[fltsim.0]
title=DreamFleet Beech Baron 58
sim=BaronB58_2k4v2.0
model=
panel=
sound=
texture=
kb_checklists=DFB58_CHECK
kb_reference=DFB58_REF
atc_id=N156DF
ui_manufacturer=DreamFleet & Flight One
ui_type=Beech Baron 58
ui_variation=N156DF
description=Raytheon Beechcraft Baron B58 by DreamFleet and Flight One\n\nCreated from the venerable single-engine Beech Bonanza over 40 years ago, the Beech Baron 58 is the ultimate in this enduring line of Beech twin-engine aircraft. Based on the fuselage, interior, and landing gear of the Beech A36, the Baron 58 is essentially a twin-engine version of this fine aircraft. Our simulated Baron 58 is based on 1999 and 2000 models, and features the standardized cockpit that is shared with the A36, and first introduced in 1984.

[fltsim.1]
title=DreamFleet Beech Baron 58 1
sim=BaronB58_2k4v2.0
model=KI525
panel=KI525
sound=
texture=1
kb_checklists=DFB58_CHECK
kb_reference=DFB58_REF
atc_id=N651DF
ui_manufacturer=DreamFleet & Flight One
ui_type=Beech Baron 58
ui_variation=N651DF
description=Raytheon Beechcraft Baron B58 by DreamFleet and Flight One\n\nCreated from the venerable single-engine Beech Bonanza over 40 years ago, the Beech Baron 58 is the ultimate in this enduring line of Beech twin-engine aircraft. Based on the fuselage, interior, and landing gear of the Beech A36, the Baron 58 is essentially a twin-engine version of this fine aircraft. Our simulated Baron 58 is based on 1999 and 2000 models, and features the standardized cockpit that is shared with the A36, and first introduced in 1984.

[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\n200 gal 757 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\n1,517 lb 688 kg"

[weight_and_balance]
max_gross_weight = 5524 //MTOW 5500 lbs
empty_weight = 3983
empty_weight_pitch_MOI  =  6482 //5637*1.1
empty_weight_roll_MOI   =  8874
empty_weight_yaw_MOI    = 11076
empty_weight_coupled_MOI= 0.0

reference_datum_position     =   6.96, 0, 0 //83.1 in 6.925 ft
empty_weight_CG_position     =  -6.16, 0, 0 // max fwd 74 in 6.16 ft

max_number_of_stations = 8

station_load.0 = 170,  -6.54, -0.9, -0.3, Pilot
station_load.1 = 170,  -6.54,  0.9, -0.3, Co-Pilot
station_load.2 =   0,  -9.79, -0.9, -0.3, Passenger 1
station_load.3 =   0,  -9.79,  0.9, -0.3, Passenger 2
station_load.4 =   0, -12.66, -0.9, -0.3, Passenger 3
station_load.5 =   0, -12.66,  0.9, -0.3, Passenger 4
station_load.6 =   0,  -1.25,  0.0,  0.0, Fwd. Baggage
station_load.7 =   0, -15.00,  0.0, -0.5, Rear Baggage

[Reference Speeds]
flaps_up_stall_speed=84 
full_flaps_stall_speed=75 
cruise_speed=180 
max_indicated_speed=223

[flight_tuning]
cruise_lift_scalar          = 1.0
parasite_drag_scalar        = 1.0
induced_drag_scalar         = 1.3
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
hi_alpha_on_roll            = 1.0
hi_alpha_on_yaw             = 1.0
p_factor_on_yaw             = 0.5
torque_on_roll              = 0.8
gyro_precession_on_roll     = 1.0
gyro_precession_on_yaw      = 1.0

[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type=0 
engine.0 = -1.8, -5.9, -0.5, 
engine.1 = -1.8,  5.9, -0.5, 
fuel_flow_scalar=0.88 //0.9
min_throttle_limit=0.0

[piston_engine]
power_scalar=1.065 //adj. for 300 SHP
cylinder_displacement=91.7
compression_ratio=8.0
number_of_cylinders=6 
max_rated_rpm=2700
max_rated_hp=300
fuel_metering_type=0 
cooling_type=0 
normalized_starter_torque=0.018 //0.02
turbocharged=0 
max_design_mp=0
min_design_mp=0
critical_altitude=0
emergency_boost_type=0 
emergency_boost_mp_offset=0
emergency_boost_gain_offset=0
fuel_air_auto_mixture=0 
auto_ignition=0 
max_rpm_mechanical_efficiency_scalar=1.0
idle_rpm_mechanical_efficiency_scalar=1.0
max_rpm_friction_scalar=1.0
idle_rpm_friction_scalar=1.0

