[fltsim.0]
title=Beech Baron 58 Mountain Air
sim=Beech_Baron_58
model=
panel=
sound=
texture=
kb_checklists=Beech_Baron_58_check
kb_reference=Beech_Baron_58_ref
atc_id=N310MA
ui_manufacturer=Beechcraft
ui_type="Baron 58"
ui_variation="Mountain Air"
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_parking_types=RAMP
atc_parking_codes=ASH
atc_flight_number=
atc_airline=Mountain Air
visual_damage=0
atc_heavy=0
[General]
atc_type=Baron
atc_model=
editable=0
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\n1,613 lb 732 kg"
[WEIGHT_AND_BALANCE]
max_gross_weight = 5524 // (pounds)
empty_weight = 3911 // (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, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170, -6.54, 1.20, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "170, -9.80, -1.20, 0.0, Passenger" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "170, -9.80, 1.20, 0.0, Passenger" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
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 = 3905.65
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 = .666
aileron_effectiveness = 1.0
rudder_effectiveness = .75
pitch_stability = 1.5
roll_stability = 1.2
yaw_stability = 1.2
elevator_trim_effectiveness = 1.5
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = .75
[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= 0.75 //Fuel flow scalar
min_throttle_limit = 0.0; //Minimum percent throttle. Generally negative for turbine reverser
[piston_engine]
power_scalar = 1.1 //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= 2850.0 //Max rated RPM
max_rated_hp= 410.0 //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= 32 //Max design manifold pressure, (inHg)
min_design_mp= 1.0 //Min design manifold pressure, (inHg)
critical_altitude= 24000 //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 = 1.1 //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, 28, 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 = .500 //Brake scalar
[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 = 162 // KIAS
blowout-speed = 250 // KIAS
lift_scalar = 1.00
drag_scalar = .65
pitch_scalar= .95
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
[pitot_static]
vertical_speed_time_constant = 2.0 //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)
//eyepoint = -8.213, -0.6012, 2.200
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -6.60, -19.29, 0.79, fx_navred ,
light.1 = 3, -6.60, 19.29, 0.79, fx_navgre ,
light.2 = 3, -25.33, 0.00, 0.72, fx_navwhi ,
light.3 = 2, -6.43, -19.29, 0.79, fx_strobe ,
light.4 = 2, -6.43, 19.29, 0.79, fx_strobe ,
light.5 = 1, -24.48, 0.00, 6.39, fx_beacon ,
light.6 = 4, -11.80, 0.00, 2.90, fx_vclight ,
light.7 = 4, -7.80, 0.00, 2.90, fx_vclighth ,
light.8 = 4, -5.80, 0.00, 2.90, fx_vclightwhi,
light.9 = 5, 2.94, -7.58, -2.36, Newll ,
light.10 = 5, 2.94, 7.58, -2.36, Newll ,
light.11 = 4, -3.50, 0.00, 2.90, fx_vclightwhi,
light.12 = 3, -20.94, 0.0, 7.36, Newll ,
[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
[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=1,1 //Turn and Bank
[fuel]
LeftMain = -8.46, -6.45, 0.0, 68.0, 0.5 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux = -8.0, -6.0, -0.5, 15.5, 0.5 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -8.46, 6.45, 0.0, 68.0, 0.5 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = -8.0, 6.0, -0.5, 15.5, 0.5 //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
[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= 0.898 //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 = 22.0 //Degrees
elevator_down_limit = 18.5 //Degrees
aileron_up_limit = 18.0 //Degrees
aileron_down_limit = 18.0 //Degrees
rudder_limit = 30.0 //Degrees
elevator_trim_limit = 18.0 //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
[Reference Speeds]
flaps_up_stall_speed = 84.0 //Knots True (KTAS)
full_flaps_stall_speed = 75.0 //Knots True (KTAS)
cruise_speed = 205.0 //Knots True (KTAS)
max_indicated_speed = 223 //Red line (KIAS)
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=500.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_max_rpm =104
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8.000000
use_no_default_pitch=1
use_no_default_bank=1
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
default_pitch_mode=0
default_bank_mode=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
