[General] atc_type=A340 atc_model=Airbus editable=1 performance=* Weight: 333045 lbs Max 606300 lbs * Power: 34058 lbs thrust * 5.5g Corner speed: 268 mph * Max speed @ SL: 655 mph * Max speed: 560 mph @ 39000 ft * Climb rate: 1763 ft\/min @ 462 mph Flight Model By: AeroDesigns \/ Eugene Shneyder Copyright 2003 Aerodesigns 5\/13\/03 04:51 PM Flight Model Workbook V2.82.98 [pitot_static] vertical_speed_time_constant = 99 [weight_and_balance] // ACM V2.0 max_gross_weight = 606300.000 empty_weight = 287780.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = -17.000, 0.000, 0.000 empty_weight_pitch_MOI = 16152934.000 empty_weight_roll_MOI = 6333130.000 empty_weight_yaw_MOI = 16176219.000 empty_weight_coupled_MOI = 0.000 max_number_of_stations = 6 station_load.0 = 410.000, 82.000, 0.000, 8.890 station_load.1 = 1211.000, -6.000, 0.000, 0.000 station_load.2 = 3075.000, 45.000, 0.000, 0.000 station_load.3 = 5330.000, 15.000, 0.000, 0.000 station_load.4 = 24440.000, -30.000, 0.000, 0.000 station_load.5 = 10799.000, 25.000, 0.000, 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 4, 82.4, 0, 8.28, Aero_vc_light , light.1 = 5, 39, -12.9, -3.2, Aero_scan_light light.2 = 5, 39, 12.9, -3.2, Aero_scan_light light.3 = 1, 17.26, -23.17, -4.83, RNLE2 light.4 = 1, 17.26, 23.17, -4.83, RNLE2 light.5 = 9, -104.4, -5.9, 25.4, RNLE2 light.6 = 9, -104.4, 5.9, 25.4, RNLE2 [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 0.800 engine.0 = -10.000, -66.000, 4.000 engine.1 = 12.000, -31.000, -2.000 engine.2 = 12.000, 31.000, -2.000 engine.3 = -10.000, 66.000, 4.000 min_throttle_limit=-0.319946 [smokesystem] smoke.0 = 3.63, -95, 66.22, Aerodesigns340_Smoke_14 smoke.1 = -2, -80, 30.18, Aerodesigns340_Smoke_23 smoke.2 = -2, -80, -30.04, Aerodesigns340_Smoke_23 smoke.3 = 3.63, -95, -66.22, Aerodesigns340_Smoke_14 [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 = 0.000, 0.000, 0.000, 13636.000, 22.000 Center2 = -102.000, 0.000, 4.000, 642.000, 3.000 LeftMain = -5.000, -17.983, 0.000, 12027.000, 17.000 RightMain = -5.000, 17.983, 0.000, 12027.000, 17.000 electric_pump=1 [contact_points] static_pitch = -1.1 static_cg_height = 12 max_number_of_points = 12 point.0 = 1.000, 67.163, 0.000, -10.200, 1200.000, 0.000, 2.080, 68.000, 0.200, 2.000, 0.700, 8.000, 7.000, 0.000, 0.000, 0.000 point.1 = 1.000, -19.000, 17.550, -12.000, 2000.000, 2.000, 4.845, 0.000, 1.000, 2.500, 0.900, 11.000, 13.000, 2.000, 246.000, 64199128.014 point.2 = 1.000, -19.000, -17.550, -12.000, 2000.000, 1.000, 4.845, 0.000, 0.850, 2.500, 0.900, 14.000, 10.000, 3.000, 246.000, 64199128.014 point.3 = 1.000, -19.000, 0.000, -12.000, 2000.000, 0.000, 4.845, 8.000, 0.850, 2.500, 0.900, 7.000, 8.000, 1.000, 0.000, 0.000 point.4 = 2, -39.6399, -98.6892, 13.4492, 0, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.5 = 2, -10.081, -66.7235, -1.0828, 700, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0 point.6 = 2, 11.6044, -30.3045, -7.3685, 700, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0 point.7 = 2, 11.6975, 30.1788, -7.3534, 700, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0 point.8 = 2, -9.9167, 66.3097, -1.0459, 700, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0 point.9 = 2, -38.8008, 97.7886, 14.0839, 700, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.10 = 2, -68.0447, 0, -6.2084, 700, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.11 = 2.000, 90.117, 0.000, 0.000, 700.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 gear_system_type=1 [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [forcefeedback] gear_bump_nose_magnitude = 6000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 6000 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 6000 gear_bump_right_direction = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 3250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1 crash_magnitude1 = 10000 crash_direction1 = 1000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 [airplane_geometry] wing_area = 3892.000 wing_span = 197.080 wing_root_chord = 19.740 wing_dihedral = 6.300 wing_incidence = 0.900 wing_twist = -0.808 oswald_efficiency_factor = 0.879 wing_winglets_flag = 1 wing_sweep = 30.000 wing_pos_apex_lon = 17.530 wing_pos_apex_vert = 0.000 htail_area = 784.404 htail_span = 76.000 htail_pos_lon = -108.000 htail_pos_vert = 0.000 htail_incidence = -0.680 htail_sweep = 30.000 vtail_area = 486.352 vtail_span = 35.000 vtail_sweep = 44.000 vtail_pos_lon = -106.000 vtail_pos_vert = 0.000 elevator_area = 353.750 aileron_area = 280.900 rudder_area = 155.700 elevator_up_limit = 28.000 elevator_down_limit = 30.000 aileron_up_limit = 25.000 aileron_down_limit = 25.000 rudder_limit = 31.600 elevator_trim_limit = 30.000 spoiler_limit = 56.000 aileron_to_spoileron_gain = 4.000 min_ailerons_for_spoilerons = 8.000 min_flaps_for_spoilerons = 0.000 spoilerons_available = 1 [electrical] //BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot = 0, 5 , 17.0 avionics_bus = 0, 10, 17.0 avionics = 1, 5 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 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 pitot_heat = 0, 15, 17.0 additional_system = 0, 20, 17.0 marker_beacon = 1, 2, 17.0 starter1 = 0, 20, 17.0 starter2 = 0, 20, 17.0 starter3 = 0, 20, 17.0 starter4 = 0, 20, 17.0 auto_brakes = 0, 15, 17.0 hydraulic_pump = 0, 2, 17.0 fuel_transfer_pump = 0, 5, 17.0 max_battery_voltage = 28.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps= 60.0 electric_always_available = 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, 1 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [TurbineEngineData] fuel_flow_gain= 0.002 inlet_area= 11.067 rated_N2_rpm= 31000.000 static_thrust= 34058.000 afterburner_available= 0 reverser_available= 1 [jet_engine] thrust_scalar=1.230 [folding_wings] wing_fold_system_type = 4 fold_rates = 0.12, 0.11 [TailHook] tailhook_length = 4 tailhook_position = -15, 0, -1 cable_force_adjust = 1 [Views] eyepoint=80.4, -1.97, 9 [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 [autopilot] 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=90.000000 pitch_takeoff_ga=8.000000 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=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 = 152.600 full_flaps_stall_speed = 123.800 cruise_speed = 482.000 max_indicated_speed=479.593750 max_mach=0.864990 [Flaps.0] type= 1 span-outboard= 0.650 extending-time= 14.000 system_type= 1 damaging-speed= 284.000 blowout-speed= 291.000 lift_scalar= 0.520 drag_scalar= 1.360 pitch_scalar= 0.300 flaps-position.0= 0.000, 0.000 flaps-position.1= 0.000, 0.000 flaps-position.2= 17.500, 0.000 flaps-position.3= 22.500, 0.000 flaps-position.4= 26.500, 0.000 flaps-position.5= 32.500, 0.000 [Flaps.1] type= 2 span-outboard= 0.800 extending-time= 8.330 system_type= 1 damaging-speed= 353.592 blowout-speed= 323.592 lift_scalar= 0.300 drag_scalar= 1.210 pitch_scalar= 0.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 20.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 24.000, 0.000 flaps-position.4= 24.000, 0.000 flaps-position.5= 24.000, 0.000 //----------------------------------------------------------------------------------------------------------------------------------------------- [fltsim.0] title=Aerodesigns A343 Etihad sim=CFM56_340_AD-V1.2 model=3class panel= sound= texture=Etihad kb_checklists=CheckList_A343_AeroDesigns kb_reference=Reference_A343_AeroDesigns atc_id=A6-ETC atc_id_color=0xffffffff atc_airline=ETIHAD atc_flight_number=901 ui_manufacturer=Airbus ui_type=A340-300 (AeroDesigns) ui_variation=Etihad Airways atc_heavy=1 visual_damage=1 description=A343 AeroDesigns\nFlight Dynamics Research\nCopyright Aerodesigns @ 2003 [brakes] toe_brakes_scale=0.640889 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=24.375000 flap_limit_idle=12.187500 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=2930.555556 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0