Aircraft selection

[Ener]

I run aircraft index in Ideal Flight Prof. (P3D v4.5) but there are some planes not showing in the aircrat selection.
How can I add these ?

[Steve Waite]

how are they installed - xml in Add-ons?

[Steve Waite]

There are various ways to point to a folder with planes. if you can show me the xml or describe the folders where they are located I can show you what to do.

They should all be picked up automatically however.

[Ener]

A2A planes are in Documents/Prepar3D v4 Addons and are not showing in the aircraft selection.
I have the Real Air Duke and Turbine in same folder and these are showing up.

My Milviz KA 350i is in Pepar3D/SimObjects/Airplanes but not showing in the ID10 selection. My other planes which are in the same folder are showing up.

[Steve Waite]

Can you show me the xml in the addon folder, that's what IF refers to.

All planes in SimObjects\Airplanes are automatically included. Do they appear in the AI subsection. Can you check in the IF htm aircraft list?

[Ener]

Do you mean these xml ?

<?xml version="1.0" encoding="UTF-8"?>
<SimBase.Document id="add-on" version="4,0" Type="AddOnXml"><AddOn.Name>A2A</AddOn.Name><AddOn.Description>Aircraft by A2A Simulations Inc.</AddOn.Description><AddOn.Component><Category>Effects</Category><Path>Effects</Path></AddOn.Component><AddOn.Component><Category>Fonts</Category><Path>Fonts</Path></AddOn.Component><AddOn.Component><Category>Gauges</Category><Path>Gauges</Path></AddOn.Component><AddOn.Component><Category>Scripts</Category><Path>Scripts</Path></AddOn.Component><AddOn.Component><Category>SimObjects</Category><Path>SimObjects\Airplanes</Path></AddOn.Component></SimBase.Document>


<?xml version="1.0" encoding="UTF-8"?>
<SimBase.Document id="add-on" version="4,0" Type="AddOnXml"><AddOn.Name>RealAir Turbine Duke V2</AddOn.Name><AddOn.Description>RealAir Turbine Duke V2</AddOn.Description><AddOn.Component><Category>SimObjects</Category><Path>SimObjects\Airplanes</Path></AddOn.Component><AddOn.Component><Category>Effects</Category><Path>Effects</Path></AddOn.Component></SimBase.Document>


All planes appear in the AI selection.

[Ener]

I did not find a xml for Milviz KA350i in the SimObjects/Airplanes

[Steve Waite]

The xml file is in the add-ons folder. That file contains the script for the location of the plane and if it's not strictly correct IF will ignore it.

A plane installed into simobjects doesn't have to have an xml so I can look at the aircraft.cfg.

[Steve Waite]

The A2A has a path statement for effects so I assume the a2a is installed to simobjects\airplanes. If so I can look at the cfg.

The duke states the simobjects folder so I should look at that cfg as well.

Have these two planes been adjusted by software of some kind?

Maybe send me the cfg's so I can check those. Never had issues with those before.

[Ener]

Where do I find the add-ons folder with this xml ?



Aircraft cfg for KA350i.

[fltsim.0]
title=Milviz KA350i N70EU
sim=MVKA350i
model=
panel=
sound=
texture=N70EU
kb_checklists=King_Air_350_check
kb_reference=King_Air_350_ref
atc_id_color=0xffffffffff
atc_id=N350KA
ui_manufacturer="Milviz"
ui_type="KA-350i"
ui_variation="N70EU"
ui_typerole="Twin Engine TurboProp"
ui_createdby="Milviz"
description="The King Air in all its variants is a beautiful airplane with classic styling and graceful lines. Many of the improvements over the years have provided better aerodynamic efficiency, increased muscle under the cowlings, greater speed, upgraded avionics and electrical systems, and increased cabin luxury. In addition to duties as a corporate shuttle, the plane is also available in cargo configurations."


