; Localized	10/09/2007 09:20 PM (GMT)	4:4.2.169 	aircraft.cfg
[fltsim.0]
title=Airbus A321 Paint2
sim=Airbus_A321
model=""
panel=""
sound=""
texture=2
kb_checklists=AirbusA321_check
kb_reference=AirbusA321_ref
atc_id=F-MSAB
atc_airline=World Travel
atc_flight_number=""
ui_manufacturer=Аэробус
ui_type=A321
ui_variation=Ворлд Трэвел Эйрлайнс
ui_typerole=Гражданский авиалайнер
ui_createdby=Корпорация Майкрософт
description="Аэробус A321" - удлиненная версия A320, настоящего бестселлера среди авиалайнеров средней и малой дальности. А321 отличается слегка увеличенной площадью крыла, усиленным шасси с более широкими колесами и более мощными двигателями. Выпущенный в 1988 году, он стал первым самолетом с компьютеризованной кабиной, полностью электронной системой управления и боковыми ручками управления.

[fltsim.1]
title=Airbus A321 Paint4
sim=Airbus_A321
model=""
panel=""
sound=""
texture=4
kb_checklists=AirbusA321_check
kb_reference=AirbusA321_ref
atc_id=I-HKSN
atc_airline=Orbit
atc_flight_number=""
ui_manufacturer=Аэробус
ui_type=A321
ui_variation=Орбит Эйрлайнс
ui_typerole=Гражданский авиалайнер
ui_createdby=Корпорация Майкрософт
description="Аэробус A321" - удлиненная версия A320, настоящего бестселлера среди авиалайнеров средней и малой дальности. А321 отличается слегка увеличенной площадью крыла, усиленным шасси с более широкими колесами и более мощными двигателями. Выпущенный в 1988 году, он стал первым самолетом с компьютеризованной кабиной, полностью электронной системой управления и боковыми ручками управления.

[fltsim.2]
title=Airbus A321 Paint5
sim=Airbus_A321
model=""
panel=""
sound=""
texture=5
kb_checklists=AirbusA321_check
kb_reference=AirbusA321_ref
atc_id=JA-3297
atc_airline=Pacifica
atc_flight_number=""
ui_manufacturer=Аэробус
ui_type=A321
ui_variation=Пасифика Эйрлайнс
ui_typerole=Гражданский авиалайнер
ui_createdby=Корпорация Майкрософт
description="Аэробус A321" - удлиненная версия A320, настоящего бестселлера среди авиалайнеров средней и малой дальности. А321 отличается слегка увеличенной площадью крыла, усиленным шасси с более широкими колесами и более мощными двигателями. Выпущенный в 1988 году, он стал первым самолетом с компьютеризованной кабиной, полностью электронной системой управления и боковыми ручками управления.

[fltsim.3]
title=Airbus A321
sim=Airbus_A321
model=""
panel=""
sound=""
texture=""
kb_checklists=AirbusA321_check
kb_reference=AirbusA321_ref
atc_id=N3213221
atc_airline="American Pacific"
atc_flight_number="322"
ui_manufacturer=Аэробус
ui_type=A321
ui_variation=Белый
ui_typerole=Гражданский авиалайнер
ui_createdby=Корпорация Майкрософт
description="Аэробус A321" - удлиненная версия A320, настоящего бестселлера среди авиалайнеров средней и малой дальности. А321 отличается слегка увеличенной площадью крыла, усиленным шасси с более широкими колесами и более мощными двигателями. Выпущенный в 1988 году, он стал первым самолетом с компьютеризованной кабиной, полностью электронной системой управления и боковыми ручками управления.

