[fltsim.0]
title=Piper PA28R201
sim=PA28R201
model=
panel=DEILU
sound=
texture=DEILU
prop_anim_ratio=1.1
kb_checklists=PA28R201_check
kb_reference=PA28R201_ref
atc_id=D-EILU
ui_manufacturer=Piper
ui_type=PA-28R-201
ui_variation=D-EILU
ui_typerole=Einmotoriges Propellerflugzeug
ui_createdby=Hauke Keitel
description=Die Piper 28-Serie gehört zu den erfolgreichsten Konstruktionen für die allgemeine Luftfahrt überhaupt. Die hervorragende Güte des Grundentwurfs war ein dauerhafter Garant für die Vielseitigkeit und die langanhaltende Beliebtheit dieses Luftfahrzeugs. Zahlreiche Weiterentwicklungen und eine umfassende Einsetzbarkeit zeichnen die vorzügliche PA 28 aus.
[fltsim.1]
title=Piper PA28R201-2
sim=PA28R201
model=2
panel=2
sound=
texture=HUSCH
prop_anim_ratio=1.1
kb_checklists=PA28R201_check
kb_reference=PA28R201_ref
atc_id=H-USCH
ui_manufacturer=Piper
ui_type=PA-28R-201
ui_variation=H-USCH
ui_typerole=Einmotoriges Propellerflugzeug
ui_createdby=Hauke Keitel
description=Die Piper 28-Serie gehört zu den erfolgreichsten Konstruktionen für die allgemeine Luftfahrt überhaupt. Die hervorragende Güte des Grundentwurfs war ein dauerhafter Garant für die Vielseitigkeit und die langanhaltende Beliebtheit dieses Luftfahrzeugs. Zahlreiche Weiterentwicklungen und eine umfassende Einsetzbarkeit zeichnen die vorzügliche PA 28 aus.
[fltsim.2]
title=Piper PA28R201-3
sim=PA28R201
model=2
panel=2
sound=
texture=N1309H
prop_anim_ratio=1.1
kb_checklists=PA28R201_check
kb_reference=PA28R201_ref
atc_id=H-USCH
ui_manufacturer=Piper
ui_type=PA-28R-201
ui_variation=N1309H
ui_typerole=single-engine monoplane
ui_createdby=Hauke Keitel
description=The Piper 28R is a single-engine monoplane with retractable gear.It is one of the most successful constructions for the general aviation. The excellent goodness of the basic draught was a lasting guarantor for the versatility and the prolonged popularity of this airplane. Numerous advancements and a comprehensive usability distinguish the superior PA 28.
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[fltsim.3]
title=Piper_PA28Rai1
sim=PA28RAI
model=ai
panel=
sound=
texture=DEILU
prop_anim_ratio=1.1
atc_id=D-EILU
ui_manufacturer=Piper
ui_type=PA-28R-201
ui_variation=AI
ui_typerole=Einmotoriges Propellerflugzeug
ui_createdby=Hauke Keitel
[fltsim.4]
title=Piper_PA28Rai2
sim=PA28RAI
model=ai
panel=
sound=
texture=HUSCH
prop_anim_ratio=1.1
atc_id=H-USCH
ui_manufacturer=Piper
ui_type=PA-28R-201
ui_variation=AI
ui_typerole=Einmotoriges Propellerflugzeug
ui_createdby=Hauke Keitel
[fltsim.5]
title=Piper_PA28Rai3
sim=PA28RAI
model=ai
panel=
sound=
texture=N1309H
prop_anim_ratio=1.1
atc_id=N1309H
ui_manufacturer=Piper
ui_type=PA-28R-201
ui_variation=AI
ui_typerole=Einmotoriges Propellerflugzeug
ui_createdby=Hauke Keitel
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[General]
atc_type=PIPER
atc_model=28R
editable=0
performance=Reisegeschwindigkeit\n173 Meilen pro Stunde 158 Knoten 254 km\/h\n\nTriebwerk\nLycoming IO-360-C1C6 Vierzylinder fahrtwindgekühlt, 200 PS\n\nPropeller\nMcCauley-Zweiblatt, konstante Drehzahl \n\nMaximale Reichweite\n880 nm 1.630 km @55%\n\nDienstgipfelhöhe\n16.200 Fuß 4.983 m\n\nTreibstoffmenge\n72 Gallonen 273 l\n\nLeergewicht\n1.795 lbs 814 kg\n\nMaximales Bruttogewicht \n2.650 lbs 1.247 kg\n\nLänge\n24,7 Fuß 7,5 m\n\nSpannweite\n35,4 Fuß 10,8 m\n\nHöhe\n7,9 Fuß 2,4 m\n\nSitzplätze\n4\n\nZuladung\n963 lbs 437 kg
category=Airplane
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[CameraDefinition.001]
Title=Trimmung
Guid={195EAB58-9E4A-4E2A-A34C-A8D9D948F078}
Origin=Virtual Cockpit
MomentumEffect=No
SnapPbhAdjust=None
SnapPbhReturn=False
PanPbhAdjust=None
PanPbhReturn=False
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=.65
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.0, -0.0, 0.0
InitialPbh=60, 10, 80
[CameraDefinition.002]
Title=Rechter Sitz
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=0.75
SmoothZoomTime=0.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.45, 0.0, 0.0
InitialPbh=10, 0, 0
[CameraDefinition.003]
Title=Funkgruppe
Guid={195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin=Virtual Cockpit
MomentumEffect=Yes
SnapPbhAdjust=Swivel
SnapPbhReturn=False
PanPbhAdjust=Swivel
PanPbhReturn=False
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=1.4
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.2, -0.1, -0.2
InitialPbh=8.0, 0, 13
[CameraDefinition.004]
Title=EGT
Guid={195EAB58-9E4A-3E2A-A34C-A8D9D948F078}
Origin=Virtual Cockpit
MomentumEffect=Yes
SnapPbhAdjust=Swivel
SnapPbhReturn=False
