[fltsim.0] title=Beech Baron 58TC sim=Beech_Baron_58TC model= panel= sound= texture= kb_checklists=Beech_Baron_58_check kb_reference=Beech_Baron_58_ref atc_id=N059BE atc_id_color=0xffffff00 ui_manufacturer="Beechcraft" ui_type="Baron 58TC" ui_variation= ui_typerole="Twin Engine Prop" ui_createdby="Microsoft Corporation" description="This Beech Baron 58TC is the turbonormalized version of the classic light twin. The Baron 58TC is the spiffed-up version of a time-tested favorite, made more modern by its new Teledyne/Continental Special engines, with GAMI injection for an ultra smooth running, high performance engine. The Baron Tornado Alley Turbo normalizer ensures that you optain sea level performance all the way up to 25,000 ft. Turbonormalized engines differ from traditional turbocharged engines in that they do not boost at sea level but progressively add boost as the aircraft gains altitude. This means that the system maintains sea level engine performance up to ceiling, but does not suffer the risk of over boost, or increased internal pressure associated with normal turbo systems. With the benefit of GAMI injectors as well you can fly faster, further and for less fuel that a conventional Beech." [General] atc_type=BEECH atc_model=BE58 editable=0 performance="Cruise Speed\n220 kts 407 km\/hr\n\nEngine\nTeledyne Continental Motors IO-550-CT 320 hp\n\nPropeller\nThree-bladed McCauley constant-speed, variable pitch\n\nMaximum Range\n1,369 nm 2,535 km\n\nService Ceiling\n25,000 ft 7,620 km\n\nFuel Capacity\n142 gal 537 L\n\nMaximum Gross Weight\n6,200 lb 2,816 kg \n\nLength\n29 ft, 10 in 9.09 m\n\nWingspan\n37 ft, 10 in 11.53 m\n\nHeight\n9 ft, 9 in 2.97 m\n\nSeating Up to 6\n\nUseful Load\n1,862 lb 846 kg" Category = airplane [CameraDefinition.0] Title = "Right Wing" Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59} Description = View from the right wing looking at the cockpit Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 1.0 ShowWeather = Yes InitialXyz = 11.5, 0.7, -0.2 InitialPbh = 5, 0, 275 XyzAdjust = TRUE Category=Aircraft ClipMode=Minimum [CameraDefinition.1] Title = "Left Wing" Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED} Description = View from the left wing looking at the cockpit Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 1.0 ShowWeather = Yes InitialXyz = -11.5, 0.6, -0.2 InitialPbh = 5, 0, 85 XyzAdjust = TRUE Category=Aircraft ClipMode=Minimum [CameraDefinition.2] Title = "Tail" Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A} Description = Looking forward from behind the aircraft Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.75 ShowWeather = Yes InitialXyz = 0, 2.0, -15.0 InitialPbh = 7, 0, 0 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.001] Title = "Right Seat" Guid = {195EAB58-9E4A-1E2A-A34C-A8D9D948F078} Origin = Virtual Cockpit MomentumEffect = Yes SnapPbhAdjust = Swivel SnapPbhReturn = False PanPbhAdjust = Swivel PanPbhReturn = False Track = None ShowAxis = YES AllowZoom = TRUE InitialZoom = 0.7 SmoothZoomTime = 2.0 ZoomPanScalar = 1.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.52, 0.0, 0.0 InitialPbh=3, 0, 0 [CameraDefinition.002] Title = "Radio Stack" Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078} Origin = Virtual Cockpit MomentumEffect = No SnapPbhAdjust = None SnapPbhReturn = False PanPbhAdjust = None PanPbhReturn = False Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 1.3 SmoothZoomTime = 2.0 ZoomPanScalar = 1.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.41, -0.06, 0.0 InitialPbh=15, 0, 0 [CameraDefinition.003] Title = "Engine Controls" Guid = {563fdda0-af36-4c28-ab71-b5db7e77e474} Origin = Virtual Cockpit MomentumEffect = No SnapPbhAdjust = None SnapPbhReturn = False PanPbhAdjust = None PanPbhReturn = False Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.9 SmoothZoomTime = 2.0 ZoomPanScalar = 1.