[fltsim.1]
title=Milviz KA350i G-POWB
sim=MVKA350i
model=
panel=
sound=
texture=G-POWB
kb_checklists=King_Air_350_check
kb_reference=King_Air_350_ref
atc_id_color=0xffffffffff
atc_id=N350KA
ui_manufacturer="Milviz"
ui_type="KA-350i"
ui_variation="G-POWB"
ui_typerole="Twin Engine TurboProp"
ui_createdby="Milviz"
description="The King Air in all its variants is a beautiful airplane with classic styling and graceful lines. Many of the improvements over the years have provided better aerodynamic efficiency, increased muscle under the cowlings, greater speed, upgraded avionics and electrical systems, and increased cabin luxury. In addition to duties as a corporate shuttle, the plane is also available in cargo configurations."



[CameraDefinition.0]
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, 3.5, -22.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
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 = 15, 1.0, 3.0
InitialPbh = 6, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[CameraDefinition.2]
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 = 0, 3.5, -22.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum

[CameraDefinition.3]
Title = "Left Wing View"
Guid = {3A2025AA-80F4-43A3-AFA8-37694BAA1F96}
Description = View from a left side seat on the aircract
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -0.4, 0.8, -1.5
InitialPbh = 9, 0, -80
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum

[CameraDefinition.4]
Title = "Right Wing View"
Guid = {D4E3827B-37E4-46BE-AEC0-3B1B0667E419}
Description = View from a right side seat on the aircract
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 0.4, 0.8, -1.5
InitialPbh = 9, 0, 80
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 = 0.5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=60
HeadingPanRate=70
InitialXyz=0.94, 0.0, 0.0
InitialPbh=2, 0, 0


[CameraDefinition.002]
Title = "Engine Controls"
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 = 1.2
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.003]
Title = "Overhead"
Guid = {2CEF9A21-A15F-4AC2-B36D-CFD1FD35966B}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.405,-0.364,-0.08
InitialPbh=-76,0,0

[CameraDefinition.004]
Title = "Center Console"
Guid = {170F26BF-15AF-4BFB-8118-1F6D0CCDDD55}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.373,-0.032,-0.204
InitialPbh=82,0,0

[CameraDefinition.005]
Title = "Left Switch Panel"
Guid = {3195EE82-3691-4751-9335-F92EB4BE63CD}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.028,-0.419,0.117
InitialPbh=17,0,0

[CameraDefinition.006]
Title = "Right Switch Panel"
Guid = {352D812B-ABFD-4490-B4D8-1378132BEFF6}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.812,-0.419,0.117
InitialPbh=17,0,0

[CameraDefinition.007]
Title = "Fuel Panel"
Guid = {1BB8AA17-29D0-42B4-B1F6-B61D1ADC16F9}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=-0.027,0,0.316
InitialPbh=50,0,-85

[General]
atc_type=BEECH
atc_model=B350
editable=0
performance="Cruise Speed\t\n315 kts 363 mph 583 km\/h\n\nEngines\t\nPratt & Whitney PT6A-60A 1,050 shp\n\nMaximum Range\t\n1,765 nm 2,031 m\t 3,269 km\n\nService Ceiling\t\n35,000 ft 10,668 m\n\nFuel Capacity\t\n539 U.S. gal 2,040 L\n\nMaximum Takeoff Weight \n15,000 lb\t 6,818 kg\n\nLength\t\n46.7 ft\t 14.23 m\n\nWingspan\t\n57.9 ft\t 17.65 m\n\nHeight\t\n14.3 ft\t 4.36 m\n\nSeating\t\nUp to 11\n\nUseful Load\t\n5,910 lb\t 2,681 kg"
Category = airplane

[WEIGHT_AND_BALANCE]
max_gross_weight = 15100
empty_weight = 9800 ;//empty_weight = 9970 <-- includes single pilot?