[propeller]
thrust_scalar=1.2
propeller_type=0 
propeller_diameter=6.40                //spec=77 inch
propeller_blades=3 
propeller_moi=3.5
beta_max=45.0 //range 1800 to 2700 at 190 kias
beta_min=15.2                          //spec=15.2 
min_gov_rpm=800
prop_tc=0.002 
gear_reduction_ratio=1.0
fixed_pitch_beta=20
low_speed_theory_limit=80
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=0 
min_rpm_for_feather=700
beta_feather=82.5                      //spec=82.5
power_absorbed_cf=0.9
defeathering_accumulators_available=0 
prop_reverse_available=0 
minimum_on_ground_beta=15
minimum_reverse_beta=0

[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 2
LeftMain  = -6.80,  -6.45, -1.4, 71.0, 3.0
RightMain = -6.80,   6.45, -1.4, 71.0, 3.0
LeftTip   = -7.00, -11.30, -0.5, 29.0, 0.0
RightTip  = -7.00,  11.30, -0.5, 29.0, 0.0
electric_pump=2

[airplane_geometry]
wing_area = 199.2
wing_span = 37.79
wing_root_chord = 5.30
wing_dihedral = 6.90
wing_incidence = 1.0
wing_twist = -1.0
oswald_efficiency_factor = 0.8
wing_winglets_flag = 0
wing_sweep = 3
wing_pos_apex_lon = -4.88
wing_pos_apex_vert = -2.33
htail_area = 60.0
htail_span = 11.94
htail_pos_lon = -19.70
htail_pos_vert = 0.44
htail_incidence = 0.5
htail_sweep = 2.5
vtail_area = 18.0
vtail_span = 4.44
vtail_sweep = 41
vtail_pos_lon = -18.59
vtail_pos_vert = 1.11
elevator_area = 38.3
aileron_area = 18.4
rudder_area = 10.5
elevator_up_limit=30.0     //spec=30
elevator_down_limit=15.0   //spec=15
aileron_up_limit=20.0      //spec=20
aileron_down_limit=20.0    //spec=20
rudder_limit=25.0          //spec=25
elevator_trim_limit=23.0   //spec=10up 23 dn
spoiler_limit=30.0         //used for cowl flaps drag
spoilerons_available=0 
aileron_to_spoileron_gain=0
min_ailerons_for_spoilerons=0
min_flaps_for_spoilerons=0

[flaps.0] //system
type=1
span-outboard=0.5
extending-time=8.0
system_type=0
flaps-position.0=0
flaps-position.1=50,152  //spec=15
flaps-position.2=100,122  //spec=30
damaging-speed=122
blowout-speed=160
lift_scalar=0.0
drag_scalar=0.0
pitch_scalar=0.0

[flaps.1] //lift
type=1
span-outboard=0.5
extending-time=8.0
system_type=0
flaps-position.0=0
flaps-position.1=15
flaps-position.2=30
damaging-speed  =122
blowout-speed   =160
lift_scalar=1.0
drag_scalar=0.0
pitch_scalar=0.0

[flaps.2] //drag & pitch
type=1
span-outboard=0.5
extending-time=8.0
system_type=0
flaps-position.0=0
flaps-position.1=12
flaps-position.2=30
damaging-speed  =122y
blowout-speed   =160
lift_scalar=0.0
drag_scalar=1.0
pitch_scalar=1.0

[Views]
eyepoint =-6.8, -1.0,  1.53 

[contact_points]
//0  Class                        <0=none,1=wheel, 2=scrape, 3=float>
//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)

point.0 = 1,  -0.48,  0.00, -4.82,  800, 0, 0.57, 20, 0.19, 2.5, 0.70, 3.90, 3.60, 0, 152, 170
point.1 = 1,  -7.88, -5.00, -4.62, 1200, 1, 0.75,  0, 0.30, 2.5, 0.80, 4.00, 3.90, 2, 152, 170
point.2 = 1,  -7.88,  5.00, -4.62, 1200, 2, 0.75,  0, 0.30, 2.5, 0.80, 4.05, 3.95, 3, 152, 170
point.3 = 2,  -6.40, -18.8,     0,  600, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2,  -6.40,  18.8,     0,  600, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -22.02,     0, -0.91,  600, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, -25.61,     0,  5.47,  600, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2,   0.41,     0, -2.16,  600, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8 = 2,  -3.59,     0, -2.46,  600, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9 = 2, -12.28,     0, -2.22,  600, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.10 = 2,-22.46,     0, -0.92,  600, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0

max_number_of_points=11
static_pitch = 2.7
static_cg_height = 4.35
gear_system_type=0

