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Guest nans2k

FSP A333 rr, pw and ge new FDE

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Can someone test these and give me an advise about them here.A lot work and research have been done to match real aircraft behavior.You should like them, I do but i wanted to know if it is worth to upload them here at AVSIM.Thanks// FDE v2.0 by Mikael NANOU made for AI A330-300 GE only [General]atc_type=Airbus atc_model=A330 editable=0 performance=Cruise Speed nMach 0.84 555 mph 893 kmhnnEngine options nP&W 4000nRR Trent 800nGE 90 seriesnnMaximum Range n5,960 nm 6,859 sm 11,038 kmnnService Ceiling n42,000 ft 12,800 mnnFuel Capacity n45,220 U.S. gal 171,160 L nnMaximum Takeoff Weight n660,000 lb 299,370 kgnnLength n242 ft, 4 in 73.9 mnnWingspan n199 ft, 11 in 60.9 mnnHeight n60 ft, 8 in 18.5 mnnSeating nSeats 386 to 550 nnCargo Capacity n7,552 ft 213.8 mn [weight_and_balance]// ACM V2.3max_gross_weight = 509000empty_weight = 267200reference_datum_position = 0, 0, 0empty_weight_CG_position = -2, 0, 0empty_weight_pitch_MOI = 14943223empty_weight_roll_MOI = 5963105empty_weight_yaw_MOI = 15094318empty_weight_coupled_MOI = 2000max_number_of_stations = 2station_load.0 = 7500, -24.75, 0, 0.25station_load.1 = 400, 95.30, 0, 3.45[lights]//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landinglight.0 = 1, 3.00, 0.00, -10.40, fx_beaconb ,light.1 = 1, 52.00, 0.00, 9.90, fx_beaconh ,light.2 = 1, 3.00, 0.00, -10.40, fx_beaconb ,light.3 = 1, 52.00, 0.00, 9.90, fx_beaconh ,[GeneralEngineData]//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turbopropengine_type = 1fuel_flow_scalar = 1engine.0 = 10.5, -32.6, -8.4engine.1 = 10.5, 32.6, -8.4min_throttle_limit=-0.250000[effects]wake = fx_wakewater = fx_spraydirt = fx_tchdrtconcrete = fx_sparkstouchdown = fx_tchdwn, 1[fuel]//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)fuel_type = 2number_of_tank_selectors = 1Center1 = 0, 0, -4, 7670, 3LeftMain = -7, -35, 0, 9000, 3RightMain = -7, 35, 0, 9000, 3electric_pump=0[contact_points]static_pitch = -0.5static_cg_height = 16.56max_number_of_points = 7point.0 = 1, 80.9927, 0, -16.2516, 1581.1, 0, 1.8, 90, 0.63, 2.5, 0.7235, 4, 4, 0, 210, 250point.1 = 1, -4.737, -18.0013, -17.6242, 2574.8, 1, 2.2, 0, 1.21, 2.5, 0.547, 6.9, 6.9, 2, 210, 250point.2 = 1, -4.782, 18.2621, -17.6628, 2574.8, 2, 2.2, 0, 1.21, 2.5, 0.547, 7.1, 7.1, 3, 210, 250point.3 = 2, -39.8568, -102.1276, 13.5122, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0point.4 = 2, -39.4636, 101.6704, 13.1292, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0point.5 = 2, -103.6883, -0.2626, 36.4766, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0point.6 = 2, 102.7405, 0, -1.2679, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0gear_system_type=0[keyboard_response]elevator = 150, 250aileron = 150, 250rudder = 150, 250[forcefeedback]gear_bump_nose_magnitude = 3000gear_bump_nose_direction = 18000gear_bump_nose_duration = 250000gear_bump_left_magnitude = 2700gear_bump_left_direction = 35500gear_bump_left_duration = 250000gear_bump_right_magnitude = 2700gear_bump_right_direction = 00500gear_bump_right_duration = 250000ground_bumps_magnitude1 = 1300ground_bumps_angle1 = 08900ground_bumps_intercept1 = 3.0ground_bumps_slope1 = 0.20ground_bumps_magnitude2 = 200ground_bumps_angle2 = 09100ground_bumps_intercept2 = 1.075ground_bumps_slope2 = 0.035crash_magnitude1 = 10000crash_direction1 = 01000crash_magnitude2 = 10000crash_direction2 = 9000crash_period2 = 75000crash_duration2 = 2500000[airplane_geometry]//ACM_AREAW1// 3.1998,3.1998,2.1533,14.3210,5.6757,5.6757,3.5490,14.4721,7.7480,7.7480//ACM_AREAW2// 