reference_datum_position = 0, 0, 0 ;//(feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline), corresponds to F.S. 203.37" ( MAC = 69.43", LE at 186.01" )
empty_weight_CG_position = 0.78, 0, 1 ;//1(feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 14

station_load.0 = 170, 6.2, -0.5, 1, pilot ;// FS 129
station_load.1 = 170, 6.2, 0.5, 1, co pilot ;// FS 129
station_load.2 = 150, 2.36, -0.5, 1, pax 1st row ;// FS 175
station_load.3 = 150, 3.03, 0.5, 1, pax 1st row ;// FS 167
station_load.4 = 150, -1.05, -0.5, 1, pax 2nd row ;// FS 216
station_load.5 = 150, -1.05, 0.5, 1, pax 2nd row ;// FS 216
station_load.6 = 150, -3.64, -0.5, 1, pax 3rd row ;// FS 247
station_load.7 = 150, -3.64, 0.5, 1, pax 3rd row ;// FS 247
station_load.8 = 170, -7.55, -0.5, 1, pax 4th row ;// FS 294
station_load.9 = 170, -7.55, 0.5, 1, pax 4th row ;// FS 294
station_load.10 = 0, -10.3, 0.5, 1, lav seat ;// FS 327
station_load.11 = 0, -12.97, 0.0, 0, bag 550 lbs ;// FS 359
station_load.12 = 0, -2.59, -8.5, 0, LW bags 300 lbs ;// FS 234.4
station_load.13 = 0, -2.59, 8.5, 0, RW bags 300 lbs ;// FS 234.4

;Moments of Inertia
empty_weight_pitch_MOI = 26348
empty_weight_roll_MOI = 27569
empty_weight_yaw_MOI = 34790
empty_weight_coupled_MOI= 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
hi_alpha_on_yaw = 1.0
p_factor_on_yaw = 0.5
torque_on_roll = 1
gyro_precession_on_yaw = 1
gyro_precession_on_pitch = 1
gyro_precession_on_roll = 1

[GeneralEngineData]
engine_type = 5 ;//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 9, -8.6, 1.0 ;//(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 9, 8.6, 1.0 ;//(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 0.85 ;//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 = 8.75 ;// 105 inches
propeller_blades = 4 ;//Number of propeller blades
propeller_moi = 4 ;//Propeller moment of inertia 20 actual 15
beta_max = 60 ;//Maximum blade pitch angle for constant speed prop, (degrees) 50
beta_min = 12 ;//Minimum blade pitch angle for constant speed prop, 12
min_gov_rpm = 1250 ;//Miminum governed RPM (52%) 19500
prop_tc = 0.001 ;//Prop time-constant 0.001 actual 0.004 0.0005 0.005 opt for prop moi 20
gear_reduction_ratio = 22.06 ;//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 = 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 = 400 ;//Minimum RPM for prop feathering
beta_feather = 86 ;//Feathering pitch angle (degrees) 86
power_absorbed_cf = 1 ;//Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 1 ;//Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available = 2 ;//Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta = 9 ;//Miminum pitch angle on ground, (degrees) 10
minimum_reverse_beta = -14 ;//Minimum pitch angle in reverse, (degrees) -14 -10 C90

[TurbineEngineData]
fuel_flow_gain = 0.0150 ;//Gain on fuel flow 0.015 opt for start 0.03 else
inlet_area = 0.5 ;//Square Feet, engine nacelle inlet area 1.0
rated_N2_rpm = 37500 ;//RPM, second stage compressor rated value (37500)
static_thrust = 210 ;//Lbs, max rated static thrust at Sea Level

[turboprop_engine]
power_scalar = 0.9 ;//Scalar on Turboprop power
maximum_torque = 3300 ;//Maximum torque available (ft-lbs) cfg 3300 faa 3224

[electrical]
max_battery_voltage = 25.20 ;// Battery Voltage valid values 0 to 30 otherwise voltage defaults to 24.00
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 300.0

;//BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
;// ALL systems conected by default to Battery, as each one is tied by code to corresponding real BUS
flap_motor = 2, 10 , 12.0
gear_motor = 2, 10 , 15.0
autopilot = 2, 5 , 12.0
avionics_bus = 2, 15 , 10.0
avionics = 1, 15 , 10.0
pitot_heat = 2, 5 , 15.0
additional_system = 2, 5 , 10.0
marker_beacon = 2, 5 , 15.0
gear_warning = 2, 2 , 12.0
fuel_pump = 2, 8 , 10.0
starter1 = 2, 20 , 20.0
light_nav = 2, 5 , 10.0
light_beacon = 2, 5 , 10.0
light_landing = 2, 15 , 10.0
light_taxi = 2, 15 , 10.0
light_strobe = 2, 5 , 10.0
light_panel = 2, 5 , 10.0



