[fltsim.0]
title=Cessna 208 Caravan Amphibian Paint2
sim=Cessna208
model=
panel=
sound=
texture=AVQ
kb_checklists=Cessna208_Check
kb_reference=Cessna208_ref
atc_id_color=0xff000000
atc_id=
atc_parking_types=RAMP
ui_manufacturer= Flotte AéroVirtuel
ui_type="C208 Caravan Amphibie"
ui_variation="AéroVirtuel Québec"
description="Textures Aérovirtuel Québec, par Jean-Pierre Fillion, Avril 2005"




[fltsim.1]
title=Cessna 208 Caravan Amphibian
sim=Cessna208
model=
panel=
sound=
texture=
kb_checklists=Cessna208_Check
kb_reference=Cessna208_ref
atc_id=N208YB
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type="C208 Caravan Amphibie"
ui_variation="Jaune et noir"
description="Si vous recherchez un nouveau défi en matière de vol, vous le trouverez aux commandes du Caravan Amphibie. L'Amphibie est le plus gros hydravion monomoteur actuellement fabriqué et convient aussi bien au transport de passagers qu'au transport de marchandises. Les flotteurs de l'Amphibie contiennent un train d'atterrissage. Vous pouvez ainsi vous poser n'importe où, sur l'eau ou sur la terre."
FSInn_IDVers=3
FSInn_IDModel=142D665E
FSInn_IDTexture=37F16286
FSInn_NetACICAO=C208
FSInn_NetALICAO=
FSInn_NetACType=L1T
FSInn_NetACLowRes=5
FSInn_NetALCallSign=
FSInn_NetACWave=L

[fltsim.2]
title=Cessna 208 Caravan Amphibian Paint1
sim=Cessna208
model=
panel=
sound=
texture=1
kb_checklists=Cessna208_Check
kb_reference=Cessna208_ref
atc_id_color=0xff000000
atc_id=N208GA
atc_airline=Gaia
atc_flight_number=1123
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type="C208 Caravan Amphibie"
ui_variation="Gaia Airlines"
description="Si vous recherchez un nouveau défi en matière de vol, vous le trouverez aux commandes du Caravan Amphibie. L'Amphibie est le plus gros hydravion monomoteur actuellement fabriqué et convient aussi bien au transport de passagers qu'au transport de marchandises. Les flotteurs de l'Amphibie contiennent un train d'atterrissage. Vous pouvez ainsi vous poser n'importe où, sur l'eau ou sur la terre."
FSInn_IDVers=3
FSInn_IDModel=142D665E
FSInn_IDTexture=9310CB4C
FSInn_NetACICAO=C208
FSInn_NetALICAO=
FSInn_NetACType=L1T
FSInn_NetACLowRes=5
FSInn_NetALCallSign=
FSInn_NetACWave=L

[fltsim.3]
title=Cessna 208 Caravan Amphibian Paint2
sim=Cessna208
model=
panel=
sound=
texture=2
kb_checklists=Cessna208_Check
kb_reference=Cessna208_ref
atc_id_color=0xff000000
atc_id=N208GB
atc_parking_types=RAMP
ui_manufacturer=Cessna
ui_type="C208 Caravan Amphibie"
ui_variation="Blanc, bleu et or"
description="Si vous recherchez un nouveau défi en matière de vol, vous le trouverez aux commandes du Caravan Amphibie. L'Amphibie est le plus gros hydravion monomoteur actuellement fabriqué et convient aussi bien au transport de passagers qu'au transport de marchandises. Les flotteurs de l'Amphibie contiennent un train d'atterrissage. Vous pouvez ainsi vous poser n'importe où, sur l'eau ou sur la terre."
FSInn_IDVers=3
FSInn_IDModel=142D665E
FSInn_IDTexture=B51D0AC2
FSInn_NetACICAO=C208
FSInn_NetALICAO=
FSInn_NetACType=L1T
FSInn_NetACLowRes=5
FSInn_NetALCallSign=
FSInn_NetACWave=L

[General]
atc_type=Cessna
atc_model=C208
editable=0
performance="Vitesse maximale\n175 noeuds            324 km\/h\n\nVitesse de croisière\n143 noeuds (8 000 livres)     265 km\/h\n130 noeuds (6 400 livres)     241 km\/h\n117 noeuds (5 200 livres)      216 km\/h\n\nMotorisation\nPratt & Whitney Canada, Inc., PT6A-114A, turbine libre limitée à 675 CV\n\nHélice\nTripale, Vitesse constante, Mise totale en drapeau, McCauley réversible, diamètre de 106 cm\n\nAutonomie maximale\n4,6 h en régime de croisière maximal à 10 000 pieds\n5,7 h en régime de croisière maximal à 20 000 pieds\n6,8 h maximales à 10 000 pieds\n8,0 h maximales à 20 000 pieds\n\nPlafond pratique\n20 000 pieds              6 096 m\n\nCapacité en carburant\n335 gal                 1 268 l\n\nPoids à vide\n4 895 livres                2 220 kg\n\nPoids total maximal\n8 035 livres               3 645 kg\n\nCharge utile\n3 140 livres                 1 424 kg\n\nLongueur\n41 pieds, 7 pouces\t               12,7 m\n\nEnvergure\n52 pieds, 1 pouce\t               15,8 m\n\nHauteur\n15 pieds, 5-1\/2 pouces          4,8 m\n\nNombre de places\njusqu'à 14"


[WEIGHT_AND_BALANCE]
max_gross_weight = 8000                         // (pounds)
empty_weight = 4895                             // (pounds)

reference_datum_position     =  13.1, 0, 0      // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     = -13.6, 0, 0      // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0  = "170.0,  -11.3, -1.5,   0.0, Pilote"              // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.1  = "170.0,  -11.3,  1.5,   0.0, Passager 2"        // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.2  = "160.0,  -13.9, -2.0,   0.0, Passager 3"        // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.3  = "160.0,  -13.9,  2.0,   0.0, Passager 4"        // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.4  =   "0.0,  -18.8, -2.0,   0.0, Passager 5"        // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.5  =   "0.0,  -18.8,  2.0,   0.0, Passager 6"        // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.6  = " 50.0,  -21.0,  0.0,   0.0, Zone de fret 3"       // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.7  =  "25.0,  -23.5,  0.0,   0.0, Zone de fret 4"       // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.8  =   "0.0,  -25.6,  0.0,   0.0, Zone de fret 5"       // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.9  =   "0.0,  -27.5,  0.0,   0.0, Zone de fret 6"       // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.10 =   "0.0,   -9.9, -5.3,  -6.5, Bagages à gauche"       // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.11 =   "0.0,   -9.9,  5.3,  -6.5, Bagages à droite"      // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 

;Moments of Inertia
empty_weight_pitch_MOI   = 7241.36
empty_weight_roll_MOI    = 5618.57
empty_weight_yaw_MOI     = 10431.43
empty_weight_coupled_MOI = 0.0

[Flaps.0]
type=1
span-outboard=0.5       // Percent span for flap position
extending-time=5.7      // Seconds, time to fully extend
system_type=0           // 0 = electrical
damaging-speed  = 175                                  // KIAS
blowout-speed   = 175                                  // KIAS
flaps-position.0= 0     // degrees
flaps-position.1=10,175     // degrees
flaps-position.2=20,150     // degrees
flaps-position.3=30,125     // degrees

[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 = 5                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -1.3, 0.0, 0.0                       //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar        = 1.12                  //Scalar for fuel flow efficiency
min_throttle_limit = -0.25                      //Minimum percent throttle.  Generally negative for turbine reverser

[propeller]
thrust_scalar           = 1.0                   //Propeller thrust scalar
propeller_type          = 0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter      = 8.8                   //Propeller Diameter, (feet)
propeller_blades        = 3                     //Number of propeller blades
propeller_moi           = 19                    //Propeller moment of inertia
beta_max                = 45                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min                = 15.6                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm             = 25520                 //Miminum governed RPM
prop_tc                 = 0.004                 //Prop time-constant
gear_reduction_ratio    = 17.4                  //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= 1                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available= 1               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather     = 700                   //Minimum RPM for prop feathering
beta_feather            = 88.0                  //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  = 1                     //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta  = 1.0                   //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta    = -14.0                 //Minimum pitch angle in reverse, (degrees)

[TurbineEngineData]
fuel_flow_gain          = 0.011                 //Gain on fuel flow
inlet_area              = 1.0                   //Square Feet, engine nacelle inlet area
rated_N2_rpm            = 33000                 //RPM, second stage compressor rated value
static_thrust           = 158                   //Lbs, max rated static thrust at Sea Level

[turboprop_engine]
power_scalar            = 1.0                   //Scalar on Turboprop power
maximum_torque          = 1865                  //Maximum torque available (ft-lbs)

[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor         = 0, 5 , 17.0
gear_motor         = 0, 5 , 17.0
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 5 , 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 2 , 17.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 0, 2 , 17.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 20, 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

[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 / Water Rudder Effectiveness  (0=Undamped, 1=Critically Damped) / 1.0 = normal
        //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,  -1.15, -5.250, -7.800, 1600, 0, 1.40, 30.0, 0.3,  2.5, 0.80, 4.0, 4.0, 0, 175.0, 175.0
point.1 = 1,  -1.15,  5.250, -7.800, 1600, 0, 1.40, 30.0, 0.3,  2.5, 0.80, 4.0, 4.0, 1, 175.0, 175.0
point.2 = 1, -16.40, -5.250, -7.700, 1600, 1, 1.50,  0.0, 0.4,  2.5, 0.80, 4.0, 4.0, 2, 175.0, 175.0
point.3 = 1, -16.40,  5.250, -7.700, 1600, 2, 1.50,  0.0, 0.4,  2.5, 0.80, 4.0, 4.0, 3, 175.0, 175.0
point.4 = 4,  -4.00, -5.250, -5.600, 1600, 0, 0.00,  0.0, 0.85, 2.5, 0.65, 0.0, 0.0, 0, 0.0, 0.0
point.5 = 4,  -4.00,  5.250, -5.600, 1600, 0, 0.00,  0.0, 0.85, 2.5, 0.65, 0.0, 0.0, 1, 0.0, 0.0
point.6 = 4, -26.35, -5.250, -4.800, 1600, 0, 0.00,  0.0, 0.95, 2.5, 0.65, 0.0, 0.0, 2, 0.0, 0.0
point.7 = 4, -26.35,  5.250, -4.800, 1600, 0, 0.00,  0.0, 0.95, 2.5, 0.65, 0.0, 0.0, 3, 0.0, 0.0
point.8 = 2, -12.90, -26.00,  3.00,  1800, 0, 0.00,  0.0, 0.0,  0.0, 0.0,  0.0, 0.0, 5, 0.0, 0.0
point.9 = 2, -12.90   26.00,  3.00,  1800, 0, 0.00,  0.0, 0.0,  0.0, 0.0,  0.0, 0.0, 6, 0.0, 0.0
point.10= 2, -36.23,   0.00,  0.00,  1800, 0, 0.00,  0.0, 0.0,  0.0, 0.0,  0.0, 0.0, 9, 0.0, 0.0
point.11= 2,  -0.50,   0.00, -2.17,  1800, 0, 0.00,  0.0, 0.0,  0.0, 0.0,  0.0, 0.0, 4, 0.0, 0.0
point.12= 2, -38.00,   0.00,  9.00,  1800, 0, 0.00,  0.0, 0.0,  0.0, 0.0,  0.0, 0.0, 7, 0.0, 0.0
point.13= 5, -30.90, -5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0,  0.0, 1.00, 1.0, 1.2, 0, 0.0, 0.0
point.14= 5, -30.90,  5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0,  0.0, 1.00, 1.1, 1.5, 0, 0.0, 0.0



max_number_of_points = 21

static_pitch=0.983             //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=7.344         //feet, altitude of CG when at rest on the ground
gear_system_type=1             //Hydraulic

[gear_warning_system]
gear_warning_available = 2     //Amphib
pct_throttle_limit =   0.1     //Percent throttle that activates warning
flap_limit_idle    =  20.1     //Flap angle that activates warning at idle
flap_limit_power   =  13.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1        //Parking brake available
toe_brakes_scale = 0.68  //Brake scalar

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

[Views]
eyepoint= -10.5, -1.4, 2.4        //(feet) longitudinal, lateral, vertical distance from reference datum

[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            
light.0 = 3, -12.80, -25.98, 2.72,  fx_navred ,
light.1 = 3, -12.80,  25.98, 2.72,  fx_navgre ,
light.2 = 3, -38.62,   0.00, 1.84,  fx_navwhi ,
light.3 = 2, -13.17, -25.98, 2.72,  fx_strobe ,
light.4 = 2, -13.17,  25.98, 2.72,  fx_strobe ,
light.5 = 1, -36.20,   0.00, 9.15,  fx_beacon ,
light.6 = 4,  -9.49,   0.00, 0.98,  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= 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=3,0

[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=1,0

[airspeed_indicators]
airspeed_indicator.0 = 1.16, -22.0

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

[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.4                               ;Percent per second

[fuel]
LeftMain  = -15.3, -1.1, 2.5, 166.0, 3.6     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -15.3,  1.1, 2.5, 166.0, 3.6     //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

[airplane_geometry]
wing_area               = 279.0                 //Square feet
wing_span               = 52.1                  //Feet
wing_root_chord         = 6.4                   //Feet
wing_dihedral           = 3.9                   //Degrees
wing_incidence          = 2.5                   //Degrees
wing_twist              = -1.7                  //Degrees
oswald_efficiency_factor= 0.7                   //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 2.96                   //Degrees, wing leading edge
wing_pos_apex_lon       = -12.3                 //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              = 39.0                  //Square feet
htail_span              = 11.7                  //Feet
htail_pos_lon           = -27.8                 //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         = 2.0                   //Degrees
htail_sweep             = 5.0                   //Degrees, horizontal tail leading edge
vtail_area              = 18.0                  //Square feet
vtail_span              = 4.8                   //Feet, tip to body
vtail_sweep             = 45.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -25.7                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 1.5                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 16.6                  //Square feet
aileron_area            = 18.3                  //Square feet
rudder_area             = 6.7                   //Square feet
elevator_up_limit       = 28.0                  //Degrees
elevator_down_limit     = 21.0                  //Degrees
aileron_up_limit        = 20.0                  //Degrees
aileron_down_limit      = 15.0                  //Degrees
rudder_limit            = 24.0                  //Degrees
elevator_trim_limit     = 19.5                  //Degrees
spoiler_limit           = 20.0                  //Degrees
spoilerons_available    = 1                     //Spoilerons Available?
aileron_to_spoileron_gain = 1                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0                 //Degrees
min_flaps_for_spoilerons = 0                    //Minimum flap handle position when spoilerons activate
spoiler_handle_available = 0                    //Defaults to True if spoiler limit > 0, else False.  Should be False for spoilerons only

[Reference Speeds]
flaps_up_stall_speed    = 72.0                  //Knots True (KCAS)
full_flaps_stall_speed  = 58.0                  //Knots True (KCAS)
cruise_speed            = 143.0                 //Knots True (KTAS)
max_mach                = 0.60
max_indicated_speed     = 175                   //Red line (KIAS)

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1000.0
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]
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

