C208B caravan

[fltsim.1]
title=Cessna Grand Caravan Paint2
sim=Cessna208B
model=
panel=
sound=
texture=2
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id_color=0xff000000
atc_id=N208EH
atc_airline=Kenmore Air
atc_flight_number=1123
atc_parking_types=RAMP
ui_manufacturer="Cessna"
ui_type="C208B Grand Caravan"
ui_variation="Kenmore Air"
ui_typerole="Single Engine TurboProp"
ui_createdby="Microsoft Corporation"
description="Wherever you want to go today, the Cessna Caravan can get you there. First introduced by Cessna in 1985, the Caravan was designed to land nearly anywhere, on land or water. Undoubtedly, it has lived up to its creators' intentions. Whether supplies need to be brought to a flooded village in the mountains of Peru, an injured person needs to be flown out from a remote lake in Alaska, or an archaeologist wants access to a tiny site in the African desert, the Caravan has what's needed to do the job."

[fltsim.2]
title=Cessna Grand Caravan Paint3
sim=Cessna208B
model=
panel=
sound=
texture=3
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id_color=0xff000000
atc_id=N208EH
atc_airline=Global Freightways
atc_flight_number=1123
atc_parking_types=RAMP
ui_manufacturer="Cessna"
ui_type="C208B Grand Caravan"
ui_variation="Global Freightways"
ui_typerole="Single Engine TurboProp"
ui_createdby="Microsoft Corporation"
description="Wherever you want to go today, the Cessna Caravan can get you there. First introduced by Cessna in 1985, the Caravan was designed to land nearly anywhere, on land or water. Undoubtedly, it has lived up to its creators' intentions. Whether supplies need to be brought to a flooded village in the mountains of Peru, an injured person needs to be flown out from a remote lake in Alaska, or an archaeologist wants access to a tiny site in the African desert, the Caravan has what's needed to do the job."

[fltsim.3]
title=Cessna Grand Caravan
sim=Cessna208B
model=
panel=
sound=
texture=
kb_checklists=Cessna208B_Check
kb_reference=Cessna208B_ref
atc_id=N208BC
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer="Cessna"
ui_type="C208B Grand Caravan"
ui_variation=" White"
ui_typerole="Single Engine TurboProp"
ui_createdby="Microsoft Corporation"
description="Wherever you want to go today, the Cessna Caravan can get you there. First introduced by Cessna in 1985, the Caravan was designed to land nearly anywhere, on land or water. Undoubtedly, it has lived up to its creators' intentions. Whether supplies need to be brought to a flooded village in the mountains of Peru, an injured person needs to be flown out from a remote lake in Alaska, or an archaeologist wants access to a tiny site in the African desert, the Caravan has what's needed to do the job."

[General]
atc_type=Cessna
atc_model=C208
editable=0
performance="Maximum Speed\n175 kts            324 km\/hr\n\nCruise Speed\n164 kts \t        305 km\/hr at 20,000 ft\n\nEngine\nPratt & Whitney Canada, Inc., PT6A-114A Free Turbine Flat Rated at 675 Shaft hp  \n\nPropeller\nThree-Bladed, Constant Speed, Full Feathering, Reversible  McCauley, 106-inch diameter\n\nMaximum Endurance\n5.1 hours maximum cruise at 10,000 ft\n6.6 hours maximum cruise at 18,000 ft\n6.4 hours maximum range at 10,000 ft\n7.2 hours maximum range at 18,000 ft\n\nService Ceiling\n22,800 ft            6,949 m\n\nFuel Capacity\n335  gal              1,268 L\n\nEmpty Weight\n4,575 lb              2,075 kg\n\nMaximum Gross Weight\n8,785 lb\t            3,985 kg\n\nUseful Load\n4,000 lb\t            1,814 kg\n\nLength\n41 ft, 7 in             12.7 m\n\nWingspan\n52 ft, 1 in\t            15.8 m\n\nHeight\n15 ft, 5-1\/2 in      4.8 m\n\nSeating\nUp to 14"
Category = airplane

[CameraDefinition.0]
Title = "Side Door"
Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description = View of the landing gear and left wing inboard flaps
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .52
ShowWeather = Yes
InitialXyz = -2.0, 0.1, -2.5
InitialPbh = 4, 0, 7
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title = "Tail"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = 0, 2.5, -20.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.2]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 10.8, 0.6, 0.0
InitialPbh = 6, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[CameraDefinition.3]
Title = "Left Wing"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -10.8, 0.6, 0.0
InitialPbh = 6, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum

[CameraDefinition.001]
Title = "Right Seat"
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 = .6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=.73, 0.0, 0.0
InitialPbh=2, 0, 0

[CameraDefinition.002]
Title = "Radios"
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 = 1.05
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.5, 0.10, 0.12
InitialPbh=28.0, 0, 0

[CameraDefinition.003]
Title = "Engine Controls"
Guid = {a5741a54-ea6d-4580-9709-c99161e38a83}
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=0.4, -0.06, -0.1
InitialPbh=39.5, 0, 0

[CameraDefinition.004]
Title = "Switches"
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 = 1.0
SmoothZoomTime = 2.0
ZoomPanScalar = 1.15
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.3, -0.1, 0.1
InitialPbh=32.0, 0, 1

[WEIGHT_AND_BALANCE]
max_gross_weight = 8785                          // (pounds)
empty_weight = 4575                              // (pounds)

reference_datum_position     =  16.2, 0, 0       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     = -15.4, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0 = 170, -11.3, -1.5, 0.0         // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170, -11.3,  1.5, 0.0         // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 0,   -13.9, -1.5, 0.0         // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = 0,   -13.9,  1.5, 0.0         // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = 170, -17.2, -1.5, 0.0         // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = 170, -17.2,  1.5, 0.0         // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = 150, -20.2, -1.5, 0.0         // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = 150, -20.2,  1.5, 0.0         // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = 0,   -23.2, -1.5, 0.0         // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = 0,   -23.2,  1.5, 0.0         // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10= 0,   -10.6,  0.0,-5.0         // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11= 0,   -15.2,  0.0,-5.0         // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.12= 50,  -19.4,  0.0,-5.0         // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.13= 50,  -24.6,  0.0,-5.0         // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_name.0 = "Pilot"       
station_name.1 = "Passenger 2"
station_name.2 = "Passenger 3"
station_name.3 = "Passenger 4"
station_name.4 = "Passenger 5"
station_name.5 = "Passenger 6"
station_name.6 = "Passenger 7"
station_name.7 = "Passenger 8"
station_name.8 = "Passenger 9"
station_name.9 = "Passenger 10"
station_name.10= "Cargo Pod 1"
station_name.11= "Cargo Pod 2"
station_name.12= "Cargo Pod 3"
station_name.13= "Cargo Pod 4"

;Moments of Inertia
empty_weight_pitch_MOI   = 8874.87
empty_weight_roll_MOI    = 6026.96
empty_weight_yaw_MOI     = 11858.54
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 = 5                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -2.4, 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)

[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

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

[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, -16.72, -25.80,  3.85,  fx_navredh
light.1 = 3, -16.28,  25.80,  3.85,  fx_navgreh
light.2 = 3, -42.28,   0.00,  2.12,  fx_navwhih
light.3 = 2, -16.90, -25.90,  3.85,  fx_strobeh
light.4 = 2, -16.45,  25.90,  3.85,  fx_strobeh
light.5 = 1, -40.10,   0.00, 10.01,  fx_beaconh
//light.6 = 4, -11.61,   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 = 1.183, -24.75

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

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=0.150000

[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 200.0

        //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]
point.0 = 1,  -4.70,  0.00, -5.40, 1500, 0, 0.5, 22.0, 0.3, 2.5, 0.7, 0.0, 0.0, 0
point.1 = 1, -18.00, -6.00, -5.40, 2500, 1, 0.5,  0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 2
point.2 = 1, -18.00,  6.00, -5.40, 2500, 2, 0.5,  0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 3
point.3 = 2, -15.90, -26.0,  3.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5
point.4 = 2, -15.90   26.0,  3.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6
point.5=  2, -39.23,   0.0,  0.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9
point.6=  2,  -2.50,   0.0, -2.17, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4
point.7=  2, -42.00,   0.0, 10.00, 1800, 0, 0.0,  0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7

max_number_of_points = 21

static_pitch    = 0.24          //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height= 5.11          //feet, altitude of CG when at rest on the ground

[brakes]
parking_brake = 1        //Parking brake available
toe_brakes_scale = 0.68  //Brake scalar
auto_brakes = 0

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

[Views]
eyepoint = -12.5, -1.2, 2.19     //(feet) longitudinal, lateral, vertical distance from reference datum

[fuel]
LeftMain  = -17.0, -1.1, 2.5, 166.0, 3.6     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -17.0,  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

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

[exits]
number_of_exits = 4
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.4                               ;Percent per second
exit_rate.2 = 0.4                               ;Percent per second
exit_rate.3 = 0.4                               ;Percent per second

[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              = 0.0                   //Degrees, wing leading edge
wing_pos_apex_lon       = -14.5                 //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           = -30.9                 //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           = -28.8                 //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
spoiler_extension_time  = 0.2         //Seconds
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
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    = 78.0                  //Knots True (KCAS)
full_flaps_stall_speed  = 60.8                  //Knots True (KCAS)
cruise_speed            = 155.0                 //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
stick_shaker=0

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