[fltsim.0]
title=SuperJet 100 Normal
sim=SSJ100
model=
panel=
sound=
texture=white
kb_checklists=
kb_reference=
atc_id=CU-T733
atc_id_color=
ui_manufacturer=AEROPROYECTO
ui_type="SUKHOI SuperJet SSJ-100"
ui_variation="Normal"
description="SUKHOI SuperJet 100 R2.0 Freeware \nAEROPROYECTO 1999-2017 \nBy Edgar Guinart Lуpez\nhttp://aeroproyecto.freetzi.com"
visual_damage=1

[fltsim.1]
title=SuperJet 100 Wide
sim=SSJ100
model=
panel=ws
sound=
texture=white
kb_checklists=
kb_reference=
atc_id=CU-T733
atc_id_color=
ui_manufacturer=AEROPROYECTO
ui_type="SUKHOI SuperJet SSJ-100"
ui_variation="Wide"
description="SUKHOI SuperJet 100 R2.0 Freeware \nAEROPROYECTO 1999-2017 \nBy Edgar Guinart Lуpez\nhttp://aeroproyecto.freetzi.com"
visual_damage=1

[fltsim.2]
title=SuperJet 100 Normal Interjet
sim=SSJ100
model=
panel=
sound=
texture=interjet
kb_checklists=
kb_reference=
atc_id=AX-A00
atc_id_color=
ui_manufacturer=AEROPROYECTO
ui_type="SUKHOI SuperJet SSJ-100"
ui_variation="Normal Interjet"
description="SUKHOI SuperJet 100 R2.0 Freeware \nAEROPROYECTO 1999-2017 \nBy Edgar Guinart Lуpez\nhttp://aeroproyecto.freetzi.com"
visual_damage=1

[fltsim.3]
title=SuperJet 100 Wide Interjet
sim=SSJ100
model=
panel=ws
sound=
texture=interjet
kb_checklists=
kb_reference=
atc_id=AX-A00
atc_id_color=
ui_manufacturer=AEROPROYECTO
ui_type="SUKHOI SuperJet SSJ-100"
ui_variation="Wide Interjet"
description="SUKHOI SuperJet 100 R2.0 Freeware \nAEROPROYECTO 1999-2017 \nBy Edgar Guinart Lуpez\nhttp://aeroproyecto.freetzi.com"
visual_damage=1

[fltsim.4]
title=SuperJet 100 Normal Aeroflot
sim=SSJ100
model=
panel=
sound=
texture=aeroflot
kb_checklists=
kb_reference=
atc_id=RA-89001
atc_id_color=
ui_manufacturer=AEROPROYECTO
ui_type="SUKHOI SuperJet SSJ-100"
ui_variation="Normal Aeroflot"
description="SUKHOI SuperJet 100 R2.0 Freeware \nAEROPROYECTO 1999-2017 \nBy Edgar Guinart Lуpez\nhttp://aeroproyecto.freetzi.com"
visual_damage=1

[fltsim.5]
title=SuperJet 100 Wide Aeroflot
sim=SSJ100
model=
panel=ws
sound=
texture=aeroflot
kb_checklists=
kb_reference=
atc_id=RA-89001
atc_id_color=
ui_manufacturer=AEROPROYECTO
ui_type="SUKHOI SuperJet SSJ-100"
ui_variation="Wide Aeroflot"
description="SUKHOI SuperJet 100 R2.0 Freeware \nAEROPROYECTO 1999-2017 \nBy Edgar Guinart Lуpez\nhttp://aeroproyecto.freetzi.com"
visual_damage=1

// Outside views just for FSX

[CameraDefinition.0]
Title = Right gears
Guid = {45A9FCC0-2822-46c6-BBE2-AA1F9D074B09}
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = False
AllowZoom = True
InitialZoom = 1.0
ZoomPanScalar = 1
ShowWeather = Yes
XyzAdjust = False
Category = Aircraft
PitchPanRate=40
HeadingPanRate=40
panacceleratortime=0
Transition = No
InitialXyz = 5.0, -2.0, -10.0 		// lat, ver, lon
InitialPbh = 0, 0, -9		// up-dn, roll, L-R
ClipMode = Minimum

[CameraDefinition.1]
Title = Left engine
Guid = {49463D43-DC63-4d6b-9460-5C4858F0F172}
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = False
AllowZoom = True
InitialZoom = 0.7
ZoomPanScalar = 1
ShowWeather = Yes
XyzAdjust = False
Category = Aircraft
PitchPanRate=40
HeadingPanRate=40
panacceleratortime=0
Transition = No
InitialXyz = -7.0, -0.5, 8.8
InitialPbh = 10, 0, 150
ClipMode = Minimum