4.8892,14.5179,9.5811,9.5811,6.1392,14.6391,14.5843,14.5843,9.1084,16.3617//ACM_AREAW3// 17.3742,17.3742,10.9420,17.2325,23.2297,23.2297,14.8240,19.3602,26.0946,26.0946//ACM_AREAW4// 16.8521,20.5006,29.1688,29.1688,19.3425,21.7754,29.8463,29.8463,20.1068,22.0230//ACM_AREAH1// 0.6074,0.6074,4.6015,5.4935,1.3794,1.3794,0.8162,5.8572,2.5504,2.5504//ACM_AREAH2// 1.3186,6.1609,3.5559,3.5559,2.0978,6.5247,4.5015,4.5015,2.5773,6.8884//ACM_AREAH3// 5.4471,5.4471,3.2967,7.0721,6.2726,6.2726,3.8361,7.3161,7.2782,7.2782//ACM_AREAH4// 4.5555,7.6198,9.1230,9.1230,5.9341,8.1034,9.8288,9.8288,7.0131,8.4671//ACM_AREAV1// 0,0,0,8.5340,1.1073,1.1073,1.4907,8.5466,1.8169,1.8169//ACM_AREAV2// 2.4247,8.8774,2.6061,2.6061,2.8814,8.9694,3.4749,3.4749,3.8949,9.2208//ACM_AREAV3// 4.3435,4.3435,4.5107,9.3927,5.0531,5.0531,5.2059,9.8823,6.0809,6.0809//ACM_AREAV4// 6.1399,10.4518,6.8702,6.8702,6.9945,10.7826,8.0571,8.0571,8.4055,11.0339//ACM_CAREAW1// 3.1689,3.1689,13.0872,14.2601,9.2698,9.2698,13.4847,14.6639,11.2594,11.2594//ACM_CAREAW2// 14.0521,15.1588,15.1877,15.1877,15.3325,16.5522,17.8353,17.8353,16.3092,17.4022//ACM_CAREAW3// 19.2856,19.2856,16.8605,17.8808,20.5706,20.5706,17.2621,18.2290,22.1159,22.1159//ACM_CAREAW4// 17.8033,18.9134,23.5251,23.5251,18.5153,19.5324,29.8614,29.8614,21.0650,22.0606//ACM_CAREAH1// 0.5393,0.5393,3.9156,5.7333,1.5448,1.5448,4.3951,5.8551,2.3106,2.3106//ACM_CAREAH2// 4.6946,6.1567,3.4361,3.4361,4.9345,6.5784,4.7413,4.7413,5.1142,6.8803//ACM_CAREAH3// 5.7466,5.7466,5.5939,7.3017,6.7522,6.7522,5.6539,7.5437,7.8175,7.8175//ACM_CAREAH4// 6.3730,7.9053,8.7629,8.7629,6.6729,8.1471,9.7686,9.7686,7.0925,8.5684//ACM_CAREAV1// -0.3562,-0.3562,7.1862,7.6314,0.0410,0.0410,5.8263,7.8411,1.3457,1.3457//ACM_CAREAV2// 6.4745,8.4069,2.8122,2.8122,7.2845,8.9729,3.6633,3.6633,7.7385,9.3767//ACM_CAREAV3// 4.6441,4.6441,8.2572,9.7810,5.3976,5.3976,8.7110,10.1203,6.3786,6.3786//ACM_CAREAV4// 9.2297,10.5242,7.2621,7.2621,9.7158,10.9280,8.0804,8.0804,10.2993,11.2995wing_area = 3892wing_span = 197.10wing_root_chord = 37.25wing_dihedral = 8.18wing_incidence = 0.0wing_twist = 0.0oswald_efficiency_factor = 0.625wing_winglets_flag = 1wing_sweep = 32.40wing_pos_apex_lon = 36.00wing_pos_apex_vert = -6.26htail_area = 933htail_span = 61.43htail_pos_lon = -81.58htail_pos_vert = 6.51htail_incidence = 0.0htail_sweep = 31.70vtail_area = 650.0vtail_span = 26.17vtail_sweep = 45.18vtail_pos_lon = -70.76vtail_pos_vert = 10.60elevator_area = 95.0aileron_area = 39.0rudder_area = 155.0elevator_up_limit = 30elevator_down_limit = 18aileron_up_limit = 25aileron_down_limit = 25rudder_limit = 45.0elevator_trim_limit = 20spoiler_limit = 35aileron_to_spoileron_gain = 0.5min_ailerons_for_spoilerons = 10.0min_flaps_for_spoilerons = 0.0spoilerons_available = 1[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 60electric_always_available = 0flap_motor = 0, 5, 17gear_motor = 0, 5, 17autopilot = 0, 5, 17avionics_bus = 0, 10, 17avionics = 1, 5, 17pitot_heat = 0, 2, 17additional_system = 0, 20, 17marker_beacon = 1, 2, 17gear_warning = 0, 2, 17fuel_pump = 0, 5, 17starter1 = 0, 20, 17light_nav = 0, 5, 17light_beacon = 0, 5, 17light_landing = 0, 5, 17light_taxi = 0, 5, 17light_strobe = 0, 5, 17light_panel = 0, 5, 17[flight_tuning]cruise_lift_scalar=0.8 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=0.005 //Gain on fuel flowinlet_area=70.0 //Square Feet, engine nacelle inlet arearated_N2_rpm=29920 //RPM, second stage compressor rated valuestatic_thrust=68600 //Lbs, max rated static thrust at Sea Levelafterburner_available=0 //Afterburner available?reverser_available=1 //Thrust reverser available?[jet_engine]thrust_scalar=1.0 [Views]eyepoint=90.0, -2.65, 8.6 [flaps.0] //Inboard Trailing Edgetype = 1span-outboard = 1.0extending-time = 20system_type = 1 //Hydraulicflaps-position.0 = 0 flaps-position.1 = 8flaps-position.2 = 14flaps-position.3 = 18flaps-position.4 = 22flaps-position.5 = 32damaging-speed = 240 blowout-speed = 260 lift_scalar = 1.25drag_scalar = 1.25pitch_scalar= 1.25 [Flaps.1]type = 1span-outboard = 1.0extending-time = 20system_type = 1flaps-position.0 = 0 flaps-position.1 = 2flaps-position.2 = 8flaps-position.3 = 14flaps-position.4 = 22flaps-position.5 = 32damaging-speed = 240 blowout-speed = 260 lift_scalar = 0.7drag_scalar = 1.0pitch_scalar= 1.0 //Hydraulic[Radios]// Radio Type = availiable, standby frequency, has glide slopeAudio.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 = 4direction_indicator.0=3,0 [exits]number_of_exits = 2exit_rate.0 = 0.4 ;Percent per secondexit_rate.1 = 0.4 ;Percent per second[Reference Speeds]flaps_up_stall_speed=155.0 //Knots True (KTAS)full_flaps_stall_speed=115.0 //Knots True (KTAS)cruise_speed=460.0 //Knots True (KTAS)max_indicated_speed=350.000000max_mach=0.860000[autopilot]autopilot_available=1 flight_director_available=1 default_vertical_speed=1200.0 autothrottle_available=1 autothrottle_arming_required= 1autothrottle_max_rpm = 90autothrottle_takeoff_ga= 1pitch_takeoff_ga=8 max_pitch=10.000000max_pitch_acceleration=1.000000max_pitch_velocity_lo_alt=2.000000max_pitch_velocity_hi_alt=1.500000max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=35.000000max_bank_acceleration=1.800000max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[brakes]toe_brakes_scale=0.5parking_brake=1[gear_warning_system]gear_warning_available=1pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=5.042029[hydraulic_system]electric_pumps=0engine_map=1,1,0,0normal_pressure=3000.000000[stall_warning]type=1[attitude_indicators]attitude_indicator.0=1[turn_indicators]turn_indicator.0=1,0/////////////////////////////////////////////////////// FDE v2.0 by Mikael NANOU made for AI A330-300 PW only [General]atc_type=Airbus atc_model=A330 editable=0 performance=Cruise Speed nMach 0.84 555 mph 893 kmhnnEngine options nP&W 4000nRR Trent 800nGE 90 seriesnnMaximum Range n5,960 nm 6,859 sm 11,038 kmnnService Ceiling n42,000 ft 12,800 mnnFuel Capacity n45,220 U.S. gal 171,160 L nnMaximum Takeoff Weight n660,000 lb 299,370 kgnnLength n242 ft, 4 in 73.9 mnnWingspan n199 ft, 11 in 60.9 mnnHeight n60 ft, 8 in 18.5 mnnSeating nSeats 386 to 550 nnCargo Capacity n7,552 ft 213.8 mn [weight_and_balance]// ACM V2.3max_gross_weight = 515700empty_weight = 274500reference_datum_position = 0, 0, 0empty_weight_CG_position = -2.5, 0, 0empty_weight_pitch_MOI = 15351477empty_weight_roll_MOI = 6126019empty_weight_yaw_MOI = 15506700empty_weight_coupled_MOI = 2000max_number_of_stations = 2station_load.0 = 3000, -24.75, 0, 1.04station_load.1 = 400, 95.30, 0, 3.45[lights]//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landinglight.0 = 1, 3.00, 0.00, -10.40, fx_beaconb ,light.1 = 1, 52.00, 0.00, 9.90, fx_beaconh ,light.2 = 1, 3.00, 0.00, -10.40, fx_beaconb ,light.3 = 1, 52.00, 0.00, 9.90, fx_beaconh ,[GeneralEngineData]//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turbopropengine_type = 1fuel_flow_scalar = 1engine.0 = 10.5, -32.6, -8.4engine.1 = 10.5, 32.6, -8.4min_throttle_limit=-0.250000[effects]wake = fx_wakewater = fx_spraydirt = fx_tchdrtconcrete = fx_sparkstouchdown = fx_tchdwn, 1[fuel]//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)fuel_type = 2number_of_tank_selectors = 1Center1 = 0, 0, -4, 7670, 3LeftMain = 6.13, -22.81, 0, 9000, 3RightMain = 7.63, 22.81, 0, 9000, 