[General]
atc_type=AIRBUS
atc_model=A321
editable=1
performance=Крейсерская скорость: М 0,80 (530 миль/ч, или 828 км/ч)\n\nДвигатель: General Electric CFM56-5B3, тяга 30000 фунтов\n\nМаксимальная дальность: 3200 м. миль (5926 км)\n\nРабочий потолок: 41000 фт. (12497 м)\n\nЗапас топлива: 52500 фнт. (198675 кг)\n\nВес без нагрузки: 107000 фнт. (48471 кг)\n\nМаксимальный вес: 206000 фнт. (93318 кг)\n\nДлина: 146 фт. (44,51 м)\n\nРазмах крыла: 111 фт. 10 д. (34,09 м)\n\nВысота: 38 фт. 7 д. (11,76 м)\n\nПосадочных мест: 185
Category=airplane

[CameraDefinition.0]
Title=Окно справа
Guid={54F54B8A-3EC2-2D4E-8D10-B8F9D0F16ACC}
Description=Вид на правое крыло из пассажирской кабины
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.9
ShowWeather=Yes
InitialXyz=3.2, 1.8, -5
InitialPbh=5, 0, 100
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title=Окно слева
Guid={0ae3f864-da10-4e5a-977c-b9bba47d6f7a}
Description=Вид на левое крыло из пассажирской кабины
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=1.0
ShowWeather=Yes
InitialXyz=-3.2, 1.8, -5
InitialPbh=5, 0, 260
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.2]
Title=Шасси
Guid={96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description=Вид от шасси и левых закрылков
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.52
ShowWeather=Yes
InitialXyz=-3.6, -1.8, -11
InitialPbh=0, 0, 18
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.3]
Title=Хвост
Guid={5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description=Вид с хвостовой части самолета
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.75
ShowWeather=Yes
InitialXyz=0, 5.5, -52.0
InitialPbh=5, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.4]
Title=Правое крыло
Guid={C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description=Вид на кабину с кончика правого крыла
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=30.8, 1.6, 4.0
InitialPbh=6, 0, 280
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum

[CameraDefinition.5]
Title=Левое крыло
Guid={f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description=Вид на кабину с кончика левого крыла
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.5
ShowWeather=Yes
InitialXyz=-30.8, 1.6, 4.0
InitialPbh=6, 0, 80
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=No
ClipMode=Minimum

[CameraDefinition.001]
Title=Правое сиденье
Guid={8ff6c134-098d-409f-baec-caba3f683f98}
Origin=Virtual Cockpit
MomentumEffect=YES
SnapPbhAdjust=Swivel
SnapPbhReturn=False
PanPbhAdjust=Swivel
PanPbhReturn=False
Track=None
ShowAxis=YES
AllowZoom=TRUE
InitialZoom=.7
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=1.35, 0.0, 0.0
InitialPbh=2, 0, 0

[CameraDefinition.002]
Title=Центральная панель
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=0.9
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.65, 0.50, -0.2
InitialPbh=70, 0, 0

[CameraDefinition.003]
Title=Верхняя приборная панель
Guid={4ca337db-ae88-4c5f-96ea-ddebbd2a86fe}
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=0.7, -0.58, -0.31
InitialPbh=-58.0, 0, 0

[WEIGHT_AND_BALANCE]
max_gross_weight=206000                      // (pounds)
empty_weight=107000                         // (pounds)

reference_datum_position=-4.5, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-4.0, 0, 0         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0=170.0,  52.0, -3.0,	2.0    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=170.0,  52.0,  3.0,	2.0    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=3360.0,  18.5, -3.0,	2.0    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=11840.0,  18.5,  3.0,	2.0    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4=11840.0, -26.0, -3.0,	2.0    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5=11840.0, -26.0,  3.0,	2.0    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_name.0=Пилот
station_name.1=2-й пилот
station_name.2=1-й класс A-C
station_name.3=1-й класс D-F
station_name.4=Тур. кл. A-C
station_name.5=Тур. кл. D-F

;Moments of Inertia
empty_weight_pitch_MOI=835131.26
empty_weight_roll_MOI=198749.02
empty_weight_yaw_MOI=806087.52
empty_weight_coupled_MOI=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=1                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=5.2, -18.6, -4.6                    //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=5.2,  18.6, -4.6                    //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=0.45                            //Scalar for fuel flow efficiency
min_throttle_limit=-0.25                      //Minimum percent throttle.  Generally negative for turbine reverser
max_contrail_temperature=-30                  //Temperature (deg C) below which contrails may appear

[TurbineEngineData]
fuel_flow_gain=0.002                          //Gain on fuel flow
inlet_area=19.6                               //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920                            //RPM, second stage compressor rated value
static_thrust=30000                           //Lbs, max rated static thrust at Sea Level
afterburner_available=0                       //Afterburner available?
reverser_available=1                          //Thrust reverser available?

