[fltsim.0] title= Dominican Cargo A300-600 sim=TFS_A300 model=A306_PW texture=Dom atc_id=HI-LONG atc_airline=DOMINICANA atc_flight_number=501 ui_manufacturer=Airbus ui_type=Airbus A300-600 ui_variation=Dominican Cargo A300-600 description=Dominican Cargo Trust atc_id_color=0x00000000 visual_damage=0 atc_heavy=1 atc_parking_codes=AIB atc_parking_types=GATE [General] atc_type=AIRBUS atc_model=A300 editable=0 performance=Cruise Speed\tMach .84\nMaximum Range\t5,720 nm\nService Ceiling\t35,000 ft\nMax Takeoff Weight\t660,000 lb\nSeating\t\t336 to 550\nCargo Capacity\t20 standard LD3 containers \n Category=airplane [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.000000 [weight_and_balance] max_gross_weight = 151000 empty_weight = 103170 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 12, 0, 0 empty_weight_pitch_MOI = 3160000 empty_weight_roll_MOI = 3262183 empty_weight_yaw_MOI = 4337024 empty_weight_coupled_MOI = 0 max_number_of_stations = 9 station_load.0 = "170.0, 41.0, -1.5, 0.0, Pilot" station_load.1 = "170.0, 41.0, 1.5, 0.0, Co-Pilot" station_load.2 = "510.0, 0.0, 0.0, 0.0, Crew" station_load.3 = "1360.0, 25.5, 0.0, 0.0, First Class" station_load.4 = "8160.0, 11.0, 0.0, 0.0, Coach 3-10" station_load.5 = "8160.0, -10.0, 0.0, 0.0, Coach 11-18" station_load.6 = "7140.0, -30.5, 0.0, 0.0, Coach 19-25" station_load.7 = "10000.0, 20.5, 0.0, 0.0, Forward Baggage" station_load.8 = "4000.0, -27.5, 0.0, 0.0, Aft Baggage" [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -22.17, -73.09, 3.294, fx_navred light.1 = 2, -21.75, -73.03, 3.296, fx_strobe light.2 = 3, -31.72, -72.88, 3.065, fx_navwhi light.3 = 2, -31.72, -72.88, 3.065, fx_strobe light.4 = 3, -22.17, 73.09, 3.294, fx_navgre light.5 = 2, -21.75, 73.03, 3.296, fx_strobe light.6 = 3, -31.72, 72.88, 3.065, fx_navwhi light.7 = 2, -31.72, 72.88, 3.065, fx_strobe light.8 = 1, -35.29, 0, -9.03, fx_beaconb light.9 = 1, 6.76, 0, 9.44, fx_beaconb [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 1 min_throttle_limit = -0.1100 max_contrail_temperature = -25 engine.0 = 0.18, -25.945, -8.622, engine.1 = 0.18, 25.945, -8.622, [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=28000 //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 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 windshield_rain_effect_available = 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 electric_pump = 0 Center1 = 0, 0, 0, 2313, 0 LeftMain = -3, -19, 0, 1500, 0 RightMain = -3, 19, 0, 1500, 0 [contact_points] static_pitch = -1.02 static_cg_height = 16.72 tailwheel_lock = 0 gear_system_type = 0 max_number_of_points = 7 point.0 = 1, 52.460, 0.0000, -16.298, 1574.8, 0, 1.442, 55.92, 0.8, 2.5, 0.6, 6, 6, 0, 220, 250 point.1 = 1, -10.582, -15.17, -17.7018, 1574.8, 1, 1.442, 0, 1, 2.5, 0.9, 8.9, 8.9, 2, 220, 250 point.2 = 1, -10.582, 15.17, -17.7018, 1574.8, 2, 1.442, 0, 1, 2.5, 0.9, 9.1, 9.1, 3, 220, 250 point.3 = 2, -25.04, -73.38, 0.15, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -25.04, 73.38, 0.15, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -48.7, 0, -8.33, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 62.31, 0, -7.71, 787.4, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 [keyboard_response] elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [airplane_geometry] wing_area = 2337.0 wing_span = 126.46 wing_root_chord = 28.58 wing_dihedral = 6.19 wing_incidence = 1.0 wing_twist = -0.5 oswald_efficiency_factor = 0.85 wing_winglets_flag = 0 wing_sweep = 28 wing_pos_apex_lon = 18.58 wing_pos_apex_vert = 0 htail_area = 338.0 htail_span = 50.15 htail_pos_lon = -59.65 htail_pos_vert = 0 htail_incidence = 0.0 htail_sweep = 34 vtail_area = 224.0 vtail_span = 28.77 vtail_sweep = 42 vtail_pos_lon = -50.76 vtail_pos_vert = 5.53 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 spoiler_handle_available = 1 min_ailerons_for_spoilerons = 10 min_flaps_for_spoilerons = 0 spoilerons_available =0 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 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 engine_generator_map = 1,1,0,0 electric_always_available = 1 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 5, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 2, 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=1.2 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=0.8 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [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 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 5.0 //Flap angle that activates warning at idle flap_limit_power = 25.5 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.485 //Brake scalar auto_brakes=4 [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint=43.7, -1.31, 3.7 //(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 = 0.1 drag_scalar = 0.0 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 = 4 // seconds flaps-position.0 = 0 // flaps-position.4 = 0.5 flaps-position.5 = 1.0 // damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.1 drag_scalar = 0.0 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 = 7 // seconds flaps-position.0 = 0 // flaps-position.4 = 0.5 flaps-position.5 = 1.0 // damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.1 drag_scalar = 0.0 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 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [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=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=33.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=12.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=25.0 gs_integrator_control=0.53 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 1.0 [Reference Speeds] flaps_up_stall_speed=150.0 //Knots True (KTAS) full_flaps_stall_speed=120.0 //Knots True (KTAS) cruise_speed=494.0 //Knots True (KTAS) max_mach = 0.85 max_indicated_speed = 330 //Red line (KIAS) [stall_warning] type=2 stick_shaker=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