3electric_pump=0[contact_points]static_pitch = -0.5static_cg_height = 16.56max_number_of_points = 7point.0 = 1, 80.9927, 0, -16.2516, 1581.1, 0, 1.8, 90, 0.63, 2.5, 0.7235, 4, 4, 0, 210, 250point.1 = 1, -4.737, -18.0013, -17.6242, 2574.8, 1, 2.2, 0, 1.21, 2.5, 0.547, 6.9, 6.9, 2, 210, 250point.2 = 1, -4.782, 18.2621, -17.6628, 2574.8, 2, 2.2, 0, 1.21, 2.5, 0.547, 7.1, 7.1, 3, 210, 250point.3 = 2, -39.8568, -102.1276, 13.5122, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0point.4 = 2, -39.4636, 101.6704, 13.1292, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0point.5 = 2, -103.6883, -0.2626, 36.4766, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0point.6 = 2, 102.7405, 0, -1.2679, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0gear_system_type=0[keyboard_response]elevator = 150, 250aileron = 150, 250rudder = 150, 250[forcefeedback]gear_bump_nose_magnitude = 3000gear_bump_nose_direction = 18000gear_bump_nose_duration = 250000gear_bump_left_magnitude = 2700gear_bump_left_direction = 35500gear_bump_left_duration = 250000gear_bump_right_magnitude = 2700gear_bump_right_direction = 00500gear_bump_right_duration = 250000ground_bumps_magnitude1 = 1300ground_bumps_angle1 = 08900ground_bumps_intercept1 = 3.0ground_bumps_slope1 = 0.20ground_bumps_magnitude2 = 200ground_bumps_angle2 = 09100ground_bumps_intercept2 = 1.075ground_bumps_slope2 = 0.035crash_magnitude1 = 10000crash_direction1 = 01000crash_magnitude2 = 10000crash_direction2 = 9000crash_period2 = 75000crash_duration2 = 2500000[airplane_geometry]//ACM_AREAW1// 3.1998,3.1998,2.1533,14.3210,5.6757,5.6757,3.5490,14.4721,7.7480,7.7480//ACM_AREAW2// 4.8892,14.5179,9.5812,9.5812,6.1392,14.6391,14.5843,14.5843,9.1087,16.3617//ACM_AREAW3// 17.3742,17.3742,10.9423,17.2325,23.2297,23.2297,14.8241,19.3602,26.0946,26.0946//ACM_AREAW4// 16.8521,20.5006,29.1688,29.1688,19.3426,21.7754,29.8463,29.8463,20.1068,22.0230//ACM_AREAH1// 0.6074,0.6074,4.6015,5.4935,1.3794,1.3794,0.8162,5.8572,2.5504,2.5504//ACM_AREAH2// 1.3186,6.1609,3.5559,3.5559,2.0978,6.5247,4.5015,4.5015,2.5773,6.8884//ACM_AREAH3// 5.4471,5.4471,3.2967,7.0721,6.2726,6.2726,3.8361,7.3161,7.2782,7.2782//ACM_AREAH4// 4.5555,7.6198,9.1230,9.1230,5.9341,8.1034,9.8288,9.8288,7.0131,8.4671//ACM_AREAV1// 0,0,0,8.5340,1.1073,1.1073,1.4907,8.5466,1.8169,1.8169//ACM_AREAV2// 2.4247,8.8774,2.6061,2.6061,2.8814,8.9694,3.4749,3.4749,3.8949,9.2208//ACM_AREAV3// 4.3435,4.3435,4.5107,9.3927,5.0531,5.0531,5.2059,9.8823,6.0809,6.0809//ACM_AREAV4// 6.1399,10.4518,6.8702,6.8702,6.9945,10.7826,8.0571,8.0571,8.4055,11.0339//ACM_CAREAW1// 3.1689,3.1689,13.0872,14.2601,9.2698,9.2698,13.4847,14.6639,11.2594,11.2594//ACM_CAREAW2// 14.0521,15.1588,15.1877,15.1877,15.3327,16.5522,17.8353,17.8353,16.3092,17.4023//ACM_CAREAW3// 19.2856,19.2856,16.8605,17.8808,20.5706,20.5706,17.2621,18.2290,22.1159,22.1159//ACM_CAREAW4// 17.8033,18.9134,23.5251,23.5251,18.5153,19.5324,29.8614,29.8614,21.0650,22.0606//ACM_CAREAH1// 0.5393,0.5393,3.9156,5.7333,1.5448,1.5448,4.3951,5.8551,2.3106,2.3106//ACM_CAREAH2// 4.6946,6.1567,3.4361,3.4361,4.9345,6.5784,4.7413,4.7413,5.1142,6.8803//ACM_CAREAH3// 5.7466,5.7466,5.5939,7.3017,6.7522,6.7522,5.6539,7.5437,7.8175,7.8175//ACM_CAREAH4// 6.3730,7.9053,8.7629,8.7629,6.6729,8.1471,9.7686,9.7686,7.0925,8.5684//ACM_CAREAV1// -0.3562,-0.3562,7.1862,7.6314,0.0410,0.0410,5.8263,7.8411,1.3457,1.3457//ACM_CAREAV2// 6.4745,8.4069,2.8122,2.8122,7.2845,8.9729,3.6633,3.6633,7.7385,9.3767//ACM_CAREAV3// 4.6441,4.6441,8.2572,9.7810,5.3976,5.3976,8.7110,10.1203,6.3786,6.3786//ACM_CAREAV4// 9.2297,10.5242,7.2621,7.2621,9.7158,10.9280,8.0804,8.0804,10.2993,11.2995wing_area = 3892wing_span = 