;//// Contact Points
;//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, 14.4, 0.0, -4.7, 1600, 0, 0.6, 96, 0.50, 2.20, 0.7, 3.0, 6.0, 0, 195, 195 ;// FS 30
point.1 = 1, -1.8, -8.9, -4.7, 1600, 1, 0.8, 0, 0.50, 1.90, 0.9, 6.2, 6.2, 2, 205, 205 ;// FS 225
point.2 = 1, -1.8, 8.9, -4.7, 1600, 2, 0.8, 0, 0.50, 1.90, 0.9, 5.9, 5.9, 3, 215, 215 ;// FS 225
point.3 = 2, 0.1, -6.7, -2.7, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 ;//ret
point.4 = 2, 0.1, 6.7, -2.7, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 ;//ret
point.5 = 2, 5.0, -6.7, -2.5, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 ;//cowl
point.6 = 2, 5.0, 6.7, -2.5, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 ;//cowl
point.7 = 2, -21.9, 0.0, 0.7, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 ;//vfin
point.9 = 2, -9.0, 0.0, -1.7, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 ;//belly
point.11 = 2, -2.0,-24.5, 1.0, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 ;//wtp
point.12 = 2, -2.0, 24.5, 1.0, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 ;//wtp
point.13 = 2, -24.0, 0.0, 10.0, 1500, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 ;//vtail

static_pitch = 0.2
static_cg_height = 4.5
gear_system_type= 0 ;//Electric

[brakes]
parking_brake = 1 ;//Parking brake available
toe_brakes_scale = 0.6 ;//Brake scalar 0.6 previous
differential_braking_scale =0.6 ;// 0.6 previous
auto_brakes = 0

[hydraulic_system]
normal_pressure = 3000.0 ;//PSI
electric_pumps = 0 ;//no electric pumps
engine_map = 1,1,0,0 ;//pumps on Eng1,2

[Views] ;// completed
eyepoint = 4.7, -1.35, 3.7

[flaps.0]
type = 1 ;// 1 - tail, 2 - lead
span-outboard = 0.5 ;// 0.0 .. 1.0
extending-time = 5.2 ;// seconds was 10 before
flaps-position.0 = 0 ;// degrees
flaps-position.1 = 14 ;// degrees
flaps-position.2 = 35 ;// degrees
damaging-speed = 210 ;// KIAS
blowout-speed = 220 ;// KIAS

[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, 1
Adf.1 = 1,
Adf.2 = 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=2,0

[attitude_indicators]
;//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2

[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, 5=landing
;// 6=taxi, 7=recognition, 8=wing, 9=logo 10=cabin
light.0 = 10, 4.91, 0.00, 1.64, fx_vclight,
light.1 = 9, -25.5, -4.00, 5.00, KA350i_TailFlood,
light.2 = 9, -25.5, 4.00, 5.00, KA350i_TailFlood,
light.3 = 8, 4.5, -15.00, 4.00, KA350i_TailFlood,
light.4 = 8, 4.5, 15.00, 4.00, KA350i_TailFlood,

[exits]
number_of_exits = 4
exit.0 = 0.4, 0, 0, 0, 0
exit.1 = 0.4, 0, 0, 0, 1
exit.2 = 0.4, 0, 0, 0, 2
exit.3 = 0.4, 0, 0, 0, 2

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
startup = fx_engstrt_MV_KA350

[fuel]
LeftMain = 0.8, -17.25, 0, 193, 3 ;//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux = 0.8, -4, 0, 80, 0.3
RightMain = 0.8, 17.25, 0, 193, 3 ;//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = 0.8, 4, 0, 80, 0.3

fuel_type = 2 ;//Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2
electric_pump=2

[airplane_geometry]
wing_area = 310 ;//Square feet
wing_span = 57.9 ;//Feet, aspect ratio 10.8
wing_root_chord = 7.82 ;//This number differs from the actual aircraft in order to produce the correct MAC length ( 69.43" ), due to the double taper wing on the actual aircraft.