[jet_engine]
thrust_scalar=1.0

[electrical]
max_battery_voltage=24.0
generator_alternator_voltage=30.0
max_generator_alternator_amps=400.0

;/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)
        
[contact_points]
point.0=1,  43.00,   0.00,  -9.70, 1600, 0, 1.442, 55.92, 0.6, 2.5, 0.9, 4.0, 4.0, 0, 220.0, 250.0
point.1=1, -11.20, -12.45, -10.30, 1600, 1, 1.442,  0.00, 1.0, 2.5, 0.9, 6.9, 6.9, 2, 220.0, 250.0
point.2=1, -11.20,  12.45, -10.30, 1600, 2, 1.442,  0.00, 1.0, 2.5, 0.9, 7.1, 7.1, 3, 220.0, 250.0
point.3=2, -19.00, -55.00,  4.00,  1000, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -19.00,  55.00,  4.00,  1000, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -51.00,   0.00, -2.00,  1000, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6=2,  54.00,   0.00, -2.00,  1000, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
point.7=2, -75.00,   0.00, 31.00,  1000, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0

max_number_of_points=21

static_pitch=0.3        //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=9.2    //feet, altitude of CG when at rest on the ground
gear_system_type=1      //Hydraulic

[gear_warning_system]
gear_warning_available=1    //Normal
pct_throttle_limit=0.1     //Percent throttle that activates warning
flap_limit_idle=5.0     //Flap angle that activates warning at idle
flap_limit_power=25.5     //Flap angle that activates warning at above idle

[brakes]
parking_brake=1         //Parking brake available
toe_brakes_scale=1.000  //Brake scalar
auto_brakes=3
hydraulic_system_scalar=1  //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure

[hydraulic_system]
normal_pressure=3000.0    //PSI
electric_pumps=1         //no electric pumps
engine_map=1,1,0,0   //pumps on Eng1,2

[Views]
eyepoint=53.0, -1.8, 4.3   //(feet) longitudinal, lateral, vertical distance from reference datum

[flaps.0]
type=1                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=20                                   // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=10                                   // degrees
flaps-position.2=15                                   // degrees
flaps-position.3=20                                   // degrees
flaps-position.4=40                                   // degrees
damaging-speed=250                                  // KIAS
blowout-speed=300                                  // KIAS
lift_scalar=0.7
drag_scalar=0.2
pitch_scalar=1.0
system_type=1                                         //Hydraulic

[flaps.1]
type=2                                    // 1 - tail, 2 - lead
span-outboard=0.8                                  // 0.0 .. 1.0
extending-time=10                                   // seconds
flaps-position.0=0                                    // degrees
flaps-position.1=18.0                                 // degrees
flaps-position.2=22.0                                 // degrees
flaps-position.3=22.0                                 // degrees
flaps-position.4=27.0                                 // degrees
damaging-speed=250                                  // KIAS
blowout-speed=300                                  // KIAS
lift_scalar=0.3
drag_scalar=0.2
pitch_scalar=0.0
system_type=1                                         //Hydraulic

[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, 1
Transponder.1=1
Marker.1=1

