; Localized	06/21/2007 02:00 AM (GMT)	4:4.2.169 	aircraft.cfg
[fltsim.0]
title=Beech Baron 58 Paint1
sim=Beech_Baron_58
model=""
panel=""
sound=""
texture=1
kb_checklists=Beech_Baron_58_check
kb_reference=Beech_Baron_58_ref
atc_id=N71FS
ui_manufacturer=Бичкрафт
ui_type=Барон-58Турбо
ui_variation=Белый с синей полосой
ui_typerole=Двухмоторный винтовой
ui_createdby=Корпорация Майкрософт
description="Бичкрафт Барон-58" - классический легкий двухмоторный самолет, достойный продолжатель серии "Бонанза" все с той же отточенной управляемостью. "Барон-58 Турбо" - улучшенная версия предыдущей модели, обновленная двигателями Continental Special с турбонаддувом и увеличенным до 190 галлонов обьёмом топливных баков. Привлекательный дизайн "Бичкрафта" в сочетании с надежностью двигателей, высотностью и дальностью полёта до 1400 морских миль даже с полной загрузкой сделали его великолепной рабочей лошадкой.

[fltsim.1]
title=Beech Baron 58 Paint2
sim=Beech_Baron_58
model=""
panel=""
sound=""
texture=2
kb_checklists=Beech_Baron_58_check
kb_reference=Beech_Baron_58_ref
atc_id=N71FS
ui_manufacturer=Бичкрафт
ui_type=Барон-58Турбо
ui_variation=Белый с красной полосой
ui_typerole=Двухмоторный винтовой
ui_createdby=Корпорация Майкрософт
description="Бичкрафт Барон-58" - классический легкий двухмоторный самолет, достойный продолжатель серии "Бонанза" все с той же отточенной управляемостью. "Барон-58 Турбо" - улучшенная версия предыдущей модели, обновленная двигателями Continental Special с турбонаддувом и увеличенным до 190 галлонов обьёмом топливных баков. Привлекательный дизайн "Бичкрафта" в сочетании с надежностью двигателей, высотностью и дальностью полёта до 1400 морских миль даже с полной загрузкой сделали его великолепной рабочей лошадкой.

[fltsim.2]
title=Beech Baron 58 Paint3
sim=Beech_Baron_58
model=""
panel=""
sound=""
texture=3
kb_checklists=Beech_Baron_58_check
kb_reference=Beech_Baron_58_ref
atc_id=N71FS
ui_manufacturer=Бичкрафт
ui_type=Барон-58Турбо
ui_variation=Частный
ui_typerole=Двухмоторный винтовой
ui_createdby=Корпорация Майкрософт
description="Бичкрафт Барон-58" - классический легкий двухмоторный самолет, достойный продолжатель серии "Бонанза" все с той же отточенной управляемостью. "Барон-58 Турбо" - улучшенная версия предыдущей модели, обновленная двигателями Continental Special с турбонаддувом и увеличенным до 190 галлонов обьёмом топливных баков. Привлекательный дизайн "Бичкрафта" в сочетании с надежностью двигателей, высотностью и дальностью полёта до 1400 морских миль даже с полной загрузкой сделали его великолепной рабочей лошадкой.

[fltsim.3]
title=Beech Baron 58 w G1000
sim=Beech_Baron_58
model=g1000
panel=g1000
sound=""
texture=g1000
kb_checklists=Beech_Baron_58_check
kb_reference=Beech_Baron_58_ref
atc_id=N71FS
ui_manufacturer=Бичкрафт
ui_type=Барон-58Турбо
ui_variation=Кабина G1000
ui_typerole=Двухмоторный винтовой
ui_createdby=Корпорация Майкрософт
description="Бичкрафт Барон-58" - классический легкий двухмоторный самолет, достойный продолжатель серии "Бонанза" все с той же отточенной управляемостью. "Барон-58 Турбо" - улучшенная версия предыдущей модели, обновленная двигателями Continental Special с турбонаддувом и увеличенным до 190 галлонов обьёмом топливных баков. Привлекательный дизайн "Бичкрафта" в сочетании с надежностью двигателей, высотностью и дальностью полёта до 1400 морских миль даже с полной загрузкой сделали его великолепной рабочей лошадкой.

[fltsim.4]
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=N058BE
ui_manufacturer=Бичкрафт
ui_type=Барон-58Турбо
ui_variation=Белый
ui_typerole=Двухмоторный винтовой
ui_createdby=Корпорация Майкрософт
description="Бичкрафт Барон-58" - классический легкий двухмоторный самолет, достойный продолжатель серии "Бонанза" все с той же отточенной управляемостью. "Барон-58 Турбо" - улучшенная версия предыдущей модели, обновленная двигателями Continental Special с турбонаддувом и увеличенным до 190 галлонов обьёмом топливных баков. Привлекательный дизайн "Бичкрафта" в сочетании с надежностью двигателей, высотностью и дальностью полёта до 1400 морских миль даже с полной загрузкой сделали его великолепной рабочей лошадкой.

[General]
atc_type=BEECH
atc_model=BE58
editable=0
performance=Крейсерская скорость: 200 узлов (370 км/ч)\n\nДвигатель: Teledyne Continental Motors TSIO-520-WB 325 л.с.\n\nВоздушный винт: McCauley, трехлопастной с регулятором постоянных оборотов и изменяемым шагом\n\nМаксимальная дальность: 1569 м. миль (2906 км)\n\nРабочий потолок: 25000 фт. (7620 м)\n\nЗапас топлива: 190 галл. (684 л)\n\nМаксимальный вес: 6240 фнт. (2827 кг)\n\nДлина: 29 фт. 10 д. (9,09 м)\n\nРазмах крыла: 37 фт. 10 д. (11,53 м)\n\nВысота: 9 фт. 9 д. (2,97 м)\n\nПосадочных мест: до 6\n\nПолезная нагрузка: 1613 фнт. (732 кг)
Category=airplane

[CameraDefinition.0]
Title=Правое крыло
Guid={C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description=Вид на кабину с правого крыла
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=Левое крыло
Guid={3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED}
Description=Вид на кабину с левого крыла
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=Хвост
Guid={D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description=Вид с хвостовой части самолета
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=Правое сиденье
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=Блок радиосвязи
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=Панель управления двигателем
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=Переключатели
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=6240                         // (pounds)
empty_weight=4078                             // (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=170, -12.67, -1.1, 0.0        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5=170, -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=Пилот
station_name.1=Пассажир
station_name.2=Пассажир
station_name.3=Пассажир
station_name.4=Пассажир
station_name.5=Пассажир
station_name.6=Багаж

;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=0.75                           //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=2700.0                           //Max rated RPM
max_rated_hp=325.0                             //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=18000.0                          //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, 95.0, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-8.46,  6.45, 0.0, 95.0, 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=основной 1=аварийный)
exit.1=0,4 // (0=основной 1=аварийный)

[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=75.0                  //Knots True (KTAS)
cruise_speed=180.0                 //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