wing_dihedral = 6 ;//Degrees
wing_incidence = 3.8 ;//Degrees, root incidence = 3°48'
wing_twist = -4.9 ;//Degrees, tip incidence = -1°7'
oswald_efficiency_factor= 0.65
wing_winglets_flag = 1 ;//Are winglets available?
wing_sweep = 2 ;//Degrees, wing leading edge
wing_pos_apex_lon = 1.872 ;//Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = -0.5 ;//Feet, vertical distance from reference point, positive going up
htail_area = 48.7 ;//Square feet, includes elevator
htail_span = 18.4 ;//Feet
htail_pos_lon = -29 ;//Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 10 ;//Feet, vertical distance from reference point, positive going up
htail_incidence = 0 ;//Degrees
htail_sweep = 10 ;//Degrees, horizontal tail leading edge
vtail_area = 52.3 ;//Square feet, includes rudder
vtail_span = 7.5 ;//Feet, tip to body
vtail_sweep = 40 ;//Degrees, vertical tail leading edge
vtail_pos_lon = -26 ;//Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 6 ;//Feet, vertical distance from reference point, positive going up
elevator_area = 19.3 ;//Square feet
aileron_area = 18 ;//Square feet
rudder_area = 15.1 ;//Square feet
elevator_up_limit = 20 ;//Degrees
elevator_down_limit = 14 ;//Degrees
aileron_up_limit = 24 ;//Degrees
aileron_down_limit = 16 ;//Degrees
rudder_limit = 25 ;//Degrees
elevator_trim_limit = 18 ;//Degrees
;//;//;//;//;// MILVIZ CUSTOM DATA ;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;///
spoiler_limit = 90 ;//Degrees = 0
spoiler_extension_time = 1 ;//Seconds
;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;///
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 = 3.0 ;//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 = -2.0 ;//Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down= 0 ;//Design G load tolerance (negative, flaps down)
load_safety_factor = 1.5 ;//Design G load safety factor

[Reference Speeds]
flaps_up_stall_speed = 96 ;//Knots True (KTAS), Clmax = 1.5
full_flaps_stall_speed = 81 ;//Knots True (KTAS), Clmax = 2.15 ( flap lift = 0.65 in air file )
cruise_speed = 200 ;//Knots True (KTAS)
max_mach = 0.60 ;// 0.58 Mmo
max_indicated_speed = 270 ;//Red line (KIAS) 263Vno

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
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=30.0,25.0,15.0
max_bank_acceleration=3.8 ;// 1.8
max_bank_velocity=6 ;//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 = 1.0
;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//
;// These ones for testing only
;//;//;//;//;//;//;//;//;//;//;//;//;//;//;///
default_pitch_mode=2
default_bank_mode=1
yaw_slip_control_gain=0.000000
yaw_control_uses_trim=0.000000


[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


;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//
;//;//;//;// MILVIZ CUSTOM DATA ;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//
;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//;//

[KA350i_TurbineEngine]
Startup_Accel_Rate = 0.300 ;// 0.400 = default (0.500 = fast)
Idle_Accel_Rate = 0.080 ;// 0.015 = ~FS default - (0.500 = very fast)
Engine_Power.0 = 1.000 ;// Engine power scalar min=0.985 max=1.015 default=1.000
Engine_Power.1 = 0.995 ;// Engine power scalar min=0.985 max=1.015 default=1.000
Axis_Power_Min_Pos = 0.00 ;// Throttle minimum position 0.00 = idle (default) or -25.00 = full reverse
Power_Beta_Flt_Enabled = 1 ;// Throttle beta (and reverse) enabled in flight 0 = no (default) 1 = yes

[KA350i_Propeller]
Axis_Prop_Min_Pos = 0.00 ;//Propeller minimum position 0.00 = high pitch (default) or -25.00 = feathered

[KA350i_Electrics]
Battery_Voltage = 25.00 ;//Battery Voltage at SIM load
Battery_Amperage = 42.00 ;//Battery Amperage at SIM load