[fltsim.0]
title=Argo02
sim=Argo02
model=
panel=
sound=RMZ
texture=
kb_checklists=Argo_Check
kb_reference=Argo_Ref
atc_id=RA-00000
atc_id_color=
ui_manufacturer="Argo"
ui_type="02"
ui_variation="Beta 23.09"
ui_typerole="Single Engine Prop"
ui_createdby=
description=

[fltsim.1]
title=Argo02mag
sim=Argo02
model=
panel=
sound=
texture=Magazine
kb_checklists=Argo_Check
kb_reference=Argo_Ref
atc_id=RA-00000
atc_id_color=
ui_manufacturer="Argo"
ui_type="02"
ui_variation="Magazine Cover"
ui_typerole="Single Engine Prop"
ui_createdby=
description=

[fltsim.2]
title=Argo02edel
sim=Argo02
model=
panel=
sound=
texture=Edelweiss
kb_checklists=Argo_Check
kb_reference=Argo_Ref
atc_id=RA-00000
atc_id_color=
ui_manufacturer="Argo"
ui_type="02"
ui_variation="Edelweiss"
ui_typerole="Single Engine Prop"
ui_createdby=
description=

[General]
atc_type=Experimental
atc_model=
editable=0
performance=" "
Category = airplane

[CameraDefinition.1]
Title = "Left Wing"
Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED}
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 = 1.0
ShowWeather = Yes
InitialXyz = -9.0, 0.38, -1.5
InitialPbh = 5, 0, 80
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.2]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description = Looking forward from the tip of the vertical stabilizer
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
ShowWeather = Yes
InitialXyz = 0, 1.9, -10.75
InitialPbh = 11, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.001]
Title = "Left Side View"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.7
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=30
HeadingPanRate=75
PanAcceleratorTime=0
InitialXyz=-0.3, -0.0, 0.0
InitialPbh=30, 5, -10

[CameraDefinition.002]
Title = "Right Side View"
Guid = {195EAB58-9E4A-4E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.7
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=30
HeadingPanRate=75
PanAcceleratorTime=0
InitialXyz=0.3, -0.0, 0.0
InitialPbh=30, -5, 10

[WEIGHT_AND_BALANCE]
max_gross_weight = 562                         // (pounds)
empty_weight =  364                             // (pounds)

reference_datum_position     =  0.0, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  0.55, 0.040, -0.3         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations =1

station_load.0 = 175.0, -1.2, 0.00, 0.0   //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 

station_name.0 = "Pilot"     


;Moments of Inertia
empty_weight_pitch_MOI   = 87.7
empty_weight_roll_MOI    = 68.4
empty_weight_yaw_MOI     = 127.3
empty_weight_coupled_MOI = 0.0


[flight_tuning]
cruise_lift_scalar     = 0.8
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 = 0.0
aileron_trim_effectiveness  = 0.0
rudder_trim_effectiveness   = 0.0
p_factor_on_yaw          = 1.0
torque_on_roll           = 1.0
gyro_precession_on_yaw   = 0.3
gyro_precession_on_pitch = 0.3


[flaps.0]
type=0                                    // 1 - tail, 2 - lead
span-outboard=0.0                         // 0.0 .. 1.0
extending-time=0.0                        // seconds
flaps-position.0=0                        // degrees
damaging-speed=102                         // KIAS
blowout-speed=102                          // KIAS
lift_scalar=0.0
drag_scalar=0.0
pitch_scalar=0.0
system_type=4                             //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None


[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 3.2, 0.0, 0.0                        //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0                           //Fuel flow scalar
min_throttle_limit = 0.0                        //Minimum percent throttle.  Generally negative for turbine reverser

[piston_engine]
max_rpm_mechanical_efficiency_scalar=1.0
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000
cylinder_displacement= 19.5
two_stroke_cycle = 1
compression_ratio= 8.2
number_of_cylinders= 2
max_rated_rpm= 5500.000
max_rated_hp= 28
fuel_metering_type= 1
cooling_type= 1
normalized_starter_torque= 0.1
turbocharged= 0
max_design_mp= 0.000
min_design_mp= 0.000
critical_altitude= 0.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
power_scalar=1
number_of_magnetos = 1

[propeller]
propeller_type= 1
propeller_diameter= 4.9
propeller_blades= 2
propeller_moi= 0.4
beta_max= 0
beta_min= 0
min_gov_rpm= 0
prop_tc= 0.1
gear_reduction_ratio= 2.0
fixed_pitch_beta= 13     // 11.4
low_speed_theory_limit= 80.0
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.0
beta_feather= 0.000
power_absorbed_cf= 0.0
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0.0
minimum_reverse_beta= 0.0
thrust_scalar=0.85