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.27, -0.1, 0.18 InitialPbh=45, 0, 0 [CameraDefinition.004] Title = "Switches" Guid = {195EAB58-9E4A-3E2A-A34C-A8D9D948F078} Origin = Virtual Cockpit MomentumEffect = No SnapPbhAdjust = None SnapPbhReturn = False PanPbhAdjust = None PanPbhReturn = False Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.8 SmoothZoomTime = 2.0 ZoomPanScalar = 1.0 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.11, -0.55, 0.18 InitialPbh=-10, 0, -16 [WEIGHT_AND_BALANCE] max_gross_weight = 6200 // (pounds) empty_weight = 4338 // (pounds) reference_datum_position = 6.96, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -6.06, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = 170, -6.54, -1.20, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = 170, -6.54, 1.20, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = 170, -9.80, -1.20, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = 170, -9.80, 1.20, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = 0, -12.67, -1.1, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5 = 0, -12.67, 1.1, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = 0, -15.00, 0.0, 0.0 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_name.0 = "Pilot" station_name.1 = "Co-Pilot" station_name.2 = "Passenger" station_name.3 = "Passenger" station_name.4 = "Passenger" station_name.5 = "Passenger" station_name.6 = "Baggage" ;Moments of Inertia empty_weight_pitch_MOI = 3905.65 empty_weight_roll_MOI = 2718.64 empty_weight_yaw_MOI = 5291.04 empty_weight_coupled_MOI= 0.0 [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 [GeneralEngineData] engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = -1.4, -5.3, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = -1.4, 5.3, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar= 1.11 //Fuel flow scalar min_throttle_limit = 0.0; //Minimum percent throttle. Generally negative for turbine reverser [piston_engine] power_scalar = 1.0 //Piston power scalar cylinder_displacement= 91.7 //Cubic inches per cylinder compression_ratio= 8.0 //Compression ratio number_of_cylinders= 6 //Number of cylinders max_rated_rpm= 2750.0 //Max rated RPM max_rated_hp= 320.0 //Max rated HP fuel_metering_type= 0 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque= 0.3 //Starter torque factor turbocharged= 1 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp= 38.0 //Max design manifold pressure, (inHg) min_design_mp= 1.0 //Min design manifold pressure, (inHg) critical_altitude= 25000.0 //Altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power emergency_boost_mp_offset= 0.0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset= 0.0 //Multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction [propeller] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter= 6.4 //Propeller Diameter, (feet) propeller_blades= 3 //Number of propeller blades propeller_moi= 6.9 //Propeller moment of inertia beta_max= 45.0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 15.2 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm= 1100.0 //Miminum governed RPM prop_tc= 0.1 //Prop time-constant gear_reduction_ratio= 1.0 //Propeller gear reduction ratio fixed_pitch_beta= 0.0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit= 80.0 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available= 1 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available= 1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available= 1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather= 700.0 //Minimum RPM for prop feathering beta_feather= 82.5 //Feathering pitch angle (degrees) power_absorbed_cf= 0.9 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta= 0.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta= 0.0 //Minimum pitch angle in reverse, (degrees) [contact_points] //0 Class //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) //GEAR point.0 = 1, 0.82, 0.00, -3.77, 1600, 0, 0.633, 40, 0.42, 4.0, 0.90, 3.0, 3.0, 0, 152, 180 point.1 = 1, -8.04, -4.79, -3.93, 1600, 1, 0.886, 0, 0.50, 2.5, 0.85, 4.1, 4.3, 2, 152, 200 point.2 = 1, -8.04, 4.79, -3.93, 1600, 2, 0.886, 0, 0.50, 2.5, 0.85, 4.3, 4.1, 3, 152, 200 //SCRAPES point.3= 2, -6.20,-18.91, 0.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4= 2, -6.20, 18.91, 0.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5= 2,-24.04, 0.00, -0.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6= 2, 0.40, 0.00, -1.24, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 static_pitch = 1.56 //Degrees static_cg_height = 3.43 //Feet gear_system_type=0 //Electric [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 0.0 //Flap angle that activates warning at idle flap_limit_power = 31.5 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 1.0 //Brake scalar auto_brakes = 0 [hydraulic_system] normal_pressure = 0.0 //PSI [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.41 // 0.0 .. 