197.10wing_root_chord = 37.25wing_dihedral = 8.18wing_incidence = 0.0wing_twist = 0.0oswald_efficiency_factor = 0.625wing_winglets_flag = 1wing_sweep = 32.40wing_pos_apex_lon = 36.00wing_pos_apex_vert = -6.26htail_area = 933htail_span = 61.43htail_pos_lon = -81.58htail_pos_vert = 6.51htail_incidence = 0.0htail_sweep = 31.70vtail_area = 650.0vtail_span = 26.17vtail_sweep = 45.18vtail_pos_lon = -70.76vtail_pos_vert = 10.60elevator_area = 95.0aileron_area = 39.0rudder_area = 155.0elevator_up_limit = 30elevator_down_limit = 18aileron_up_limit = 25aileron_down_limit = 25rudder_limit = 45.0elevator_trim_limit = 20spoiler_limit = 35aileron_to_spoileron_gain = 0.5min_ailerons_for_spoilerons = 10.0min_flaps_for_spoilerons = 0.0spoilerons_available = 1[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 60electric_always_available = 0flap_motor = 0, 5, 17gear_motor = 0, 5, 17autopilot = 0, 5, 17avionics_bus = 0, 10, 17avionics = 1, 5, 17pitot_heat = 0, 2, 17additional_system = 0, 20, 17marker_beacon = 1, 2, 17gear_warning = 0, 2, 17fuel_pump = 0, 5, 17starter1 = 0, 20, 17light_nav = 0, 5, 17light_beacon = 0, 5, 17light_landing = 0, 5, 17light_taxi = 0, 5, 17light_strobe = 0, 5, 17light_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=0.005 //Gain on fuel flowinlet_area=54.5 //Square Feet, engine nacelle inlet arearated_N2_rpm=29920 //RPM, second stage compressor rated valuestatic_thrust=42000 //Lbs, max rated static thrust at Sea Levelafterburner_available=0 //Afterburner available?reverser_available=1 //Thrust reverser available?[jet_engine]thrust_scalar=1.0 [Views]eyepoint=90.0, -2.65, 8.6 [flaps.0] //Inboard Trailing Edgetype = 1 // 1 - tail, 2 - leadspan-outboard = 0.2 // 0.0 .. 1.0extending-time = 25 // secondsflaps-position.0 = 0 // degreesflaps-position.1 = 0 // degreesflaps-position.2 = 5 // degreesflaps-position.3 = 15 // degreesflaps-position.4 = 20 // degreesflaps-position.5 = 25 // degreesflaps-position.6 = 30 // degreesdamaging-speed = 240 // KIASblowout-speed = 260 // KIASlift_scalar = 0.55drag_scalar = 0.55pitch_scalar= 0.55system_type = 1 //Hydraulic[flaps.1] //Outboard Trailing Edgetype = 1 // 1 - tail, 2 - leadspan-outboard = 0.8 // 0.0 .. 1.0extending-time = 23 // secondsflaps-position.0 = 0 // degreesflaps-position.1 = 0 // degreesflaps-position.2 = 5 // degreesflaps-position.3 = 15 // degreesflaps-position.4 = 20 // degreesflaps-position.5 = 25 // degreesflaps-position.6 = 30 // degreesdamaging-speed = 240 // KIASblowout-speed = 260 // KIASlift_scalar = 0.605drag_scalar = 0.605pitch_scalar= 0.605system_type = 1 //Hydraulic[flaps.2] //Inboard Leading Edge Slatstype = 2 // 1 - tail, 2 - leadspan-outboard = 0.5 // 0.0 .. 1.0extending-time = 4 // secondsflaps-position.0 = 0 // degreesflaps-position.1 = 0.5 // degreesflaps-position.2 = 0.5 // degreesflaps-position.3 = 0.5 // degreesflaps-position.4 = 0.5 // degreesflaps-position.5 = 1.0 // degreesflaps-position.6 = 1.0 // degreesdamaging-speed = 260 // KIASblowout-speed = 300 // KIASlift_scalar = 0.605drag_scalar = 0.405pitch_scalar= 0.05system_type = 1 //Hydraulic[Radios]// Radio Type = availiable, standby frequency, has glide slopeAudio.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 = 4direction_indicator.0=3,0 [exits]number_of_exits = 2exit_rate.0 = 0.4 ;Percent per secondexit_rate.1 = 0.4 ;Percent per second[Reference Speeds]flaps_up_stall_speed=155.0 //Knots True (KTAS)full_flaps_stall_speed=115.0 //Knots True (KTAS)cruise_speed=460.0 //Knots True (KTAS)max_indicated_speed=330.000000max_mach=0.860000[autopilot]autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=1 autothrottle_arming_required= 1autothrottle_max_rpm = 90autothrottle_takeoff_ga= 1pitch_takeoff_ga=8 max_pitch=10.000000max_pitch_acceleration=1.000000max_pitch_velocity_lo_alt=2.000000max_pitch_velocity_hi_alt=1.500000max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=35.000000max_bank_acceleration=1.800000max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[brakes]toe_brakes_scale=0.5parking_brake=1[gear_warning_system]gear_warning_available=1pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=5.042029[hydraulic_system]electric_pumps=1engine_map=1,1,0,0normal_pressure=3000.000000[stall_warning]type=1[attitude_indicators]attitude_indicator.0=1[turn_indicators]turn_indicator.0=1,0/////////////////////////////////////////////// FDE v2.0 by Mikael NANOU made for AI A330-300 RR only [General]atc_type=Airbus atc_model=A330 editable=0 performance=Cruise Speed nMach 0.84 555 mph 893 kmhnnEngine options nP&W 4000nRR Trent 800nGE 90 seriesnnMaximum Range n5,960 nm 6,859 sm 11,038 kmnnService Ceiling n42,000 ft 12,800 mnnFuel Capacity n45,220 U.S. gal 171,160 L nnMaximum Takeoff Weight n660,000 lb 299,370 kgnnLength n242 ft, 4 in 73.9 mnnWingspan n199 ft, 11 in 60.9 mnnHeight n60 ft, 8 in 18.5 mnnSeating nSeats 386 to 550 nnCargo Capacity n7,552 ft 213.8 mn [weight_and_balance]// ACM V2.3max_gross_weight = 512350empty_weight = 270850reference_datum_position = 0, 0, 0empty_weight_CG_position = -2.5, 0, 0empty_weight_pitch_MOI = 15147350empty_weight_roll_MOI = 6044562empty_weight_yaw_MOI = 15300509empty_weight_coupled_MOI = 2000max_number_of_stations = 2station_load.0 = 3000, -23.15, 0, 0.22station_load.1 = 400, 95.30, 0, 3.45[lights]//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landinglight.0 = 2, -102.38, 12.26, 6.76, fx_navwhilight.1 = 1, 52.00, 0.00, 9.90, fx_beaconh ,light.2 = 1, 9.52, 0, -10.39, fx_beaconb[GeneralEngineData]//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turbopropengine_type = 1fuel_flow_scalar = 1engine.0 = 10.5, -32.6, -8.4engine.1 = 10.5, 32.6, -8.4min_throttle_limit=-0.250000[effects]wake = fx_wakewater = fx_spraydirt = fx_tchdrtconcrete = fx_sparkstouchdown = fx_tchdwn, 1[fuel]//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)fuel_type = 2number_of_tank_selectors = 1Center1 = 0, 0, -4, 7670, 3LeftMain = 6.31, -22.15, 0, 9000, 3RightMain = 6.31, 22.15, 0, 9000, 3electric_pump=0[contact_points]static_pitch = -0.5static_cg_height = 16.56max_number_of_points = 7point.0 = 1, 80.9927, 0, -16.2516, 1581.1, 0, 1.8, 90, 0.63, 2.5, 0.7235, 4, 4, 0, 210, 250point.1 = 1, -4.737, -18.0013, -17.6242, 2574.8, 1, 2.2, 0, 1.21, 2.5, 0.547, 6.9, 6.9, 2, 210, 250point.2 = 1, -4.782, 18.2621, -17.6628, 2574.8, 2, 2.2, 0, 1.21, 2.5, 0.547, 7.1, 7.1, 3, 210, 250point.3 = 2, -39.8568, -102.1276, 13.5122, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0point.4 = 2, -39.4636, 101.6704, 13.1292, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0point.5 = 2, -102.6391, -0.2626, 7.1693, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0point.6 = 2, 102.7405, 0, -1.2679, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0gear_system_type=0[keyboard_response]elevator = 150, 250aileron = 150, 250rudder = 150, 250[forcefeedback]gear_bump_nose_magnitude = 3000gear_bump_nose_direction = 18000gear_bump_nose_duration = 250000gear_bump_left_magnitude = 2700gear_bump_left_direction = 35500gear_bump_left_duration = 250000gear_bump_right_magnitude = 2700gear_bump_right_direction = 00500gear_bump_right_duration = 250000ground_bumps_magnitude1 = 1300ground_bumps_angle1 = 08900ground_bumps_intercept1 = 3.0ground_bumps_slope1 = 0.20ground_bumps_magnitude2 = 200ground_bumps_angle2 = 09100ground_bumps_intercept2 = 1.075ground_bumps_slope2 = 0.035crash_magnitude1 = 10000crash_direction1 = 01000crash_magnitude2 = 10000crash_direction2 = 9000crash_period2 = 75000crash_duration2 = 2500000[airplane_geometry]//ACM_AREAW1// 3.1998,3.1998,2.1533,14.3210,5.6757,5.6757,3.5490,14.4721,7.7480,7.7480//ACM_AREAW2// 4.8892,14.5179,9.5811,9.5811,6.1392,14.6391,14.5843,14.5843,9.1085,16.3617//ACM_AREAW3// 17.3742,17.3742,10.9421,17.2325,23.2297,23.2297,14.8240,19.3602,26.0946,26.0946//ACM_AREAW4// 16.8521,20.5006,29.1688,29.1688,19.3425,21.7754,29.8463,29.8463,20.1068,22.0230//ACM_AREAH1// 0.6074,0.6074,4.6015,5.4935,1.3794,1.3794,0.8162,5.8572,2.5504,2.5504//ACM_AREAH2// 1.3186,6.1609,3.5559,3.5559,2.0978,6.5247,4.5015,4.5015,2.5773,6.8884//ACM_AREAH3// 5.4471,5.4471,3.2967,7.0721,6.2726,6.2726,3.8361,7.3161,7.2782,7.2782//ACM_AREAH4// 4.5555,7.6198,9.1230,9.1230,5.9341,8.1034,9.8288,9.8288,7.0131,8.4671//ACM_AREAV1// 0,0,0,8.5340,1.1073,1.1073,1.4907,8.5466,1.8169,1.8169//ACM_AREAV2// 2.4247,8.8774,2.6061,2.6061,2.8814,8.9694,3.4749,3.4749,3.8949,9.2208//ACM_AREAV3// 4.3435,4.3435,4.5107,9.3927,5.0531,5.0531,5.2059,9.8823,6.0809,6.0809//ACM_AREAV4// 6.1399,10.4518,6.8702,6.8702,6.9945,10.7826,8.0571,8.0571,8.4055,11.0339//ACM_CAREAW1// 3.1689,3.1689,13.0872,14.2601,9.2698,9.2698,13.4847,14.6639,11.2594,11.2594//ACM_CAREAW2// 14.0521,15.1588,15.1877,15.1877,15.3325,16.5522,17.8353,17.8353,16.3092,17.4022//ACM_CAREAW3// 19.2856,19.2856,16.8605,17.8808,20.5706,20.5706,17.2621,18.2290,22.1159,22.1159//ACM_CAREAW4// 17.8033,18.9134,23.5251,23.5251,18.5153,19.5324,29.8614,29.8614,21.0650,22.0606//ACM_CAREAH1// 0.5393,0.5393,3.9156,5.7333,1.5448,1.5448,4.3951,5.8551,2.3106,2.3106//ACM_CAREAH2// 4.6946,6.1567,3.4361,3.4361,4.9345,6.5784,4.7413,4.7413,5.1142,6.8803//ACM_CAREAH3// 5.7466,5.7466,5.5939,7.3017,6.7522,6.7522,5.6539,7.5437,7.8175,7.8175//ACM_CAREAH4// 6.3730,7.9053,8.7629,8.7629,6.6729,8.1471,9.7686,9.7686,7.0925,8.5684//ACM_CAREAV1// -0.3562,-0.3562,7.1862,7.6314,0.0410,0.0410,5.8263,7.8411,1.3457,1.3457//ACM_CAREAV2// 6.4745,8.4069,2.8122,2.8122,7.2845,8.9729,3.6633,3.6633,7.7385,9.3767//ACM_CAREAV3// 4.6441,4.6441,8.2572,9.7810,5.3976,5.3976,8.7110,10.1203,6.3786,6.3786//ACM_CAREAV4// 9.2297,10.5242,7.2621,7.2621,9.7158,10.9280,8.0804,8.0804,10.2993,11.2995wing_area = 3892wing_span = 197.10wing_root_chord = 37.25wing_dihedral = 8.18wing_incidence = 0.0wing_twist = 0.0oswald_efficiency_factor = 0.625wing_winglets_flag = 1wing_sweep = 32.40wing_pos_apex_lon = 36.00wing_pos_apex_vert = -6.26htail_area = 933htail_span = 61.43htail_pos_lon = -81.58htail_pos_vert = 6.51htail_incidence = 0.0htail_sweep = 31.70vtail_area = 650.0vtail_span = 26.17vtail_sweep = 45.18vtail_pos_lon = -70.76vtail_pos_vert = 10.60elevator_area = 95.0aileron_area = 39.0rudder_area = 155.0elevator_up_limit = 30elevator_down_limit = 18aileron_up_limit = 25aileron_down_limit = 25rudder_limit = 45.0elevator_trim_limit = 20spoiler_limit = 35aileron_to_spoileron_gain = 0.5min_ailerons_for_spoilerons = 10.0min_flaps_for_spoilerons = 0.0spoilerons_available = 1[electrical]max_battery_voltage = 24generator_alternator_voltage = 28max_generator_alternator_amps = 60electric_always_available = 0flap_motor = 0, 5, 17gear_motor = 0, 5, 17autopilot = 0, 5, 17avionics_bus = 0, 10, 17avionics = 1, 5, 17pitot_heat = 0, 2, 17additional_system = 0, 20, 17marker_beacon = 1, 2, 17gear_warning = 0, 2, 17fuel_pump = 0, 5, 17starter1 = 0, 20, 17light_nav = 0, 5, 17light_beacon = 0, 5, 17light_landing = 0, 5, 17light_taxi = 0, 5, 17light_strobe = 0, 5, 17light_panel = 0, 5, 17[flight_tuning]cruise_lift_scalar=0.8 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 flowinlet_area=51.7 //Square Feet, engine nacelle inlet arearated_N2_rpm=29990 //RPM, second stage compressor rated valuestatic_thrust=71100 //Lbs, max rated static thrust at Sea Levelafterburner_available=0 //Afterburner available?reverser_available=1 //Thrust reverser available?