[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi, 7=recognition, 8=wing, 9=logo, 10=cabin
light.0 = 3,  -6.78, -18.70,  0.17, fx_navred_dfb58
light.1 = 3,  -6.78,  18.70,  0.17, fx_navgre_dfb58
light.2 = 3, -24.00,      0,  0.12, fx_navwhi_dfb58
light.3 = 2,  -6.33, -18.37,  0.17, fx_strobe_dfb58
light.4 = 2,  -6.33,  18.37,  0.17, fx_strobe_dfb58
light.5 = 1, -22.67,      0,  5.77, fx_beacon_dfb58
light.6 = 9,  -6.30,      0,  1.40, fx_vclight_dfb58
light.7 = 8, -10.23,      0,  0.92, fx_vclight_dfb58
light.8 = 8, -12.23,      0,  0.92, fx_vclight_dfb58
light.9 = 2,  -6.33, -22.37, -0.10, fx_VCstrobe_dfb58
light.10 = 2, -6.33,  22.37, -0.10, fx_VCstrobe_dfb58
light.11 = 3, -6.78, -22.70, -0.10, fx_VCnavred_dfb58
light.12 = 3, -6.78,  22.70, -0.10, fx_VCnavgre_dfb58
light.13 = 5, -1.72,   6.86, -0.86, fx_navwhi_dfb58
light.14 = 5, -1.72,  -6.88, -0.86, fx_navwhi_dfb58

[electrical]
//BusType, MaxAmpLoad, MinVoltage       //BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage = 24.0
generator_alternator_voltage = 28.5
max_generator_alternator_amps = 100.0
flap_motor=        0,  4, 17
gear_motor=        0,  5, 17
autopilot=         0,  5, 17
avionics_bus=      0, 20, 17
avionics=          1, 15, 17
pitot_heat=        0,  5, 17
additional_system= 0, 20, 17
marker_beacon=     1,  5, 17
gear_warning=      0,  1, 17
fuel_pump=         0,  2, 17
starter1=          0, 20, 17
starter2=          0, 20, 17
light_nav=         0,  5, 17
light_beacon=      0,  5, 17
light_landing=     0, 10, 17
light_taxi=        0, 10, 17
light_strobe=      0,  6, 17
light_panel=       0,  4, 17
light_cabin=       0,  5, 17
light_recognition= 0,  5, 17
light_wing=        0,  5, 17
light_logo=        0,  5, 17
directiona_gyro=   0,  2, 17
prop_sync=         0, 15, 17
propeller_deice=   0, 10, 17

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 500
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=5000
max_pitch_velocity_hi_alt_breakpoint=10000
max_bank=27.5
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=20
nav_integrator_control=0.25
nav_derivative_control=0.0
nav_integrator_boundary=1.5
nav_derivative_boundary=0.0
gs_proportional_control=15
gs_integrator_control=0.5
gs_derivative_control=0.0
gs_integrator_boundary=0.5
gs_derivative_boundary=0.0
yaw_damper_gain = 0.0
default_pitch_mode=1 //1= pitch hold 2=alt hold
default_bank_mode=1  //1= wing level 2=bank hold

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0=1 
attitude_indicator.1=2

[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

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=1,1    //Turn AND Bank

[pitot_static]
vertical_speed_time_constant=1.0

[stall_warning]
//Type: 0=none 1=suction 2=electric
type=2

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000

[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

[brakes]
parking_brake = 1                  //Parking brake available
toe_brakes_scale = 1.0             //Brake scalar
differential_braking_scale = 1.0   //Delta on the amount of brake when the rudder pedals deflected

[hydraulic_system]
normal_pressure = 50.0    //PSI
engine_map=1,0,0,0

[exits]
//Percent per second
number_of_exits = 2
exit_rate.0 = 0.4
exit_rate.1 = 0.4

[effects]
wake = fx_wake
water = fx_spray
dirt=fx_dustrun
;dirt=fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
startup = fx_DFB58_engstrt

[folding_wings]
wing_fold_system_type = 4
fold_rates = 200.00,200.00

[smokesystem]
smoke.0 = 0.0, -2.5, -14.50, fx_dfb58_icelight
smoke.1 = 0.0, -5.65, -7.35, fx_dfb58_icelight2 

[tailhook]
tailhook_length=1                        //(feet)
tailhook_position = -15.0, 0.0, -1.0     //(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0

[keyboard_response]
elevator = 100, 180
aileron = 100, 180
rudder = 100, 180

[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 = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1.0
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