1.0 extending-time = 4 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 15 // degrees flaps-position.2 = 30 // degrees damaging-speed = 152 // KIAS blowout-speed = 250 // KIAS [electrical] max_battery_voltage = 24.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps = 60.0 [pitot_static] vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat = 1.0 //Scalar on heat effectiveness, 0 = not available [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 [Views] eyepoint = -8.213, -0.80, 2.32 //Longitudinal, Lateral, Vertical (feet) [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -6.81, -19.30, 1.17, fx_navred , light.1 = 3, -6.82, 19.29, 1.17, fx_navgre , light.2 = 3, -25.33, 0.01, 1.08, fx_navwhi , light.3 = 2, -6.48, -19.04, 1.17, fx_strobe , light.4 = 2, -6.48, 19.04, 1.17, fx_strobe , light.5 = 1, -24.20, 0.00, 6.44, fx_beacon , light.6 = 2, -7.52, 0.01, -1.28, fx_strobe , light.7 = 4, -8.30, 0.00, 2.70, fx_vclight, [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [altimeters] altimeter.0=1 altimeter.1=1 [airspeed_indicators] airspeed_indicator.0=1 airspeed_indicator.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 attitude_indicator.1 = 2 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=1,1 //Turn and Bank [vacuum_system] max_pressure=5.15 //PSI vacuum_type=1 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi electric_backup_pressure=4.900000 engine_map=1,1 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=0.00000 [fuel] LeftMain = -8.46, -6.45, 0.0, 71.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -8.46, 6.45, 0.0, 71.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 2 electric_pump=1 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [exits] number_of_exits = 2 exit.0 = 0.4 // (0=Main 1=Emergency) exit.1 = 0.4 // (0=Main 1=Emergency) [airplane_geometry] wing_area = 199.0 //Square feet wing_span = 37.8 //Feet wing_root_chord = 5.3 //Feet wing_dihedral = 6.9 //Degrees wing_incidence = 1.0 //Degrees wing_twist = -1.0 //Degrees oswald_efficiency_factor= 0.7 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 0.0 //Degrees, wing leading edge wing_pos_apex_lon = -5.6 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up htail_area = 60.0 //Square feet htail_span = 15.9 //Feet htail_pos_lon = -20.1 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up htail_incidence = 0.5 //Degrees htail_sweep = 0.0 //Degrees, horizontal tail leading edge vtail_area = 88.0 //Square feet vtail_span = 10.7 //Feet, tip to body vtail_sweep = 0.0 //Degrees, vertical tail leading edge vtail_pos_lon = -22.9 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 3.1 //Feet, vertical distance from reference point, positive going up elevator_area = 20.0 //Square feet aileron_area = 11.3 //Square feet rudder_area = 10.5 //Square feet elevator_up_limit = 17.0 //Degrees elevator_down_limit = 15.5 //Degrees aileron_up_limit = 18.0 //Degrees aileron_down_limit = 18.0 //Degrees rudder_limit = 30.0 //Degrees elevator_trim_limit = 15.0 //Degrees spoiler_limit = 0.0 //Degrees spoilerons_available = 0 //Spoilerons Available? aileron_to_spoileron_gain = 0 //Aileron to spoileron gain min_ailerons_for_spoilerons = 0 //Degrees min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate auto_spoiler_available = 0 positive_g_limit_flaps_up = 3.0 //Design G load tolerance (positive, flaps up) positive_g_limit_flaps_down= 2.0 //Design G load tolerance (positive, flaps down) negative_g_limit_flaps_up = -2.0 //Design G load tolerance (negative, flaps up) negative_g_limit_flaps_down= -2.0 //Design G load tolerance (negative, flaps down) load_safety_factor = 1.5 //Design G load safety factor [Reference Speeds] flaps_up_stall_speed = 84.0 //Knots True (KTAS) full_flaps_stall_speed = 79.0 //Knots True (KTAS) cruise_speed = 217.0 //Knots True (KTAS) max_indicated_speed = 223 //Red line (KIAS) [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 700.0 autothrottle_available= 0 pitch_takeoff_ga=8.0 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=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 0.0 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds 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=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 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 [stall_warning] type=2 stick_shaker=0 [deice_system] structural_deice_type=3 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots