[fltsim.0]
title=PTDI N-250-100 PA2
sim=N250
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=PK-XNK
ui_manufacturer="IPTN"
ui_type="N-250-100"
ui_variation="PA 2"
ui_typerole="Twin Engine TurboProp"
ui_createdby="haditahir"
description="N250."

[fltsim.1]
title=PTDI N-250-100 Putih
sim=N250
model=1
panel=
sound=
texture=1
kb_checklists=
kb_reference=
atc_id_color=0xffffffffff
atc_id=PK-XNK
ui_manufacturer="IPTN"
ui_type="N-250-100"
ui_variation="Putih"
ui_typerole="Twin Engine TurboProp"
ui_createdby="haditahir"
description="N250."

[General]
atc_type=IPTN
atc_model=N250
editable=0
performance="Cruise Speed\t\n315 kts            616 km\/h\n\nEngines\t\nAllison AE-2100 C    3 200 shp\n\nMaximum Range\t\n11 481 km\n\nService Ceiling\t\n7 620 m\n\nFuel Capacity\t\n4 200 kg\n\nMaximum Takeoff Weight \n24 800 kg\n\nLength\t\n28 153 mm\n\nWingspan\t\n28 m\n\nHeight\t\n8 785 mm\n\nSeating\t\nUp to 64\n\nUseful Load\t\n4 900 kg"
Category = airplane

[CameraDefinition.0]
Title = "Ekor"
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, 3.5, -40.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title = "Sayap Kanan"
Guid = {E3E97D3E-4075-457f-96A1-253B58D19052}
Description = Pandangan dari sayap kanan
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 20, 1.0, 3.0
InitialPbh = 6, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[CameraDefinition.2]
Title = "Sayap Kiri"
Guid = {FEE3C4E6-95B2-4b2a-A122-756E73CF186F}
Description = Pandangan dari sayap kiri
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -20, 1.0, 3.0
InitialPbh = 6, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum

[CameraDefinition.001]
Title = "Engine Controls"
Guid = {5910B228-AADE-47e1-8B9F-BA90FA110936}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.2
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.0, 0.25, -0.2
InitialPbh=48, 0, 27

[CameraDefinition.002]
Title = "Ko-Pilot"
Guid = {73687666-15A3-48b2-8D40-AE04DB4031DB}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.3
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=1, 0 , 0
InitialPbh=0, 0, 0

[CameraDefinition.003]
Title = "Belakang"
Guid = {5D89B263-27BA-4301-85CD-99D102D7F2F3}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.3
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.4, -0.2, -8
InitialPbh=0, 0, 0

[WEIGHT_AND_BALANCE]
max_gross_weight = 54675	                   // (pounds)
empty_weight = 34612                            // (pounds)

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

max_number_of_stations = 50

station_load.0 = 170,  37.75, -1.7, -1.2        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170,  37.75,  1.7, -1.2        //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2	=	680	,	28	,	0	,	-2
station_load.3	=	680	,	25.5	,	0	,	-2
station_load.4	=	680	,	23	,	0	,	-2
station_load.5	=	680	,	20.5	,	0	,	-2
station_load.6	=	680	,	18	,	0	,	-2
station_load.7	=	680	,	15.5	,	0	,	-2
station_load.8	=	680	,	13	,	0	,	-2
station_load.9	=	680	,	10.5	,	0	,	-2
station_load.10	=	680	,	8	,	0	,	-2
station_load.11	=	680	,	5.5	,	0	,	-2
station_load.12	=	680	,	3	,	0	,	-2
station_load.13	=	680	,	0.5	,	0	,	-2
station_load.14	=	680	,	-2	,	0	,	-2
station_load.15	=	680	,	-4.5	,	0	,	-2
station_load.16	=	680	,	-7	,	0	,	-2
station_load.17	=	340	,	-12	,	2.4	,	-2
station_load.18	=	340	,	-14.5	,	1.6	,	-2
station_load.19	=	340	,	-25.9	,	0	,	0.5