        //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]
//      0      1      2      3      4    5   6        7      8     9    10    11    12   13   14   15
point.0=3,   -8.9,   0.0,  -0.99,  1800, 0, 0.1,     180,  0.015, 2.5,  0.3,   0,   0.0, 9.0, 0.0, 0.0
point.1=1,    0.4,  -2.2,  -3.12,  3300, 1, 0.6,     0.0,  0.083, 4.3,  0.2,   0,   0.0, 2.0, 0.0, 0.0
point.2=1,    0.4,   2.2,  -3.12,  3300, 2, 0.6,     0.0,  0.083, 4.3,  0.2,   0,   0.0, 3.0, 0.0, 0.0
point.3=2,   -0.6,  -10.5,  -0.8,  2000, 0, 0.000,   0.0,  0.000, 0.0,  0.000, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2,   -0.6,   10.5,  -0.8,  2000, 0, 0.000,   0.0,  0.000, 0.0,  0.000, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2,  -10.40,  0.0,    3,    800,  0, 0.000,   0.0,  0.000, 0.0,  0.000, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2,    5.20,  0.0,    0,    800,  0, 0.000,   0.0,  0.000, 0.0,  0.000, 0.0, 0.0, 4.0, 0.0, 0.0
point.6=2,    -9.8,  0.0,   -1,    1800, 0, 0.000,   0.0,  0.000, 0.0,  0.000, 0.0, 0.0, 4.0, 0.0, 0.0
point.6=2,    -11,   0.0,    0,    800,  0, 0.000,   0.0,  0.000, 0.0,  0.000, 0.0, 0.0, 4.0, 0.0, 0.0

static_pitch = 13.3
static_cg_height = 3.2  //3.2
gear_system_type=0

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 0.0  //Brake scalar
differential_braking_scale = 0        //Delta on the amount of brake when the rudder pedals deflected
auto_brakes = 0

[hydraulic_system]
normal_pressure = 0.0    //PSI

[Views]
eyepoint = -1.8, 0.000, 1.57

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4,  -1.1,   0.00,  1.50, fx_vclight,

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

[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 =200, 1000
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=0,0

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

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0

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

[pneumatic_system]
max_pressure=0

[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 0.0    //Scalar on heat effectiveness, 0 = not available

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

[SMOKESYSTEM]
smoke.0=-10.00, -0.70, 0.0, fx_smoke_w

[electrical]
max_battery_voltage = 0
generator_alternator_voltage = 14
avionics_bus=0, 0 , 0.0
avionics=1, 5 , 0.0
starter1=3, 0, 0.0

[LIGHTS]
;/Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit

[fuel]
Center1 = 1.4, 0.0, 0.25, 4.0, 0.0       //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1                            //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=0
engine_driven_pump=0

[airplane_geometry]
wing_area               = 67.8                 //Square feet
wing_span               = 20.7                  //Feet
wing_root_chord         = 3.28                  //Feet
wing_dihedral           = 4                   //Degrees
wing_incidence          = 4                  //Degrees
wing_twist              = 0                  //Degrees
oswald_efficiency_factor= 0.6                   //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       = 0.82                  //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = -0.7                   //Feet, vertical distance from reference point, positive going up

htail_area              = 12.9                  //Square feet
htail_span              = 6.7                   //Feet
htail_pos_lon           = -8.45                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 0                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 0                  //Degrees
htail_sweep             = 0                  //Degrees, horizontal tail leading edge

vtail_area              = 7.1                  //Square feet
vtail_span              = 3.2                  //Feet, tip to body
vtail_sweep             = 37                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -8.8                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 1.2                   //Feet, vertical distance from reference point, positive going up

elevator_area           = 6.7                 //Square feet
aileron_area            = 16.0                   //Square feet
rudder_area             = 4.8                  //Square feet
elevator_up_limit       = 25.0                  //Degrees
elevator_down_limit     = 25.0                  //Degrees
aileron_up_limit        = 25                  //Degrees
aileron_down_limit      = 16                  //Degrees
rudder_limit            = 25.0                  //Degrees
elevator_trim_limit     = 20.0                   //Degrees
spoiler_limit           = 10.0                   //Degrees
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  =  5.0               //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down=  5.0               //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= -3.0               //Design G load tolerance (negative, flaps down) 
load_safety_factor         =  1.0               //Design G load safety factor 
flap_to_aileron_scale = 1.0
spoiler_extension_time=0.000000


[Reference Speeds]
flaps_up_stall_speed    = 38.9                  //Knots True (KTAS)
full_flaps_stall_speed  = 38.9                  //Knots True (KTAS)
cruise_speed            = 64.8                  //Knots True (KTAS)
max_indicated_speed     = 126.9                   //Red line (KIAS)

[autopilot]
autopilot_available= 0
flight_director_available= 0

[forcefeedback]
ground_bumps_magnitude1=2600            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200            ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000                 ; in microseconds

[stall_warning]
type=0
stick_shaker=0

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