[CameraDefinition.2]
Title = Nose gear
Guid = {C227C51D-5464-484e-BC93-B67752EC0722}
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = False
AllowZoom = True
InitialZoom = 1.0
ZoomPanScalar = 1
ShowWeather = Yes
XyzAdjust = False
Category = Aircraft
PitchPanRate=40
HeadingPanRate=40
panacceleratortime=0
Transition = No
InitialXyz = 3.0, -2.0, 15.0
InitialPbh = 5, 0, -150
ClipMode = Minimum

//Please, donґt edit behind this point, the dynamics could be seriously damage!

[General]
atc_type=SUKHOI
atc_model=SuperJet
editable=0
performance="Velocidad de crucero:   477 nudos (885 km\/h)   \nMotores:   SAM-146 with 17,270 lbs max thrust   \nAlcance mбximo:    2390 mn (4420 km)    \nTecho de servicio:    41000 pies (12500 m)    \nCapacidad de combustible:    3500 U.S. galons (10681 kg)    \nPeso en vacнo:    55000 lb (25000 kg)    \nPeso bruto mбximo:    105000 lbs (47727 kg)    \nLargo:   98,23 pies (29,94 m)    \nEnvergadura:    91,20 pies (27,8 m)    \nAlto:    33,73 pies (10,28 m)    \nPlazas:    Asientos 98 (Standard single class)    \nCapacidad de carga:    775,8 pies3 (21,97 m3)"
Category=airplane

[pitot_static]
vertical_speed_time_constant = 999                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000

[WEIGHT_AND_BALANCE]
max_gross_weight = 105000                      // (pounds)
empty_weight = 55000                           // (pounds)  *** 55000 lbs Empty Weight (EW)

reference_datum_position     =  0, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  2.0, 0.0, -3.6         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50 

//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)  *** Tipical conf.: 15488 lbs pax, 800 lbs F-bag and 2200 lbs R-bag 
station_load.0 = "4000,	 18.7, 0.0, 0.0, 23 Pax 5060 lbs Max"
station_load.1 = "4000,	   6.0, 0.0, 0.0, 25 Pax 5500 lbs Max"
station_load.2 = "4000,	  -6.6, 0.0, 0.0, 25 Pax 5500 lbs Max"
station_load.3 = "4000,	-19.3, 0.0, 0.0, 25 Pax 5500 lbs Max"
station_load.4 = "1200,	 24.0, 0.0, -4.6, Bag 3180 lbs Max"
station_load.5 = "1000,	-22.0, 0.0, -4.6, Bag 4960 lbs Max"


;Moments of Inertia
empty_weight_pitch_MOI	=652000		// 632000 calculations
empty_weight_roll_MOI	=243000		// 443000 
empty_weight_yaw_MOI	=637000		// 657000
empty_weight_coupled_MOI=0
CG_forward_limit=0.0
CG_aft_limit=1.0


[fuel]
Center1   =  4.0,    0, -3.3,  440, 0                 // 1473 LR - 440 BASIC //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain  = -1.9, -19, -2.6, 1351, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -1.9,  19, -2.6, 1351, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2                                   //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2                    
electric_pump=1


[GeneralEngineData]
engine_type = 1                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 0.0, -14.9, -6.9                    //(feet) longitudinal, lateral, vertical distance from reference datum *** 0.0, -14.9, -6.9
Engine.1 = 0.0,  14.9, -6.9                   //(feet) longitudinal, lateral, vertical distance from reference datum  *** 0.0, 14.9, -6.9
fuel_flow_scalar = 0.93                            //Scalar for fuel flow efficiency
min_throttle_limit = -0.3                      //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 = 12.56                               //Square Feet, engine nacelle inlet area  *** FAN = 12.56 sf
rated_N2_rpm = 18523                            //RPM, second stage compressor rated value
static_thrust = 17270                           //Lbs, max rated static thrust at Sea Level  *** Max  = 17270 lbf
afterburner_available = 0                       //Afterburner available?
reverser_available = 1                          //Thrust reverser available?