[LIGHTS]
;/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -19.10, -54.15,  5.85, fx_navredm ,
light.1=3, -19.10,  54.15,  5.85, fx_navgrem ,
light.2=3, -83.60,   0.00,  7.60, fx_navwhih ,
light.3=2, -18.60, -53.50,  5.75, fx_strobeh ,
light.4=2, -18.60,  53.50,  5.75, fx_strobeh ,
light.5=2,   3.70,   0.00, -2.80, fx_beaconb ,
light.6=1,  -3.30,   0.00, 11.50, fx_beaconh ,
;/light.7 = 4,  53.41,   0.00,  4.50, fx_vclighth ,

[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
direction_indicator.1=3,0

[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1

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

[altimeters]
altimeter.0=1
altimeter.1=1

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

[vacuum_system]
max_pressure=5.15   // PSI
vacuum_type=2       //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi

[pitot_static]
vertical_speed_time_constant=1                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.0    //Scalar on heat effectiveness, 0 = not available

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000

[exits]
number_of_exits=3
exit.0=0.4,  45.50, -6.0, 7.0, 0  //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.1=0.4, -33.50, 5.85, 0.0, 1  //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.2=0.4,  29.90, 6.0,  1.0, 2  //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
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=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=1.0

[fuel]
Center1=-4.0,   0.0, 0.0, 2150, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain=-6.4, -16.8, 0.0, 2040, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-6.4,  16.8  0.0, 2040, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux=-15.2, -37.6, 2.0,  780, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux=-15.2,  37.6, 2.0,  780, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type=2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=1
fuel_dump_rate=0.0167                        //Percent of max quantity per second, i.e. about 1 minute for full fuel

[airplane_geometry]
wing_area=1320.0                //Square feet
wing_span=112.04                 //Feet
wing_root_chord=20.0                  //Feet
wing_dihedral=6.5                   //Degrees
wing_incidence=1.0                   //Degrees
wing_twist=-0.5                  //Degrees
oswald_efficiency_factor=0.67                  //Measure of lift effeciency of wing
wing_winglets_flag=1                     //Are winglets available?
wing_sweep=25.0                  //Degrees, wing leading edge
wing_pos_apex_lon=8.4                   //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=-1.6                  //Feet, vertical distance from reference point, positive going up
htail_area=280.0                 //Square feet
htail_span=39.2                  //Feet
htail_pos_lon=-69.0                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=3.2                   //Feet, vertical distance from reference point, positive going up
htail_incidence=0.0                   //Degrees
htail_sweep=34.0                  //Degrees, horizontal tail leading edge
vtail_area=288.0                 //Square feet
vtail_span=25.6                  //Feet, tip to body
vtail_sweep=44.0                  //Degrees, vertical tail leading edge
vtail_pos_lon=-35.8                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=12.0                  //Feet, vertical distance from reference point, positive going up
elevator_area=70.5                  //Square feet
aileron_area=26.9                  //Square feet
rudder_area=56.2                  //Square feet
elevator_up_limit=22.5                  //Degrees
elevator_down_limit=19.5                  //Degrees
aileron_up_limit=20.0                  //Degrees
aileron_down_limit=20.0                  //Degrees
rudder_limit=26.0                  //Degrees
elevator_trim_limit=20.0                  //Degrees
spoiler_limit=60.0                  //Degrees
spoiler_extension_time=2.0			//Seconds
spoilerons_available=1                     //Spoilerons Available?
aileron_to_spoileron_gain=3                   //Aileron to spoileron gain
min_ailerons_for_spoilerons=10                //Degrees
min_flaps_for_spoilerons=0                    //Minimum flap handle position when spoilerons activate
auto_spoiler_available=1
positive_g_limit_flaps_up=4.0               //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down=3.0               //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up=-3.0               //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
fly_by_wire=1

[Reference Speeds]
flaps_up_stall_speed=142.0                 //Knots True (KTAS)
full_flaps_stall_speed=113.0                 //Knots True (KTAS)
cruise_speed=452.0                 //Knots True (KTAS)
max_mach=1.22
max_indicated_speed=340                   //Red line (KIAS)

[stall_warning]
type=2
stick_shaker=1

[deice_system]
structural_deice_type=1     //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots