[fltsim.0] title=Beech Baron 58 sim=Beech_Baron_58 model= panel= sound= texture= kb_checklists=Beech_Baron_58_check kb_reference=Beech_Baron_58_ref atc_id=N456HI ui_manufacturer=Beechcraft ui_type=Baron 58 ui_variation=White with blue and gold description=With the wonderful control harmony that is the hallmark of the Bonanza line, the Beech Baron 58 is considered a classic light twin. The Baron 58 is the spiffed-up version of a time-tested favorite, made more modern by its new Continental Special engines. The Baron combines the attractiveness of Beechcraft design with the reliability of twin engines, resulting in a gorgeous workhorse of an aircraft. atc_airline=Airwave [fltsim.1] title=Beech Baron 58 Coca Cola Edition sim=Beech_Baron_58 model= panel= sound= texture=coca kb_checklists=Beech_Baron_58_check kb_reference=Beech_Baron_58_ref atc_id= ui_manufacturer=Beechcraft ui_type=Baron 58 ui_variation=Coca Cola description=The Coca-Cola Company exists to benefit and refresh everyone it touches. Founded in 1886, our Company is the world's leading manufacturer, marketer, and distributor of nonalcoholic beverage concentrates and syrups, used to produce more than 300 beverage brands. The corporate headquarters are in Atlanta, with local operations in over 200 countries around the world. atc_airline= atc_heavy=0 atc_flight_number=CC407 [General] atc_type=BARON atc_model= editable=1 performance=Cruise Speed\n200 kts 370 km\/hr\n\nEngine\nTeledyne Continental Motors IO-550-C 300 hp\n\nPropeller\nThree-bladed McCauley constant-speed, variable pitch\n\nMaximum Range\n1,569 nm 2,906 km\n\nService Ceiling\n20,688 ft 6,306 km\n\nFuel Capacity\n142 gal 537 L\n\nMaximum Gross Weight\n5,524 lb 2,509 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\n1,634 lb 741 kg [WEIGHT_AND_BALANCE] max_gross_weight= 5524.000 empty_weight= 3911.000 reference_datum_position= 6.960, 0.000, 0.000 empty_weight_CG_position= -6.060, 0.000, 0.000 max_number_of_stations=50 station_load.0= 170.000, -6.540, -1.200, 0.000 station_load.1= 170.000, -6.540, 1.200, 0.000 station_load.2= 170.000, -9.800, -1.200, 0.000 station_load.3= 170.000, -9.800, 1.200, 0.000 station_load.4=0, -12.67, -1.1, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5=0, -12.67, 1.1, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6=0, -15.00, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI= 3905.650 empty_weight_roll_MOI= 2718.640 empty_weight_yaw_MOI= 5291.040 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [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 Engine.0= -1.400, -5.300, 0.000 Engine.1= -1.400, 5.300, 0.000 fuel_flow_scalar= 0.900 [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement= 91.700 compression_ratio= 8.000 number_of_cylinders= 6 max_rated_rpm= 2700.000 max_rated_hp= 300.000 fuel_metering_type= 0 cooling_type= 0 normalized_starter_torque= 0.300 turbocharged= 0 max_design_mp= 0.000 min_design_mp= 0.000 critical_altitude= 0.000 emergency_boost_type= 0 emergency_boost_mp_offset= 0.000 emergency_boost_gain_offset= 0.000 fuel_air_auto_mixture= 0 auto_ignition= 0 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 propeller_diameter= 6.400 propeller_blades= 3 propeller_moi= 6.900 beta_max= 45.000 beta_min= 15.200 min_gov_rpm= 1100.000 prop_tc= 0.100 gear_reduction_ratio= 1.000 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= 82.500 power_absorbed_cf= 0.900 defeathering_accumulators_available= 0 prop_reverse_available= 0 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 [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= 1.000, 0.820, 0.000, -3.960, 1600.000, 0.000, 0.633, 40.000, 0.420, 2.500, 0.900, 3.000, 3.000, 0.000, 152.000, 303.850 point.1= 1.000, -8.040, -4.790, -3.960, 1600.000, 1.000, 0.886, 0.000, 0.500, 2.500, 0.850, 4.100, 4.300, 2.000, 152.000, 337.611 point.2= 1.000, -8.040, 4.790, -3.960, 1600.000, 2.000, 0.886, 0.000, 0.500, 2.500, 0.850, 4.300, 4.100, 3.000, 152.000, 337.611 //SCRAPES point.3= 2.000, -6.200, -18.910, 0.500, 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, -6.200, 18.910, 0.500, 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, -24.040, 0.000, -0.500, 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, 0.400, 0.000, -1.240, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= 1.560 static_cg_height= 3.430 [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 [exits] number_of_exits=1 exit_rate.0=0.4 ;Percent per second [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, -0.8612, 2.220 //Longitudinal, Lateral, Vertical (feet) [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -6.80, -19.29, 0.79, fx_navred , light.1=3, -6.80, 19.29, 0.79, fx_navgre , light.2=3, -25.33, 0.00, 0.72, fx_navwhi , light.3=2, -6.63, -19.29, 0.79, fx_strobe , light.4=2, -6.63, 19.29, 0.79, fx_strobe , light.5=1, -24.18, 0.00, 6.17, fx_beacon , light.6=2, -8.00, 0.00, -1.60, fx_strobe , light.7=4, -8.00, 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 [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 [fuel] LeftMain= -8.460, -6.450, 0.000, 71.000, 0.000 RightMain= -8.460, 6.450, 0.000, 71.000, 0.000 fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=2 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [airplane_geometry] wing_area= 199.000 wing_span= 37.800 wing_root_chord= 5.300 wing_dihedral= 6.900 wing_incidence= 1.000 wing_twist= -1.000 oswald_efficiency_factor= 0.700 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= -5.600 wing_pos_apex_vert= 0.000 htail_area= 60.000 htail_span= 15.900 htail_pos_lon= -20.100 htail_pos_vert= 0.000 htail_incidence= 0.500 htail_sweep= 0.000 vtail_area= 88.000 vtail_span= 10.700 vtail_sweep= 0.000 vtail_pos_lon= -22.900 vtail_pos_vert= 3.100 elevator_area= 20.000 aileron_area= 11.300 rudder_area= 10.500 elevator_up_limit= 17.000 elevator_down_limit= 15.500 aileron_up_limit= 18.000 aileron_down_limit= 18.000 rudder_limit= 30.000 elevator_trim_limit= 15.000 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 [Reference Speeds] flaps_up_stall_speed= 96.000 full_flaps_stall_speed= 76.800 cruise_speed= 200.000 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000 autothrottle_available=0 pitch_takeoff_ga=8.000000 [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 [Flaps.0] type= 1 span-outboard= 0.410 extending-time= 4.000 system_type= 0 damaging-speed= 152.000 blowout-speed= 250.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 15.000, 0.000 flaps-position.2= 30.000, 0.000
