[fltsim.0] title=Airbus A340-313E Aigle Azur Rafik B sim=Airbus_a330_300 model= panel= sound= texture= checklists= atc_airline=Aigle Azur atc_id=7T-VKN atc_flight_number=1 atc_heavy=1 atc_parking_types=GATE, RAMP, CARGO atc_parking_code=KZW ui_manufacturer=Airbus ui_type=A340-300 ui_variation=Aigle Azur Rafik Pilot visual_damage=1 description=Airbus 340-313E High Gross\nVersion 2004.8.1\n\nFSx \n\nEngine Type: GE CFM56-5C4/P\n\nModel Designer\n Shervin Ahooraei\n\nFlight Dynamics Designer\n Warren C. Daniel\n\nMaster Texture Designer\n Rafik B.\n\nTechnical Resource\n Simon Ng\n\nTest Pilots\n brafik2001@hotmail.com [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations= 8 station_load.0 = "2100.0, 60.0, 0.0, 4.0, First Class (12 pax)" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "7345.0, 40.0, 0.0, 4.0, Business Class (42 pax)" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "42175.0, 0.0, 0.0, 4.0, Tourist Class (241 pax)" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = "1090.0, 70.0, 0.0, 4.0, Fwd Galley" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = "2000.0, 20.0, 0.0, 4.0, Center Galley" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = "1726.0, 0.0, 0.0, 4.0, Aft Galley" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = "31500.0, 40.0, 0.0, -3.0, Fwd Cargo Compt (2844 cu ft)" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7 = "24500.0, 0.0, 0.0, -3.0, Aft Cargo Compt (2212 cu ft)" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) empty_weight= 298311.000 max_gross_weight= 618750.000 // Total A340-300 High Gross Max Structural Payload per Airbus = 112,436 lb // Opensky Total A340-300 Total Possible Payload = 112,436 lb empty_weight_roll_MOI= 9146509.000 empty_weight_pitch_MOI= 16143375.000 empty_weight_yaw_MOI= 26494495.000 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =1.000 induced_drag_scalar =1.000 elevator_effectiveness =1.200 aileron_effectiveness =1.500 rudder_effectiveness =2.500 pitch_stability =1.500 roll_stability =1.000 yaw_stability =1.000 elevator_trim_effectiveness =1.000 aileron_trim_effectiveness =1.000 rudder_trim_effectiveness =1.000 [pitot_static] vertical_speed_time_constant=999 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.000000 [fuel] Center1= 0.000, 0.000, -4.000, 11210.000, 3.000 Center2= -83.676, 0.000, 0.000, 1650.000, 3.000 Center3= 3.000, 0.000, -4.000, 1814.500, 3.000 LeftMain= -7.000, -37.983, 0.000, 11303.000, 3.000 RightMain= -7.000, 37.983, 0.000, 11303.000, 3.000 LeftAux= -13.000, -70.269, 0.000, 970.000, 3.000 RightAux= -13.000, 70.269, 0.000, 970.000, 3.000 fuel_type= 2.000 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors= 1 electric_pump=1 [airplane_geometry] wing_area= 3892.000 wing_span= 197.833 wing_root_chord= 25.000 wing_dihedral= 6.218 wing_incidence= 0.750 wing_twist= -0.500 oswald_efficiency_factor= 0.600 wing_winglets_flag= 1 wing_sweep= 30.000 wing_pos_apex_lon= 30.000 wing_pos_apex_vert= 0.000 htail_area= 1050.000 htail_span= 69.700 htail_pos_lon= -85.100 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 40.000 vtail_area= 690.000 vtail_span= 27.300 vtail_sweep= 35.000 vtail_pos_lon= -79.576 vtail_pos_vert= 5.800 elevator_area= 137.000 aileron_area= 68.000 rudder_area= 232.000 elevator_up_limit= 15.000 elevator_down_limit= 30.000 aileron_up_limit= 25.000 aileron_down_limit= 25.000 rudder_limit= 31.350 elevator_trim_limit= 15.000 spoiler_limit= 35.000 spoilerons_available= 0 aileron_to_spoileron_gain= 3.000 min_ailerons_for_spoilerons= 9.969 min_flaps_for_spoilerons= 0.000 auto_spoiler_available=1 spoiler_extension_time=2.000000 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 [GeneralEngineData] engine_type= 1 Engine.0= -10.000, -64.300, -2.413 Engine.1= 10.000, -30.900, -5.583 Engine.2= 10.000, 30.900, -5.583 Engine.3= -10.000, 64.300, -2.413 fuel_flow_scalar= 0.750 min_throttle_limit=-0.229907 // Basic engine information - thrust/Bypass ratio // CFM56-5C2 - 31,200 lbs/6.6 // CFM56-5C3 - 32,500 lbs/6.5 // CFM56-5C4 - 34,000 lbs/6.4 [TurbineEngineData] bypass_ratio=6.4 fuel_flow_gain= 0.001 inlet_area= 28.496 rated_N2_rpm= 29920.000 static_thrust= 34000.000 afterburner_available= 0 reverser_available= 1 [jet_engine] thrust_scalar=1.070 [Reference Speeds] flaps_up_stall_speed= 132.000 full_flaps_stall_speed= 124.000 cruise_speed= 460.000 max_indicated_speed=330.000000 max_mach=0.860010 [keyboard_response] elevator= 100.000, 200.000 aileron= 100.000, 200.000 rudder= 100.000, 200.000 [Views] eyepoint= 78.9, -1.756, 8.1 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 800.000 autothrottle_available= 1 autothrottle_arming_required= 1 autothrottle_takeoff_ga= 1 autothrottle_max_rpm= 100.30 pitch_takeoff_ga= 0.000 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. 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=0.300000 max_pitch_velocity_lo_alt_breakpoint= 7000.000000 max_pitch_velocity_hi_alt_breakpoint=24000.000000 max_bank=30.000000 max_bank_acceleration=1.050000 max_bank_velocity=2.000000 max_throttle_rate=0.050000 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=1.000000 [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] direction_indicator.0=3,0 [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) //Nose Gear point.0= 1.000, 74.443, 0.000, -11.500, 1181.102, 0.000, 4.845, 72.000, 1.000, 1.400, 0.510, 7.000, 9.000, 0.000, 280.000, 300.000 point.1= 1.000, -13.500, -17.750, -12.300, 1574.803, 2.000, 2.450, -8.000, 0.700, 0.800, 0.550, 10.600, 11.800, 2.000, 280.000, 300.000 point.2= 1.000, -13.500, 17.750, -12.300, 1574.803, 1.000, 2.450, -8.000, 0.700, 0.800, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000 //point.3= 1.000, -11.067, 0.000, -12.500, 1574.803, 0.000, 4.845, -8.000, 1.000, 1.400, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000 point.4= 2.000, -14.167, -84.717, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.5= 2.000, -14.167, 91.817, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.6= 2.000, -120.667, 0.000, 6.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.7= 2.000, 78.417, 0.000, -3.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.8= 2.000, 14.167, -99.917, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000 point.9= 2.000, 0.000, 44.750, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 static_pitch= -2.000 static_cg_height= 10.560 gear_system_type=0 //Nose Gear //point.0= 1.000, 74.443, -2.000, -11.500, 1181.102, 0.000, 4.845, 72.000, 1.000, 2.400, 0.510, 7.000, 9.000, 0.000, 280.000, 300.000 //point.1= 1.000, 74.443, 2.000, -11.500, 1181.102, 0.000, 4.845, 72.000, 1.000, 2.400, 0.510, 7.000, 9.000, 0.000, 280.000, 300.000 // //Main Gear (Left) //point.2= 1.000, -11.067, -20.500, -13.500, 1574.803, 1.000, 4.845, -8.000, 2.200, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000 //point.3= 1.000, -11.067, -15.000, -13.500, 1574.803, 1.000, 4.845, -8.000, 2.200, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000 //point.4= 1.000, -6.667, -20.500, -13.200, 1574.803, 1.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000 //point.5= 1.000, -6.667, -15.000, -13.200, 1574.803, 1.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000 // //Main Gear (Right) //point.6= 1.000, -11.067, 20.500, -13.500, 1574.803, 2.000, 4.845, -8.000, 2.200, 2.400, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000 //point.7= 1.000, -11.067, 15.000, -13.500, 1574.803, 2.000, 4.845, -8.000, 2.200, 2.400, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000 //point.8= 1.000, -6.667, 20.500, -13.200, 1574.803, 2.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000 //point.9= 1.000, -6.667, 15.500, -13.200, 1574.803, 2.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000 // // Main Gear (Center) //point.10= 1.000, -11.067, 2.200, -13.200, 1574.803, 0.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 3.000, 280.000, 300.000 //point.11= 1.000, -11.067, -2.200, -13.200, 1574.803, 0.000, 4.845, -8.000, 1.000, 2.400, 0.550, 10.900, 11.900, 2.000, 280.000, 300.000 // // //Scrape Points //point.12= 2.000, -14.167, -84.717, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 //point.13= 2.000, -14.167, 91.817, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 //point.14= 2.000, -120.667, 0.000, 6.500, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //point.15= 2.000, 88.417, 0.000, -3.750, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //point.16= 2.000, 14.167, -99.917, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000 //point.17= 2.000, 0.000, 44.750, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 // //static_pitch= -2.000 //static_cg_height= 11.560 //gear_system_type=0 [LIGHTS] Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 1, 0.000, 0.000, 14.800, Opensky_beacon, light.1 = 1, 8.225, 0.000, -4.800, Opensky_beacon, light.2 = 4, 86.000, 0.000, 1.000, fx_vclight , light.3 = 5, 18.000, 27.000, -4.000, Opensky_wing_light, light.4 = 5, 19.933, 8.826, -4.368, Opensky_wing_light, light.5 = 5, 18.000, -27.000, -4.000, Opensky_wing_light, light.6 = 5, 19.933, -8.826, -5.368, Opensky_wing_light, light.7 = 5, 17.700, 19.000, -1.000, Opensky_nacelle_refl, light.8 = 5, 17.700, -19.000, -1.000, Opensky_nacelle_refl, light.9 = 3, -116.500, 0.000, 11.200, Opensky_nav_yellow , light.10 = 2, -116.500, 0.200, 11.200, fx_strobeh , ;light.11 = 5, 46.250, 9.350, 4.900, Opensky_nav_yellow , ;light.12 = 5, 46.250, -9.350, 4.900, Opensky_nav_yellow , ;light.13 = 5, 47.850, 9.350, 4.900, Opensky_nav_yellow , ;light.14 = 5, 47.850, -9.350, 4.900, Opensky_nav_yellow , [General] performance=Passengers\n3-class conf: 295\n\nCargo\n26\/27 LD3 containers \/ 10 Pallets \n\nTotal lower hold volume: 4,800 cu ft \n\nDimensions\nSpan 197 ft 10 in\nLength 193 ft 7 in\nHeight 54 ft 11 in \n\nEngines: GE CFM56-5C4/P\nTO Thrust Rating: 34,000 lb\n\nMax Fuel Cap.: 39220.50 gal\nMaxTOW: 618,750 lb\nOEW: 298,331 lb\nMax Payload: 112,436 lb\n\nMax Range: 7,200 nm\nTypical Cruise Speed\n @ FL350: M.82 atc_type=AIRBUS atc_model=A340 Category=airplane [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=Opensky_sparks, 1 touchdown=fx_tchdwn, 1 [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 [electrical] // ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot = 0, 5 , 17.0 flap_motor = 1, 0 , 1.0 gear_motor = 0, 5 , 17.0 avionics_bus = 0, 0 , 1.0 avionics = 1, 5 , 17.0 pitot_heat = 0, 0 , 1.0 additional_system = 0, 0 , 1.0 marker_beacon = 1, 2 , 17.0 gear_warning = 7, 0 , 99.0 gear_motor = 4, 0 , 1.0 fuel_pump = 0, 0 , 1.0 fuel_transfer_pump = 0, 0 , 1.0 starter1 = 0, 20, 17.0 starter2 = 0, 0 , 1.0 light_nav = 0, 0 , 1.0 light_beacon = 0, 0 , 1.0 light_landing = 0, 0 , 1.0 light_taxi = 0, 0 , 1.0 light_strobe = 0, 0 , 1.0 light_panel = 0, 7 , 99.0 light_recognition = 0, 0 , 1.0 light_wing = 0, 0 , 1.0 marker_beacon = 0, 0 , 1.0 standby_vacuum = 0, 0 , 1.0 auto_brakes = 0, 0 , 1.0 hydraulic_pump = 0, 0 , 1.0 propeller_device = 0, 0 , 1.0 [Flaps.0] type= 1 span-outboard= 0.800 extending-time= 18.000 system_type= 1 damaging-speed= 200.000 blowout-speed= 250.000 lift_scalar= 1.000 drag_scalar= 1.500 pitch_scalar= 3.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 8.000, 0.000 flaps-position.2= 14.000, 0.000 flaps-position.3= 22.000, 0.000 flaps-position.4= 32.000, 0.000 [Flaps.1] type= 2 span-outboard= 0.800 extending-time= 25.000 system_type= 1 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 1.000 drag_scalar= 1.500 pitch_scalar= 3.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 20.000, 0.000 [brakes] toe_brakes_scale=1.000000 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=1,1,1,1 normal_pressure=3000.000000 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [TailHook] // For opening cargo door. tailhook_length=1 ;(feet) tailhook_position = 0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum [folding_wings] // For opening main deck cargo door. wing_fold_system_type = 4 ;0=None fold_rates = 0.05,0.05 ;Percent per second cable_force_adjust = 1.0 [exits] number_of_exits = 2 exit_rate.0 = 0.2 ;Percent per second exit_rate.1 = 0.1 ;Percent per second [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