[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