[fltsim.0]
title=Antonov AN-124 Sovjet Air Force 82005
sim=an124
model=
panel=
sound=
texture=
checklists=
description=The Anotonov-124 Ruslan (Condor) has become one of the most famous cargo transporter worldwide for military and comercial transports (like parts of the european Ariane rocket). Model by Thomas Ruth & Alex Kvitta, Sound by Leonid Korshunov, Paint by Johns, Collect by Alexander Khrustitskyi.
ui_manufacturer=ANTK Antonov
ui_type=An-124
ui_variation=Sovjet Air Force 82005
atc_heavy=1
atc_id=82005
atc_airline=AEROFLOT
atc_flight_number=82005
visual_damage=1


[fltsim.1]
title=Antonov AN-124 Antonov Air Cargo UR-82009
sim=an124
model=
panel=
sound=
texture=1
checklists=
description=The Anotonov-124 Ruslan (Condor) has become one of the most famous cargo transporter worldwide for military and comercial transports (like parts of the european Ariane rocket). Model by Thomas Ruth & Alex Kvitta, Sound by Leonid Korshunov, Paint by Johns, Collect by Alexander Khrustitskyi.
ui_manufacturer=ANTK Antonov
ui_type=An-124
ui_variation=Antonov Air Cargo UR-82009
atc_heavy=1
atc_id=UR-82009
atc_airline=Antonov Airlines
atc_flight_number=UR-82009
visual_damage=1


[fltsim.2]
title=Antonov AN-124 Antonov Air Cargo UR-82027
sim=an124
model=
panel=
sound=
texture=2
checklists=
description=The Anotonov-124 Ruslan (Condor) has become one of the most famous cargo transporter worldwide for military and comercial transports (like parts of the european Ariane rocket). Model by Thomas Ruth & Alex Kvitta, Sound by Leonid Korshunov, Paint by Johns, Collect by Alexander Khrustitskyi.
ui_manufacturer=ANTK Antonov
ui_type=An-124
ui_variation=Antonov Air Cargo UR-82027
atc_heavy=1
atc_id=UR-82027
atc_airline=Antonov Airlines
atc_flight_number=UR-82027
visual_damage=1


[fltsim.3]
title=Antonov AN-124 Air Foyle Antonov CP-82008
sim=an124
model=
panel=
sound=
texture=3
checklists=
description=The Anotonov-124 Ruslan (Condor) has become one of the most famous cargo transporter worldwide for military and comercial transports (like parts of the european Ariane rocket). Model by Thomas Ruth & Alex Kvitta, Sound by Leonid Korshunov, Paint by Johns, Collect by Alexander Khrustitskyi.
ui_manufacturer=ANTK Antonov
ui_type=An-124
ui_variation=Air Foyle Antonov CP-82008
atc_heavy=1
atc_id=CP-82008
atc_airline=Air Foyle Antonov
atc_flight_number=CP-82008
visual_damage=1


[fltsim.4]
title=Antonov AN-124 VolgaDnepr-HeavyLift RA-82045
sim=an124
model=
panel=
sound=
texture=4
checklists=
description=The Anotonov-124 Ruslan (Condor) has become one of the most famous cargo transporter worldwide for military and comercial transports (like parts of the european Ariane rocket). Model by Thomas Ruth & Alex Kvitta, Sound by Leonid Korshunov, Paint by Johns, Collect by Alexander Khrustitskyi.
ui_manufacturer=ANTK Antonov
ui_type=An-124
ui_variation=VolgaDnepr-HeavyLift RA-82045
atc_heavy=1
atc_id=RA-82045
atc_airline=VolgaDnepr-HeavyLift
atc_flight_number=RA-82045
visual_damage=1


[fltsim.5]
title=Antonov AN-124 Polet RA-82077
sim=an124
model=
panel=
sound=
texture=5
checklists=
description=The Anotonov-124 Ruslan (Condor) has become one of the most famous cargo transporter worldwide for military and comercial transports (like parts of the european Ariane rocket). Model by Thomas Ruth & Alex Kvitta, Sound by Leonid Korshunov, Paint by Johns, Collect by Alexander Khrustitskyi.
ui_manufacturer=ANTK Antonov
ui_type=An-124
ui_variation=Polet RA-82077
atc_heavy=1
atc_id=RA-82077
atc_airline=Polet Airlines
atc_flight_number=RA-82077
visual_damage=1


[fltsim.6]
title=Antonov AN-124 Russia Air Cargo RA-82072
sim=an124
model=
panel=
sound=
texture=6
checklists=
description=The Anotonov-124 Ruslan (Condor) has become one of the most famous cargo transporter worldwide for military and comercial transports (like parts of the european Ariane rocket). Model by Thomas Ruth & Alex Kvitta, Sound by Leonid Korshunov, Paint by Johns, Collect by Alexander Khrustitskyi.
ui_manufacturer=ANTK Antonov
ui_type=An-124
ui_variation=Russia Air Cargo RA-82072
atc_heavy=1
atc_id=RA-82072
atc_airline=Governmental airgroup
atc_flight_number=RA-82072
visual_damage=1


[fltsim.7]
title=Antonov AN-124 Russian Air Force 09
sim=an124
model=
panel=
sound=
texture=7
checklists=
description=The Anotonov-124 Ruslan (Condor) has become one of the most famous cargo transporter worldwide for military and comercial transports (like parts of the european Ariane rocket). Model by Thomas Ruth & Alex Kvitta, Sound by Leonid Korshunov, Paint by Johns, Collect by Alexander Khrustitskyi.
ui_manufacturer=ANTK Antonov
ui_type=An-124
ui_variation=Russian Air Force 09
atc_heavy=1
atc_id=09
atc_airline=Antonov Airlines
atc_flight_number=09
visual_damage=1


[fltsim.8]
title=Antonov AN-124 Titan Cargo RA-82003
sim=an124
model=
panel=
sound=
texture=8
checklists=
description=The Anotonov-124 Ruslan (Condor) has become one of the most famous cargo transporter worldwide for military and comercial transports (like parts of the european Ariane rocket). Model by Thomas Ruth & Alex Kvitta, Sound by Leonid Korshunov, Paint by Johns, Collect by Alexander Khrustitskyi.
ui_manufacturer=ANTK Antonov
ui_type=An-124
ui_variation=Titan Cargo RA-82003
atc_heavy=1
atc_id=RA-82003
atc_airline=Trans Charter Titan Cargo
atc_flight_number=RA-82003
visual_damage=1


[fltsim.9]
title=Antonov AN-124 United Arab Emirates UR-ZYD
sim=an124
model=
panel=
sound=
texture=9
checklists=
description=United Arab Emirates UR-ZYD (cn 19530502843). The Anotonov-124 Ruslan (Condor) has become one of the most famous cargo transporter worldwide for military and comercial transports (like parts of the european Ariane rocket). Model by Thomas Ruth & Alex Kvitta, Sound by Leonid Korshunov, Paint by Alexander Khrustitskyi, Collect by Alexander Khrustitskyi.
ui_manufacturer=ANTK Antonov
ui_type=An-124
ui_variation=United Arab Emirates UR-ZYD
atc_heavy=1
atc_id=UR-ZYD
atc_airline=United Arab Emirates
atc_flight_number=UR-ZYD
visual_damage=1


[fltsim.10]
title=Antonov AN-124 Hrust UR-HRUST
sim=an124
model=
panel=
sound=
texture=10
checklists=
description=Personal aircraft by Alexander Khrustitskyi.  Model by Thomas Ruth & Alex Kvitta, Sound by Leonid Korshunov, Paint by Alexander Khrustitskyi, Collect by Alexander Khrustitskyi.

ui_manufacturer=ANTK Antonov
ui_type=An-124
ui_variation=Hrust UR-HRUST
atc_heavy=1
atc_id=UR-HRUST
atc_airline=Hrust
atc_flight_number=UR-HRUST
visual_damage=1


[General]
performance=4 LotarevD-18T with 229.5kN each   MTOW: 402 metrical tons    MaxPayload 150 metrical tons  Cruise speed:870km/h Max Mach 0.77  Max payload range:4500km  Max fuel range:  15400km  Max ceiling: 12000 meters
atc_type=ANTONOV
atc_model=AN124


[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI


[WEIGHT_AND_BALANCE]
max_gross_weight = 924198                       // (pounds)
empty_weight = 395428                           // (pounds)

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

max_number_of_stations = 50

station_load.0  =   "170.0,	 59.7,	-2.0,	 8.5,	Pilot"               //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.1  =   "170.0,	 59.7,	 2.0,	 8.5,	Co-Pilot"            //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.2  =  "700.0,	 50.9,	 0.0,	 8.5,	Crew"                //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.3  =  "1540.0,	 36.7,	 0.0,	 8.5,	Upper CrewDeck"          //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.4  =  "2140.0,	 -43.0,	 0.0,	 8.5,	Upper PaxDeck"          //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.5  = "0.0,	 -1.0,	 0.0,	 0.0,	Cargo"           //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 

;Moments of Inertia
empty_weight_roll_MOI    = 13352310
empty_weight_pitch_MOI   = 24223159
empty_weight_yaw_MOI     = 39531785
empty_weight_coupled_MOI = 0


[fuel]
LeftMain  =   0.0, -28.0, 4.0, 27027.0, 0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) 
RightMain =   0.0,  28.0, 4.0, 27027.0, 0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) 
LeftAux   =   0.0, -36.5, 3.0,  6784.0, 0.0    //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) 
RightAux  =   0.0,  36.5, 3.0,  6784.0, 0.0    //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=0

[airplane_geometry]
wing_area               = 6525.0                //Square feet
wing_span               = 240.5                 //Feet
wing_root_chord         = 48.8                  //Feet
wing_dihedral           = 7.0                   //Degrees
wing_incidence          = 2.0                   //Degrees
wing_twist              = -1.0                  //Degrees
oswald_efficiency_factor= 0.58                  //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 37.5                  //Degrees, wing leading edge
wing_pos_apex_lon       = 1                    //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 10                    //Feet, vertical distance from reference point, positive going up
htail_area              = 2470                  //Square feet
htail_span              = 72.8                  //Feet
htail_pos_lon           = -121.4                //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 10.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 0.0                   //Degrees
htail_sweep             = 37.5                  //Degrees, horizontal tail leading edge
vtail_area              = 1660                  //Square feet
vtail_span              = 37.1                  //Feet, tip to body
vtail_sweep             = 45.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -120.5                //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 26.1                  //Feet, vertical distance from reference point, positive going up
elevator_area           = 527                   //Square feet
aileron_area            = 325                   //Square feet
rudder_area             = 330                   //Square feet
elevator_up_limit       = 25                    //Degrees
elevator_down_limit     = 15                    //Degrees
aileron_up_limit        = 25                    //Degrees
aileron_down_limit      = 25                    //Degrees
rudder_limit            = 25.5                  //Degrees
elevator_trim_limit     = 20                    //Degrees
spoiler_limit           = 40                    //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

[Reference Speeds]
flaps_up_stall_speed    = 130.0                 //Knots True (KTAS)
full_flaps_stall_speed  = 102.0                 //Knots True (KTAS)
cruise_speed            = 475.0                 //Knots True (KTAS)
max_mach                = 0.77
max_indicated_speed     = 365.0                 //Red line (KIAS)

[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 = 20                                   // degrees
flaps-position.3 = 30                                   // degrees
flaps-position.4 = 40                                   // degrees
damaging-speed   = 200                                  // KIAS
blowout-speed    = 250                                  // KIAS
lift_scalar = 0.7
drag_scalar = 0.9
pitch_scalar= 0.9
system_type = 1                                         //Hydraulic

[flaps.1]
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.3                                  // 0.0 .. 1.0
extending-time   = 8                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 1.0                                  // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 0.3
drag_scalar = 0.1
pitch_scalar= 0.1
system_type = 1                                         //Hydraulic

[flight_tuning]
cruise_lift_scalar     = 1.0
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 0.7
aileron_effectiveness  = 0.5
rudder_effectiveness   = 0.5
pitch_stability        = 1.0
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 0.7
aileron_trim_effectiveness  = 0.5
rudder_trim_effectiveness   = 0.5

[GeneralEngineData]
engine_type = 1                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -2.0, -59.1, -2.6                 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -18.4, -33.5, -4.3                  //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 = -18.4, 33.5, -4.3                   //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.3 = -2.0, 59.1, -2.6                  //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar        = 1.0                   //Scalar for fuel flow efficiency
min_throttle_limit = -0.25;                     //Minimum percent throttle.  Generally negative for turbine reverser

[SMOKESYSTEM]
smoke.0= -2.6, -2.0, -59.1, fx_smoke_w              
smoke.1= -4.3, -18.4, -33.5, fx_smoke_w
smoke.2= -4.3, -18.4, 33.5, fx_smoke_w
smoke.3= -2.6, -2.0, 59.1, fx_smoke_w

[TurbineEngineData]
fuel_flow_gain          = 0.002                 //Gain on fuel flow
inlet_area              = 60.0                  //Square Feet, engine nacelle inlet area
rated_N2_rpm            = 29920                 //RPM, second stage compressor rated value
static_thrust           = 44577                 //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

[autopilot]
autopilot_available             = 1
flight_director_available       = 1
default_vertical_speed          = 1000.0
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=16.00
nav_integrator_control=0.17
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control  = 18.0 
gs_integrator_control    = 0.33
gs_derivative_control    = 0.00
gs_integrator_boundary   = 0.70
gs_derivative_boundary   = 0.00
yaw_damper_gain = 1.0

[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,  51.5,    0.0, -20.3, 1000.0, 0, 3.0, 70.0, 1.5, 1.5, 0.900, 12.0,  12.0, 0, 200, 230
point.1 = 1, -35.4,   -13.5, -20.5, 3000.0, 1, 3.5, 13.0, 1.0, 2.5, 0.900, 15.0,  15.0, 2, 200, 230
point.2 = 1, -35.4,    13.5, -20.5, 3000.0, 2, 3.5, 13.0, 1.0, 2.5, 0.900, 15.0,  15.0, 3, 200, 230
point.3 = 2,  84.3,    0.0,   -6.2,  700.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 5,   0,   0
point.4 = 2,  58.4,    0.0,   12.8,  700.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 6,   0,   0
point.5 = 2, -13.1,    0.0,   50.5,  700.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 9,   0,   0
point.6 = 2, -144.7,   0.0,   8.9,  700.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0
point.7 = 2, -79.1,    0.0,  -13.1,  700.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0
point.8 = 2,  56.1,    0.0,   -15.4,  700.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0
point.9 = 2, -48.2,    121.4,   3.6,  700.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0
point.10 = 2, -48.2,   -121.4,  3.6,  700.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0
point.11 = 2, -140.1,   44.3,   6.9,  700.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0
point.12 = 2, -140.1,  -44.3,   6.9,  700.0, 0, 0.0,  0.0, 0.0, 0.0, 0.000,  0.0,  0.0, 4,   0,   0

static_pitch = -1.5
static_cg_height = 18.6
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 = 1.24  //Brake scalar

[hydraulic_system]
normal_pressure = 3000.0    //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,1,1   //pumps on Eng1,2,3,4

[Views]
eyepoint = -19.05, -1.97, 9.7              ; Longitude, Latitude and Vertical position from Reference Point, (FEET)

[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 5 , 17.0
avionics           = 1, 5 , 17.0
gear_warning       = 0, 2 , 17.0
fuel_pump          = 0, 5 , 17.0
light_nav          = 0, 5 , 17.0
light_beacon       = 0, 5 , 17.0
light_landing      = 0, 5 , 17.0
light_taxi         = 0, 5 , 17.0
light_strobe       = 0, 5 , 17.0
light_panel        = 0, 5 , 17.0


[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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing                   
light.5 = 2, -144.4,    0.00,  8.2, fx_strobeh ,
light.6 = 1,  35.1,    0.00,  12.9, fx_beaconh ,
light.7 = 1,  44.2,    0.00, -15.1, fx_beaconb ,
light.8 = 4,  59.7,    0.00,   11.2, fx_vclighth,

[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 = 2 
attitude_indicator.1 = 1 

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

[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

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

[exits]
number_of_exits = 2
exit_rate.0 = 0.2                               ;Percent per second
exit_rate.1 = 0.05                               ;Percent per second

[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position=-15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=0.9

[folding_wings]
wing_fold_system_type=4                    
fold_rates=0.11,0.13                         ;Percent per second

[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 microseconds

[stall_warning]
type=2