[jet_engine]thrust_scalar=1.0 [Views]eyepoint=90.0, -2.65, 8.6 [flaps.0] //Inboard Trailing Edgetype = 1 // 1 - tail, 2 - leadspan-outboard = 0.2 // 0.0 .. 1.0extending-time = 25 // secondsflaps-position.0 = 0 // degreesflaps-position.1 = 0 // degreesflaps-position.2 = 5 // degreesflaps-position.3 = 15 // degreesflaps-position.4 = 20 // degreesflaps-position.5 = 25 // degreesflaps-position.6 = 30 // degreesdamaging-speed = 240 // KIASblowout-speed = 260 // KIASlift_scalar = 1.05drag_scalar = 1.05pitch_scalar= 1.05system_type = 1 //Hydraulic[flaps.1] //Outboard Trailing Edgetype = 1 // 1 - tail, 2 - leadspan-outboard = 0.8 // 0.0 .. 1.0extending-time = 23 // secondsflaps-position.0 = 0 // degreesflaps-position.1 = 0 // degreesflaps-position.2 = 5 // degreesflaps-position.3 = 15 // degreesflaps-position.4 = 20 // degreesflaps-position.5 = 25 // degreesflaps-position.6 = 30 // degreesdamaging-speed = 260 // KIASblowout-speed = 300 // KIASlift_scalar = 0.605drag_scalar = 0.605pitch_scalar= 0.605system_type = 1 //Hydraulic[flaps.2] //Inboard Leading Edge Slatstype = 2 // 1 - tail, 2 - leadspan-outboard = 0.5 // 0.0 .. 1.0extending-time = 4 // secondsflaps-position.0 = 0 // degreesflaps-position.1 = 0.5 // degreesflaps-position.2 = 0.5 // degreesflaps-position.3 = 0.5 // degreesflaps-position.4 = 0.5 // degreesflaps-position.5 = 1.0 // degreesflaps-position.6 = 1.0 // degreesdamaging-speed = 260 // KIASblowout-speed = 300 // KIASlift_scalar = 0.605drag_scalar = 0.405pitch_scalar= 0.05system_type = 1 //Hydraulic[Radios]// Radio Type = availiable, standby frequency, has glide slopeAudio.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 = 4direction_indicator.0=3,0 [exits]number_of_exits = 2exit_rate.0 = 0.4 ;Percent per secondexit_rate.1 = 0.4 ;Percent per second[Reference Speeds]flaps_up_stall_speed=155.0 //Knots True (KTAS)full_flaps_stall_speed=115.0 //Knots True (KTAS)cruise_speed=470.0 //Knots True (KTAS)max_indicated_speed=330.000000max_mach=0.860000[autopilot]autopilot_available=1 flight_director_available=1 default_vertical_speed=1500.0 autothrottle_available=1 autothrottle_arming_required= 1autothrottle_max_rpm = 90autothrottle_takeoff_ga= 1pitch_takeoff_ga=8 max_pitch=08.000000max_pitch_acceleration=1.000000max_pitch_velocity_lo_alt=2.000000max_pitch_velocity_hi_alt=1.500000max_pitch_velocity_lo_alt_breakpoint=20000.000000max_pitch_velocity_hi_alt_breakpoint=28000.000000max_bank=35.000000max_bank_acceleration=1.800000max_bank_velocity=3.000000max_throttle_rate=0.100000nav_proportional_control=9.000000nav_integrator_control=0.250000nav_derivative_control=0.000000nav_integrator_boundary=2.500000nav_derivative_boundary=0.000000gs_proportional_control=9.520000gs_integrator_control=0.260000gs_derivative_control=0.000000gs_integrator_boundary=0.700000gs_derivative_boundary=0.000000yaw_damper_gain=0.000000[brakes]toe_brakes_scale=0.5parking_brake=1[gear_warning_system]gear_warning_available=1pct_throttle_limit=0.099976flap_limit_power=25.496622flap_limit_idle=5.042029[hydraulic_system]electric_pumps=1engine_map=1,1,0,0normal_pressure=3000.000000[stall_warning]type=1[attitude_indicators]attitude_indicator.0=1[turn_indicators]turn_indicator.0=1,0

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Mistake : the static thrust of the pw is 72000 instead of 42000

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