[jet_engine]
thrust_scalar = 1.0


[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)

max_battery_voltage		=28.0
generator_alternator_voltate		=30.0
max_generator_alternator_amps	=200.0
flap_motor 			= 0, 0 , 17.0
gear_motor 			= 0, 0 , 17.0
autopilot 			= 0, 0 , 17.0
avionics_bus 			= 0, 0 , 17.0
avionics 			= 1, 0 , 17.0
pitot_heat 			= 0, 0 , 17.0
additional_system 		= 0, 0 , 17.0
marker_beacon 			= 1, 0 , 17.0
gear_warning 			= 0, 0 , 17.0
fuel_pump 			= 0, 0 , 17.0
starter1 			= 0, 0 , 17.0
starter2 			= 0, 0 , 17.0
light_nav 			= 0, 0 , 17.0
light_beacon 			= 0, 0 , 17.0
light_strobe 			= 0, 0 , 17.0
light_landing 			= 0, 0 , 17.0
light_taxi 			= 0, 0 , 17.0
light_panel 			= 0, 0 , 17.0
light_cabin 			= 0, 0 , 17.0
light_recognition 		= 0, 0 , 17.0
light_wing 			= 0, 0 , 17.0
light_logo 			= 0, 0 , 17.0
auto_brakes 			= 0, 0 , 17.0
standby_vacuum 			= 0, 0 , 17.0
hydraulic_pump 			= 0, 0 , 17.0
fuel_transfer_pump 		= 0, 0 , 17.0
propeller_deice 		= 0, 0 , 17.0
directional_gyro 		= 0, 0 , 17.0
directional_gyro_slaving 	= 0, 0 , 17.0


        //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,  33.70,   0.00, -11.80, 1181.1, 0, 1.0, 65.00, 0.6, 2.0, 0.5, 4.0, 4.0, 0, 216.0, 256.0
point.1=1,  -3.00,  -9.20, -11.80, 1574.8, 1, 1.5,  0.00, 0.6, 1.5, 0.5, 7.0, 7.0, 2, 216.0, 256.0
point.2=1,  -3.00,   9.20, -11.80, 1574.8, 2, 1.5,  0.00, 0.6, 1.5, 0.5, 7.0, 7.0, 3, 216.0, 256.0
// Hard countach
point.3 = 2,  10.0, -14.90, -10.00, 1600, 0, 0.00,  0.0, 0.3, 2.5, 0.6, 0.0, 0.0, 7, 0.0, 0.0
point.4 = 2,  10.0,  14.90, -10.00, 1600, 0, 0.00,  0.0, 0.3, 2.5, 0.6, 0.0, 0.0, 7, 0.0, 0.0
point.5 = 2,  34.00,   0.00, -6.00, 1600, 0, 0.00,  0.0, 0.5, 2.5, 0.5, 0.0, 0.0, 7, 0.0, 0.0
point.6 = 2, -25.00,   0.00, -6.00, 1600, 0, 0.00,  0.0, 0.5, 2.5, 0.5, 0.0, 0.0, 7, 0.0, 0.0
// crash points
point.7 =2,   -11.60, -45.00,  0.00,  515, 0, 0.0,  0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.8 =2,   -11.60,  45.00,  0.00,  515, 0, 0.0,  0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.9 =2,   40.00,   0.00,  -3.00,  920, 0, 0.0,  0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.10=2, -51.00,   0.00,   0.00,  920, 0, 0.0,  0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0

max_number_of_points = 21

static_pitch=0.00       //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=11.60   //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    =  9.0     //Flap angle that activates warning at idle
flap_limit_power   = 25.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1         //Parking brake available
toe_brakes_scale = 0.8  //Brake scalar

[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=36.3, -1.85, 1.8   //(feet) longitudinal, lateral, vertical distance from reference datum

[flaps.0]       //Trailing Edge Flaps
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.7                                  // 0.0 .. 1.0
extending-time   = 20                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 3                                    // degrees
flaps-position.2 = 9                                    // degrees
flaps-position.3 = 16                                    // degrees
flaps-position.4 = 25                                    // degrees
flaps-position.5 = 36                                   // degrees
damaging-speed   = 260                                  // KIAS
blowout-speed    = 308                                  // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic

[flaps.1]       //Leading Edge Slats
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.9                                  // 0.0 .. 1.0
extending-time   = 10                                    // seconds
flaps-position.0 = 0                                    //  degrees
flaps-position.1 = 18.0                                  //  degrees
flaps-position.2 = 18.0                                  //  degrees
flaps-position.3 = 24.0                                  //  degrees
damaging-speed   = 260                                  // KIAS
blowout-speed    = 308                                  // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic


[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1       = 1
Com.1         = 1, 0
Com.2         = 1, 1
Nav.1         = 1, 1, 1
Nav.2         = 1, 1, 0
Adf.1         = 1, 0
Adf.2         = 1, 0
Transponder.1 = 1
Marker.1      = 1

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -11.50, -44.90,   0.51, fx_navredm ,
light.1 = 3, -11.50,  44.90,   0.51, fx_navgrem ,
light.2 = 2, -53.70,   0.00,   1.25, fx_strobeh ,
light.3 = 2, -11.60, -45.00,   0.51, fx_strobeh ,
light.4 = 2, -11.60,  45.00,   0.51, fx_strobeh ,
light.5 = 1,   3.20,  -0.75,  -6.90, fx_beaconb ,
light.6 = 1,   3.65,   0.00,   5.76, fx_beaconh ,
light.7 = 4,  35.50,   0.00,   2.88, fx_vclighth ,
light.8 = 5,  10.30,  -6.10,  -3.35, SSJ100_LandSpot ,
light.9 = 5,  10.30,   6.10,  -3.35, SSJ100_LandSpot ,
light.10= 7,  10.60,  -5.70,  -3.25, fx_landing ,
light.11= 7,  10.60,   5.70,  -3.25, fx_landing ,
light.12= 6,  34.70,  -0.55,  -8.35, SSJ100_TaxiSpot ,
light.13= 6,  34.70,   0.55,  -8.35, SSJ100_TaxiSpot ,
light.14= 3, -16.10, -45.70,   0.52, fx_navwhi ,
light.15= 3, -16.10,  45.70,   0.52, fx_navwhi ,
light.16= 9,  34.80,  -0.25,  -8.70, SSJ100_TaxiSpot ,
light.17= 9,  34.80,   0.25,  -8.70, SSJ100_TaxiSpot ,


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

[SMOKESYSTEM]
smoke.0= 0.00,  -15.5, -45.5, SSJ100_vortex
smoke.1= 0.00,  -15.5,  45.5, SSJ100_vortex

[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=0,0

[exits]
number_of_exits = 2
exit_rate.0 = 0.3                               ;Percent per second
exit_rate.1 = 0.3                               ;Percent per second


[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 99
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8;
max_pitch=10.0
max_pitch_acceleration=0.8
max_pitch_velocity_lo_alt=1.0
max_pitch_velocity_hi_alt=1.0
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=25.0
max_bank_acceleration=3.0
max_bank_velocity=3.00
max_throttle_rate=0.1
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=19.0
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


[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 = 1.3
aileron_trim_effectiveness  = 1.3
rudder_trim_effectiveness   = 1.0
hi_alpha_on_roll=1.0
hi_alpha_on_yaw=1.0


[airplane_geometry]
wing_area               = 829                //Square feet *** 829 wings *** 212 between wings root
wing_span               = 91.21                 //Feet
wing_root_chord         = 17.7                  //Feet
wing_dihedral           = 6.0                   //Degrees
wing_incidence          = 1.5                   //Degrees
wing_twist              = -1.0                  //Degrees
oswald_efficiency_factor= 0.75                  //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 28.7                  //Degrees, wing leading edge
wing_pos_apex_lon       = 13.5                   //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = -3.6                   //Feet, vertical distance from reference point, positive going up

htail_area              = 213.0                 //Square feet
htail_span              = 34.0                  //Feet
htail_pos_lon           = -37.1                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 2.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = -3.0                   //Degrees
htail_sweep             = 34.0                  //Degrees, horizontal tail leading edge

vtail_area              = 165.0                 //Square feet
vtail_span              = 17.25                  //Feet, tip to body
vtail_sweep             = 40.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -30.6                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 5.0                   //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     = 16.0                  //Degrees
spoiler_limit           = 60.0                  //Degrees
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=0
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000

[Reference Speeds]
flaps_up_stall_speed    = 110.0                 //Knots True (KTAS)
full_flaps_stall_speed  = 95.0                 //Knots True (KTAS)
cruise_speed            = 460.0                 //Knots True (KTAS)
max_mach                = 0.81	                //Max Mach
max_indicated_speed     = 308                   //Red line (KIAS)

[stall_warning]
type=2
stick_shaker=0

[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000 

[deice_system]
structural_deice_type=1

[GPWS]
max_warning_height         =  1000
sink_rate_fpm              = -1500
excessive_sink_rate_fpm    = -2000
climbout_sink_rate_fpm     = -100
flap_and_gear_sink_rate_fpm= -100


[forcefeedback]
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=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 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 microse