PanPbhAdjust=Swivel
PanPbhReturn=False
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=1.05
SmoothZoomTime=2.0
ZoomPanScalar=1.0
ShowWeather=Yes
XyzAdjust=TRUE
ShowLensFlare=FALSE
Category=Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.29, -0.35, 0
InitialPbh=10, 0, 357
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[WEIGHT_AND_BALANCE]
max_gross_weight=2750 // (pounds)
empty_weight=1664 // (pounds)
//CG_forward_limit=-6.67 //1800 lbs
CG_forward_limit=-7.275 //2750 lbs
CG_aft_limit=-7.75 //all weights
reference_datum_position=7.30, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-7.22, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
station_load.0=180, -6.71, -1.5, 0.6 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=180, -6.71, 1.5, 0.6 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=000, -9.84, -1.5, 0.4 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=000, -9.84, 1.5, 0.4 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4=015, -11.9, 0.0, 0.0 // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.0 = "Flugzeugführer"
station_name.1 = "Fluggast vorne"
station_name.2 = "Fluggast hinten links"
station_name.3 = "Fluggast hinten rechts"
station_name.4 = "Gepäck"
;Moments of Inertia
empty_weight_pitch_MOI=1236.6
empty_weight_roll_MOI=1205.1
empty_weight_yaw_MOI=3032.5
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=0.0, 0.0, -0.2 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.0 //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=90.7 //Cubic inches per cylinder
compression_ratio=8.7 //Compression ratio
number_of_cylinders=4 //Number of cylinders
max_rated_rpm=2700 //Max rated RPM
max_rated_hp=200 //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=0.4 //Starter torque factor
turbocharged=0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=0 //Max design manifold pressure, (inHg)
min_design_mp=0 //Min design manifold pressure, (inHg)
critical_altitude=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 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=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=0.8 //Scalar on idle RPM friction
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=6.33 //Propeller Diameter, (feet)
propeller_blades=2 //Number of propeller blades
propeller_moi=7.4 //Propeller moment of inertia
beta_max=29.0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=13.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=1400 //Miminum governed RPM
prop_tc=0.1 //Prop time-constant
gear_reduction_ratio=1.0 //Propeller gear reduction ratio
fixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=0 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=0 //Minimum RPM for prop feathering
beta_feather=0 //Feathering pitch angle (degrees)
power_absorbed_cf=0 //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 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0 //Minimum pitch angle in reverse, (degrees)
[electrical]
max_battery_voltage=12.0
generator_alternator_voltage=13.0
max_generator_alternator_amps=60.0
;/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
[contact_points]
//gear--0------1-------2-------3------4---5---6-------7----8------9----10----11---12--13--14-----15
point.0=1, -0.77, 0.0, -3.97, 1200, 0, 0.50, 30.0, 0.20, 2.5, 0.794, 3.5, 3.5, 0, 107.0, 129.0
point.1=1, -8.34, -5.25, -3.78, 1700, 1, 0.60, 0.0, 0.25, 2.5, 0.808, 4.7, 4.7, 1, 107.0, 129.0
point.2=1, -8.34, 5.25, -3.78, 1700, 2, 0.60, 0.0, 0.25, 2.5, 0.808, 5.2, 5.2, 2, 107.0, 129.0
//scrapes
point.3=2, -8.72, -17.72, 0.38, 1000, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -8.72 17.72, 0.38, 1000, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -19.64, 0.00, -1.61, 1000, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, -21.99, 0.00, 4.34, 1000, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 4, 0.0, 0.0
point.7=2, 0.72, 0.00, -2.99, 1000, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0.0, 0.0, 7, 0.0, 0.0
point.8=5
max_number_of_points=21
static_pitch = 1.2
static_cg_height = 3.86
gear_system_type=0 //Electric
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 10.0 //Percent throttle that activates warning
flap_limit_idle = 11.0 //Flap angle that activates warning at idle
flap_limit_power = 11.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.8 //Brake scalar
differential_braking_scale = 0.2 //Delta on the amount of brake when the rudder pedals deflected
auto_brakes=0
[hydraulic_system]
normal_pressure=0.0 //PSI
[fuel]
;/Tanks Position and capacity:
;/Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -7.92, -6.2, -0.5, 36, 1
RightMain = -7.92, 6.2, -0.5, 36, 1
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
;/Fuel type: 1 = Avgas, 2 = JetA
fuel_type=1
number_of_tank_selectors=1
electric_pump=1
engine_driven_pump=0
[Views]
eyepoint = -7.9, -0.85, 1.15 //Longitudinal (feet), Lateral (feet), Vertical (feet)
[flaps.0]
type=1 // 1 - tail, 2 - lead
span-outboard=0.4 // 0.0 .. 1.0
extending-time=3 // seconds
flaps-position.0=0 // degrees
flaps-position.1=10 // degrees
flaps-position.2=25 // degrees
flaps-position.3=40 // degrees
damaging-speed=110 // KIAS
blowout-speed=140 // KIAS
lift_scalar=1.0
drag_scalar=1.0
pitch_scalar=1.0
system_type=3 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[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
[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=100, 180
aileron=200, 1000
rudder=200, 1000
//[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
//direction_indicator.1=1
[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=1,1 //Turn AND Bank
[airspeed_indicators]
airspeed_indicator.0=1
[vacuum_system]
max_pressure=5.15 //PSI
vacuum_type=1 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
engine_map=1
[pneumatic_system]
max_pressure=0.000000
[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
[stall_warning]
type=2
stick_shaker=0
[deice_system]
structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -8.60, -17.72, 0.38, fx_navred,
light.1 = 3, -8.60, 17.72, 0.38, fx_navgre,
light.2 = 3, -22.69, 0.00, 3.89, fx_navwhi,
light.3 = 1, -21.06, 0.00, 4.47, fx_beacon,
light.4 = 2, -8.82, -17.72, 0.38, fx_strobe,
light.5 = 2, -8.82, 17.72, 0.38, fx_strobe,
light.6 = 5, -0.58, 0.00, -1.21, fx_navwhi,
light.7 = 4, -7.90, 0.00, 1.15, fx_vclight,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[exits]
number_of_exits=3
exit.0=0.4 // (0=Main 1=Cargo 2=Emergency)
exit.1=0.4 // (0=Main 1=Cargo 2=Emergency)
exit.2=0.4 // (0=Main 1=Cargo 2=Emergency)
/////////////////////////////////////////////////////////
[airplane_geometry]
wing_area=170.0 //Square feet
wing_span=35.0 //Feet
wing_root_chord=5.2 //Feet
wing_dihedral=5.5 //Degrees
wing_incidence=2.9 //Degrees
wing_twist=-0.9 //Degrees
oswald_efficiency_factor=0.70 //Measure of lift effeciency of wing
wing_winglets_flag=0 //Are winglets available?
wing_sweep=1.0 //Degrees, wing leading edge
wing_pos_apex_lon=-6.05 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=-0.45 //Feet, vertical distance from reference point, positive going up
htail_area=27.08 //Square feet
htail_span=10.83 //Feet
htail_pos_lon=-19.36 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=-0.49 //Feet, vertical distance from reference point, positive going up
htail_incidence=0.0 //Degrees
htail_sweep=0.0 //Degrees, horizontal tail leading edge
vtail_area=11.9 //Square feet
vtail_span=4.0 //Feet, tip to body
vtail_sweep=42.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-18.76 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=2.1 //Feet, vertical distance from reference point, positive going up
elevator_area=27.08 //Square feet
aileron_area=11.27 //Square feet
rudder_area=4.6 //Square feet
elevator_up_limit=18.0 //Degrees
elevator_down_limit=03.0 //Degrees
aileron_up_limit=30.0 //Degrees
aileron_down_limit=15.0 //Degrees
rudder_limit=27.0 //Degrees
elevator_trim_limit=12.0 //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=4.0 //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=-1.5 //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down=-1.5 //Design G load tolerance (negative, flaps down)
load_safety_factor=1.5 //Design G load safety factor
[Reference Speeds]
flaps_up_stall_speed=62.0 //Knots True (KTAS)
full_flaps_stall_speed=56.0 //Knots True (KTAS)
cruise_speed=121.0 //Knots True (KTAS) at 23/2300/4500ft
max_indicated_speed=183.0 //Red line (KIAS)
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=0.0
autothrottle_available=0
pitch_takeoff_ga=8.0
default_pitch_mode=2
default_bank_mode=1
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=23.5
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]
gear_bump_nose_magnitude=6000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=6000 ; 0 - 10000
gear_bump_left_direction=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=6000 ; 0 - 10000
gear_bump_right_direction=00500 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=3250 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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
[direction_indicators]
direction_indicator.0=1,0