station_name.0 = "Pilot"      
station_name.1 = "Ko-Pilot"   
station_load.2	=	"Penumpang – Baris	1"
station_load.3	=	"Penumpang – Baris	2"
station_load.4	=	"Penumpang – Baris	3"
station_load.5	=	"Penumpang – Baris	4"
station_load.6	=	"Penumpang – Baris	5"
station_load.7	=	"Penumpang – Baris	6"
station_load.8	=	"Penumpang – Baris	7"
station_load.9	=	"Penumpang – Baris	8"
station_load.10	=	"Penumpang – Baris	9"
station_load.11	=	"Penumpang – Baris	10"
station_load.12	=	"Penumpang – Baris	11"
station_load.13	=	"Penumpang – Baris	12"
station_load.14	=	"Penumpang – Baris	13"
station_load.15	=	"Penumpang – Baris	14"
station_load.16	=	"Penumpang – Baris	15"
station_load.17	=	"Penumpang – Baris	16"
station_load.18	=	"Penumpang – Baris	17"
station_load.19	=	"Kargo"


;Moments of Inertia
empty_weight_pitch_MOI  = 231763.000
empty_weight_roll_MOI   = 243463.000
empty_weight_yaw_MOI    = 327461.000
empty_weight_coupled_MOI= 1300.000

[flight_tuning]
cruise_lift_scalar     =1.3
parasite_drag_scalar   =0.5
induced_drag_scalar    =1.0
elevator_effectiveness =2.0
aileron_effectiveness  =2.3
rudder_effectiveness   =2.0
pitch_stability        =1.5
roll_stability         =1.4
yaw_stability          =1.5
elevator_trim_effectiveness =0.9
aileron_trim_effectiveness  =0.9
rudder_trim_effectiveness   =0.9

[GeneralEngineData] //sdh
engine_type = 5                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 7.0398, -12.5753, 0.1682             //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 7.0398,  12.5753, 0.1682             //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar   = 0.8                        //Scalar for fuel flow efficiency
min_throttle_limit = -0.50;                     //Minimum percent throttle.  Generally negative for turbine reverser

[propeller] //sdh
thrust_scalar           = 1.278                 //Propeller thrust scalar
propeller_type          = 0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter      = 12.5                  //Propeller Diameter, (feet) 
propeller_blades        = 6                     //Number of propeller blades 
propeller_moi           = 115                   //Propeller moment of inertia
beta_max                = 35                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min                = 20.2                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm             = 25555                 //Miminum governed RPM
prop_tc                 = 0.004                 //Prop time-constant
gear_reduction_ratio    = 13.98                 //Propeller gear reduction ratio ,sdh
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     = 1                     //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     = 770                   //Minimum RPM for prop feathering
beta_feather            = 79.3                  //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] //sdh
fuel_flow_gain          = 0.011
inlet_area              = 1.1
rated_N2_rpm            = 29920.000
static_thrust           = 1500.000
afterburner_available= 0

[turboprop_engine] //sdh
power_scalar            = 1.3                   //Scalar on Turboprop power
maximum_torque          = 7956.865              //Maximum torque available (ft-lbs)
max_rpm_mechanical_efficiency_scalar=0.99
idle_rpm_mechanical_efficiency_scalar=0.618
max_rpm_friction_scalar=0.718
idle_rpm_friction_scalar=0.718



[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

        //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,  39.3386,   0.00, -9.5, 1181, 0, 0.9843, 60, 0.4009, 1.1, 0.9516,  4.8,  4.8, 0, 184.0, 184.0
point.1=1,  -5.5175,  -7.2427, -10.5, 1574, 1, 1.6404,  0.0, 1.192022, 1.1, 0.8152,  4.5,  5.2, 2, 184.0, 184.0
point.2=1,  -5.5175,   7.2427, -10.5, 1574, 2, 1.6404,  0.0, 1.192022, 1.1, 0.8152,  4.8,  4.9, 3, 184.0, 184.0
point.3=2,  -3.33, -23.92, -3.00,  787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 5, 0.0, 0.0
point.4=2,  -3.33,  23.92, -3.00,  787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 6, 0.0, 0.0
point.5=2, -22.67,   0.00,  0.00,  787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 9, 0.0, 0.0
point.6=2,  23.08,   0.00, -1.50,  787, 0, 0.000,  0.0, 0.000, 0.0, 0.0000,  0.0,  0.0, 4, 0.0, 0.0

static_pitch = 0.0
static_cg_height = 10
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    = 15.0     //Flap angle that activates warning at idle
flap_limit_power   = 30.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 1.0  //Brake scalar
auto_brakes = 1

[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 = 37.456, -1.8045, 1.2487

[exits]
number_of_exits = 5
exit.0 = 0.4, 31.4307, -4.3537, -0.4663, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.1 = 0.4, 31.1684, 4.5548,  -0.9511, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.2 = 0.4, -11.3243, 4.5073,  -1.10676, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.3 = 0.4, -20.3576, -4.0521,  -1.0273, 1 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.4 = 0.4, -11.385, -4.6033,  -1.1452, 2 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)

[flaps.0] //sudah
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0
extending-time   = 5                                    // 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   = 150                                  // KIAS
blowout-speed    = 250                                  // KIAS

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

[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=1.000000

[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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
//light.0 = 3,   8, -45.5,  5.1, fx_navredm ,
//light.1 = 3,   8,  45.5,  5.1, fx_navgrem ,
//light.2 = 3, -31.20,   0.00,  9.75, fx_navwhi ,
light.3 = 1,-41.996,   0.00,20.232, fx_beaconh ,
light.4 = 1, 19.491,   0.00,-6.186, fx_beaconb ,
//light.5 = 2, 7.9, -45.6,  5.1, fx_strobe ,
//light.6 = 2, 7.9,  45.6,  5.1, fx_strobe ,
light.7 = 4,     37,   0.00,  2.5, fx_vclighth,
light.8 = 4,     -2,   0.00,  2., fx_vclightwhi,
light.9 = 4,     14,   0.00,  2., fx_vclightwhi,
light.10 = 4,     6,   0.00,  2., fx_vclightwhi,
light.11 = 4,    22,   0.00,  2., fx_vclightwhi,


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

[fuel]
LeftMain  = 7.5, -7.02, 4.0, 687, 0.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = 7.5,  7.02, 4.0, 687, 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=1

[airplane_geometry] //sdh
wing_area               = 788	      		    //Square feet
wing_span               = 91.9                  //Feet
wing_root_chord         = 9.26                  //Feet
wing_dihedral           = 3.0                   //Degrees
wing_incidence          = 1.0                   //Degrees
wing_twist              = -1.5                  //Degrees
oswald_efficiency_factor= 0.7                   //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 5.0                   //Degrees, wing leading edge
wing_pos_apex_lon       = -1.5                  //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 5.28                  //Feet, vertical distance from reference point, positive going up
htail_area              = 166.7                 //Square feet
htail_span              = 29.7                  //Feet
htail_pos_lon           = -66                   //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 12                    //Feet, vertical distance from reference point, positive going up
htail_incidence         = 0.5                   //Degrees
htail_sweep             = 9.50                  //Degrees, horizontal tail leading edge
vtail_area              = 225.41                //Square feet
vtail_span              = 16.43                 //Feet, tip to body
vtail_sweep             = 33.5                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -36                   //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 12                    //Feet, vertical distance from reference point, positive going up
elevator_area           = 152.2                 //Square feet
aileron_area            = 48.5                  //Square feet
rudder_area             = 58.2                  //Square feet
elevator_up_limit       = 27.5                  //Degrees
elevator_down_limit     = 20.6                  //Degrees
aileron_up_limit        = 19.5                  //Degrees
aileron_down_limit      = 14.9                  //Degrees
rudder_limit            = 33.5                  //Degrees
elevator_trim_limit     =  5.0                  //Degrees
spoiler_limit           = 60.0                  //Degrees
spoiler_extension_time  = 2.0			//Seconds
spoilerons_available    = 0                     //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
positive_g_limit_flaps_up  =  4.0               //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down=  3.0               //Design G load tolerance (positive, flaps down) 
negative_g_limit_flaps_up  = -3.0               //Design G load tolerance (negative, flaps up) 
negative_g_limit_flaps_down= -2.0               //Design G load tolerance (negative, flaps down) 
load_safety_factor         =  1.5               //Design G load safety factor 
fly_by_wire = 1

[Reference Speeds] //sdh
flaps_up_stall_speed    = 112.0                 //Knots True (KTAS)
full_flaps_stall_speed  = 90.0                  //Knots True (KTAS)
cruise_speed            = 330.0                 //Knots True (KTAS)
max_mach                = 0.7
max_indicated_speed     = 363                   //Red line (KIAS)

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
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=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
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

[forcefeedback]
stick_shaker_magnitude=5000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
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=9000           ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=27000         ; 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

[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