[fltsim.0] title=Avro Tudor sim=AvroTudor model= panel= sound= texture= panel_alias = beech_baron_58\panel sound_alias = beech_baron_58\sound kb_checklists= kb_reference= atc_id=GFOOL ui_manufacturer=Avro ui_type=Tudor ui_variation=Mk XIII description=Long Range Commercial Transport.\nCrew: 5 (two pilots, flight engineer, radio operator, navigator)\nCapacity: 60 passengers\nPowerplant: 4× Rolls-Royce Merlin 600 12-cylinder V12 engines, 1,770 hp\n atc_heavy=0 atc_airline=Landmark atc_flight_number=013 [General] atc_type=Tudor atc_model=ATP performance=Maximum speed: 330 mph at 8,000 ft\nCruise speed: 285 mph at 12,000 ft\nRange: 3,630 miles\nService ceiling 28,600 ft [WEIGHT_AND_BALANCE] max_gross_weight = 66000.000 empty_weight = 46300.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = -0.500, 0.000, 0.000 CG_forward_limit = 0.000 CG_aft_limit = 1.000 empty_weight_pitch_MOI = 395351.000 empty_weight_roll_MOI = 444748.000 empty_weight_yaw_MOI = 811988.000 empty_weight_coupled_MOI = 0.000 station_load.0=400.000000, 37.000000, 0.000000, 0.000000, Pilots [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =1.000 induced_drag_scalar =1.000 elevator_effectiveness =1.000 aileron_effectiveness =6.000 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 hi_alpha_on_roll =1.00000 hi_alpha_on_yaw =1.00000 p_factor_on_yaw =1.00000 torque_on_roll =1.00000 gyro_precession_on_roll =1.00000 gyro_precession_on_yaw =1.00000 [GeneralEngineData] engine_type = 0 Engine.0 = 10.000, -25.000, 0.900 Engine.1 = 12.000, -12.000, 0.100 Engine.2 = 12.000, 12.000, 0.100 Engine.3 = 10.000, 25.000, 0.900 fuel_flow_scalar = 1.050 min_throttle_limit = 0 master_ignition_switch = 1 [piston_engine] power_scalar =1.000 cylinder_displacement = 137.250 compression_ratio = 6.100 number_of_cylinders = 12 max_rated_rpm = 3000.000 max_rated_hp = 1770.000 fuel_metering_type = 1 cooling_type = 1 normalized_starter_torque = 0.015 turbocharged = 1 max_design_mp = 58.000 min_design_mp = 10.000 critical_altitude = 15000.000 emergency_boost_type = 0 emergency_boost_mp_offset = 0.000 emergency_boost_gain_offset = 0.000 fuel_air_auto_mixture = 1 auto_ignition = 0 emergency_boost_duration =360.00000 max_rpm_mechanical_efficiency_scalar =1.000 idle_rpm_mechanical_efficiency_scalar =1.000 max_rpm_friction_scalar =1.000 idle_rpm_friction_scalar =1.000 [propeller] thrust_scalar =1.000 propeller_type = 0 propeller_diameter = 13.000 propeller_blades = 4 propeller_moi = 100.000 beta_max = 65.000 beta_min = 19.000 min_gov_rpm = 1800.000 prop_tc = 0.010 gear_reduction_ratio = 2.380 fixed_pitch_beta = 0.000 low_speed_theory_limit = 80.000 prop_sync_available = 1 prop_deice_available = 1 prop_feathering_available = 1 prop_auto_feathering_available = 0 min_rpm_for_feather = 700.000 beta_feather = 88.500 power_absorbed_cf = 0.900 defeathering_accumulators_available = 0 prop_reverse_available = 0.000 minimum_on_ground_beta = 0.000 minimum_reverse_beta = 0.000 feathering_switches = 1 [contact_points] max_number_of_points =9 static_pitch= 10.000 static_cg_height= 10.874 gear_system_type =1 tailwheel_lock=1 //GEAR point.0 = 1.000, -56.140, 0.000, -0.865, 2600.000, 0.000, 1.636, 40.000, 0.305, 1.679, 0.911, 8.000, 8.000, 0.000, 280.000, 287.000 point.1 = 1.000, 4.180, -11.865, -11.851, 2600.000, 1.000, 2.647, 0.000, 0.806, 1.476, 0.691, 8.000, 8.000, 2.000, 181.000, 190.000 point.2 = 1.000, 4.180, 11.865, -11.851, 2600.000, 2.000, 2.647, 0.000, 0.806, 1.476, 0.691, 8.000, 8.000, 3.000, 181.000, 190.000 //SCRAPES point.3= 2.000, -3.660, -60.000, 3.100, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, -3.660, 60.000, 3.100, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -33.300, 0.000, -1.500, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, 31.600, 0.000, -1.500, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 [Views] eyepoint= 23.363, -1.602, 1.704 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 24 max_generator_alternator_amps = 80 electric_always_available = 1 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 starter2 = 0, 20, 17 starter3 = 0, 20, 17 starter4 = 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 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 propeller_deice = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, -2.449, -50.128, 4.802, fx_navred light.1 = 3, -2.449, 50.128, 4.802, fx_navgre light.2 = 3, -49.589, 0, -0.619, fx_navwhi light.3 = 4, 23.363, -1.602, 1.704, fx_vclight [Radios] // availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 0 Nav.1 = 1, 0, 1 Nav.2 = 0, 0, 0 Adf.1 = 1 Adf.2 = 0 Transponder.1 = 1 Marker.1 = 1 [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [direction_indicators] direction_indicator.0 = 1, 0 [exits] number_of_exits = 1 exit_rate.0 = 0.4 [EFFECTS] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 [autopilot] autopilot_available =1 flight_director_available =0 attitude_indicator=1 directional_indicator=0 default_vertical_speed =0.00000 autothrottle_available =0 autothrottle_arming_required =0 autothrottle_takeoff_ga =1.00000 autothrottle_max_rpm =90.00000 pitch_takeoff_ga =4.00000 default_pitch_mode =1 default_bank_mode =0 max_pitch =10.00000 max_pitch_acceleration =1.00000 max_pitch_velocity_lo_alt =2.00000 max_pitch_velocity_hi_alt =1.50000 max_pitch_velocity_lo_alt_breakpoint =20000.00000 max_pitch_velocity_hi_alt_breakpoint =28000.00000 max_bank=25.00000 max_bank_acceleration =1.80000 max_bank_velocity =3.00000 max_throttle_rate =0.10000 nav_proportional_control =9.00000 nav_integrator_control =0.25000 nav_derivative_control =0.00000 nav_integrator_boundary =2.50000 nav_derivative_boundary =0.00000 gs_proportional_control =9.52000 gs_integrator_control =0.26000 gs_derivative_control =0.00000 gs_integrator_boundary =0.70000 gs_derivative_boundary =0.00000 yaw_damper_gain =0.00000 [fuel] LeftMain = -3.000, -15.000, 0.000, 1285.000, 0.000 RightMain = -3.000, 15.000, 0.000, 1285.000, 0.000 fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 2 electric_pump=1 [airplane_geometry] wing_area = 1421.000 wing_span = 120.000 wing_root_chord = 17.500 wing_dihedral = 5.000 wing_incidence = 0.000 wing_twist = 0.000 oswald_efficiency_factor = 0.800 wing_winglets_flag = 0 wing_sweep = 0.000 wing_pos_apex_lon = 3.000 wing_pos_apex_vert = 3.000 htail_area = 380.000 //htail was 117 htail_span = 48.000 htail_pos_lon = -54.000 htail_pos_vert = 4.000 htail_incidence = 0.000 htail_sweep = 0.000 vtail_area = 152.000 vtail_span = 19.000 vtail_sweep = 15.000 vtail_pos_lon = -55.000 vtail_pos_vert = 5.000 elevator_area = 70.000 aileron_area = 106.000 rudder_area = 54.000 elevator_up_limit = 15.000 elevator_down_limit = 12.000 aileron_up_limit = -12.000 aileron_down_limit = -11.000 rudder_limit = 28.000 elevator_trim_limit = 18.000 spoiler_limit = 0.000 spoilerons_available = 0 aileron_to_spoileron_gain = 0.000 min_ailerons_for_spoilerons = 0.000 min_flaps_for_spoilerons = 0.000 auto_spoiler_available=0 positive_g_limit_flaps_up=3.00000 negative_g_limit_flaps_up=-2.40000 positive_g_limit_flaps_down=2.10000 negative_g_limit_flaps_down=-1.80000 load_safety_factor=1.00000 [Reference Speeds] flaps_up_stall_speed = 90.000 full_flaps_stall_speed = 80.000 cruise_speed = 285.000 max_indicated_speed =350.00000 max_mach =0.60000 [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 stick_shaker_magnitude =5000 stick_shaker_direction =0 stick_shaker_period =111111 [gear_warning_system] gear_warning_available =1 pct_throttle_limit =0.10000 flap_limit_idle =30.00000 flap_limit_power =15.00000 [brakes] toe_brakes_scale =0.34089 parking_brake = 1 differential_braking_scale = 1 [stall_warning] // 0 = None, 1 = Suction, 2 = Electric. type = 1 [hydraulic_system] electric_pumps = 0 engine_map = 1, 1, 1, 1 normal_pressure =1000.00000 [attitude_indicators] // 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] // 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0 = 1, 0 [direction_indicators] // 0=None, 1=Vac Gyro, 2=Elec Gyro, 3=EM Slave Compass, 4=Slave to other ind direction_indicator.0 = 1, 0 [airspeed_indicators] airspeed_indicator.0 = 1, 0 [smokesystem] smoke.0 =3 smoke.1 = 3.17892156862745, 51, 0, fx_smoke_w [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 6.000 system_type= 1 damaging-speed= 191.000 blowout-speed= 199.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 10.000, 0.000 flaps-position.2= 15.000, 0.000 flaps-position.3= 20.000, 0.000 flaps-position.4= 25.000, 0.000 flaps-position.5= 35.000, 0.000 flaps-position.6= 45.000, 0.000