIS model=321 panel= sound= texture=321_ALITALIA kb_checklists= kb_reference= atc_id= atc_airline=AlItaia atc_flight_number=1512 ui_manufacturer=AI ui_type=Airbus A321 ui_variation=AlItaia atc_id_color=000000ff80 visual_damage=0 atc_heavy=1 [fltsim.2] title=Airbus A321 Lufthansa sim=3xx_AIIS model=321 panel= sound= texture=321_LUFT kb_checklists= kb_reference= atc_id= atc_airline=LUFTHANSA atc_flight_number=0732 ui_manufacturer=AI ui_type=Airbus A321 ui_variation=Lufthansa atc_id_color=000000ff80 visual_damage=0 atc_heavy=1 [General] atc_type=Airbus atc_model=A320 editable=0 performance=Cruise Speed\t.74 Mach\nMaximum Range\t2,059 nm\nService Ceiling\t36,089 ft\nMax Takeoff Weight\t138,500 lb\nSeating\t\t147 to 168\nCargo Capacity\t1,373 CU ft\n [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI [weight_and_balance] // ACM V2.0 max_gross_weight = 138500 empty_weight = 100792 reference_datum_position = 5, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 3172439 empty_weight_roll_MOI = 2262183 empty_weight_yaw_MOI = 3337024 empty_weight_coupled_MOI = 0 max_number_of_stations = 1 station_load.0 = 0.000000,0.000000,0.000000,0.000000 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.4 = 2, -2.65, 0, -4, fx_beaconb light.5 = 1, 2.2, 0, 10.2, fx_beaconh [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 1 engine.0 = 4.75, -16.1, -2.5 engine.1 = 4.75, 16.1, -2.5 min_throttle_limit=-0.250000 [smokesystem] smoke.0 = -4, -48.28, 19, fx_smoke_w smoke.1 = -4, -48.28, -19, fx_smoke_w [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 Center1 = 0, 0, 0, 2313, 0 LeftMain = -3, -19, 0, 1500, 0 RightMain = -3, 19, 0, 1500, 0 electric_pump=0 [contact_points] static_pitch = 0 static_cg_height = 8.6 max_number_of_points = 7 point.0 = 1, 35.4753, 0, -9.5471, 1181.1, 0, 1.3, 55.92, 1, 2.5, 0.9, 4, 4, 0, 0, 0 point.1 = 1, -5.0039, -13, -10.4862, 1574.8, 1, 2, 0, 1.8, 2.5, 0.9, 6.9, 6.9, 2, 0, 0 point.2 = 1, -5.0053, 13, -10.4862, 1574.8, 2, 2, 0, 1.8, 2.5, 0.9, 7.1, 7.1, 3, 0, 0 point.3 = 2, -14.17, -55.3413, 4.42, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -14.17, 55.3416, 4.1437, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -54.2387, 0, 1.6921, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 42.2554, 0, -2.9364, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 gear_system_type=0 [keyboard_response] elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [forcefeedback] gear_bump_nose_magnitude = 3000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2700 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2700 gear_bump_right_direction = 00500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1300 ground_bumps_angle1 = 08900 ground_bumps_intercept1 = 3.0 ground_bumps_slope1 = 0.20 ground_bumps_magnitude2 = 200 ground_bumps_angle2 = 09100 ground_bumps_intercept2 = 1.075 ground_bumps_slope2 = 0.035 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 [airplane_geometry] //ACM_AREAW1// 0,0,0,5.4864,1.6044,1.6044,0.7480,5.9601,3.2088,3.2088 //ACM_AREAW2// 1.4960,6.4340,4.8133,4.8133,2.2444,6.9078,6.4176,6.4176,2.9925,7.3817 //ACM_AREAW3// 8.0221,8.0221,3.7407,7.8555,9.6266,9.6266,4.4889,8.3294,11.2306,11.2306 //ACM_AREAW4// 5.2371,8.8030,12.8353,12.8353,5.9850,9.2770,14.4399,14.4399,6.7333,9.7509 //ACM_AREAH1// 0,0,0,4.2367,0.7059,0.7059,0.4074,4.4324,1.4119,1.4119 //ACM_AREAH2// 0.8151,4.6283,2.1182,2.1182,1.2230,4.8242,2.8243,2.8243,1.6303,5.0198 //ACM_AREAH3// 3.5306,3.5306,2.0383,5.2157,4.2367,4.2367,2.4460,5.4116,4.9428,4.9428 //ACM_AREAH4// 2.8536,5.6076,5.6489,5.6489,3.2613,5.8034,6.3550,6.3550,3.6691,5.9993 //ACM_AREAV1// 0,0,0,6.0960,0.6772,0.6772,0.4742,6.0823,1.3545,1.3545 //ACM_AREAV2// 0.9484,6.0689,2.0320,2.0320,1.4227,6.0556,2.7093,2.7093,1.8969,6.0423 //ACM_AREAV3// 3.3866,3.3866,2.3712,6.0289,4.0640,4.0640,2.8454,6.0155,4.7413,4.7413 //ACM_AREAV4// 3.3199,6.0019,5.4186,5.4186,3.7941,5.9885,6.0960,6.0960,4.2684,5.9752 //ACM_CAREAW1// 7.2199,7.2199,6.1097,7.2069,8.0221,8.0221,6.4839,7.5264,8.8240,8.8240 //ACM_CAREAW2// 6.8579,7.8456,9.6266,9.6266,7.2321,8.1646,10.4287,10.4287,7.6062,8.4840 //ACM_CAREAW3// 11.2306,11.2306,7.9801,8.8030,12.0332,12.0332,8.3542,9.1224,12.8353,12.8353 //ACM_CAREAW4// 8.7284,9.4413,13.6372,13.6372,9.1021,9.7608,14.4399,14.4399,9.4764,10.0801 //ACM_CAREAH1// 0,0,2.1182,4.2367,0.7059,0.7059,2.5260,4.5384,1.4119,1.4119 //ACM_CAREAH2// 2.9337,4.8400,2.1182,2.1182,3.3413,5.1420,2.8243,2.8243,3.7490,5.4436 //ACM_CAREAH3// 3.5306,3.5306,4.1567,5.7455,4.2367,4.2367,4.5644,6.0472,4.9428,4.9428 //ACM_CAREAH4// 4.9720,6.3488,5.6489,5.6489,5.3797,6.6508,6.3550,6.3550,5.7873,6.9524 //ACM_CAREAV1// 0,0,1.5240,4.5720,0.6772,0.6772,1.9982,4.8024,1.3545,1.3545 //ACM_CAREAV2// 2.4725,5.0328,2.0320,2.0320,2.9467,5.2631,2.7093,2.7093,3.4210,5.4937 //ACM_CAREAV3// 3.3866,3.3866,3.8952,5.7241,4.0640,4.0640,4.3695,5.9545,4.7413,4.7413 //ACM_CAREAV4// 4.8439,6.1848,5.4186,5.4186,5.3179,6.4154,6.0960,6.0960,5.7923,6.6458 wing_area = 1137.0 wing_span = 94.75 wing_root_chord = 18.0 wing_dihedral = 6.2 wing_incidence = 1.0 wing_twist = -0.5 oswald_efficiency_factor = 0.75 wing_winglets_flag = 0 wing_sweep = 25.0 wing_pos_apex_lon = 8.0 wing_pos_apex_vert = 0.0 htail_area = 338.0 htail_span = 41.7 htail_pos_lon = -35.0 htail_pos_vert = 0.0 htail_incidence = 0.0 htail_sweep = 30.0 vtail_area = 224.0 vtail_span = 20.0 vtail_sweep = 35.0 vtail_pos_lon = -35.8 vtail_pos_vert = 5.8 elevator_area = 70.5 aileron_area = 26.9 rudder_area = 56.2 elevator_up_limit = 22.5 elevator_down_limit = 19.5 aileron_up_limit = 20.0 aileron_down_limit = 20.0 rudder_limit = 26.0 elevator_trim_limit = 20.0 spoiler_limit = 60.0 aileron_to_spoileron_gain = 3 min_ailerons_for_spoilerons = 10 min_flaps_for_spoilerons = 0 spoilerons_available = 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 electric_always_available = 0 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 20, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 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 [TurbineEngineData] 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=23500 //Lbs, max rated static thrust at Sea Level afterburner_available=0 //Afterburner available? reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar=1.0 [Views] eyepoint=43.7, -1.31, 3.55 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.0] //Trailing Edge Flaps type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 20 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 1 // degrees flaps-position.2 = 2 // degrees flaps-position.3 = 5 // degrees flaps-position.4 = 10 // degrees flaps-position.5 = 15 // degrees flaps-position.6 = 25 // degrees flaps-position.7 = 30 // degrees flaps-position.8 = 40 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS 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 = 0.8 // 0.0 .. 1.0 extending-time = 2 // seconds flaps-position.0 = 0 // flaps-position.1 = 1.0 // damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [flaps.2] //Outboard Leading Edge Slat type = 2 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 3 // seconds flaps-position.0 = 0 // flaps-position.1 = 0.5 // flaps-position.4 = 1.0 // damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar= 1.0 system_type = 1 //Hydraulic [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 [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 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm = 90 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 [Reference Speeds] flaps_up_stall_speed=142.0 //Knots True (KTAS) full_flaps_stall_speed=113.0 //Knots True (KTAS) cruise_speed=477 max_indicated_speed=340.000000 max_mach=0.820020 [brakes] toe_brakes_scale=0.885037 parking_brake=1 [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=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
