[accusim]
//The version below only indicates when this file was last edited and is rarely the same as the core update version
version = 2.1

[fltsim.0]
title=C182_VH-DLL
sim=C182
model=
panel=
sound=
texture=1
kb_checklists=C182_check
kb_reference=C182_ref
atc_id=VH-DLL
ui_manufacturer=A2A Cessna
ui_type="C182T Skylane"
ui_variation="VH-DLL"
ui_typerole="Single Engine Prop"
ui_createdby="A2A Simulations Inc."
description=""

[fltsim.1]
title=C182_N6182G
sim=C182
model=
panel=
sound=
texture=2
kb_checklists=C182_check
kb_reference=C182_ref
atc_id=N6182G
ui_manufacturer=A2A Cessna
ui_type="C182T Skylane"
ui_variation="N6182G"
ui_typerole="Single Engine Prop"
ui_createdby="A2A Simulations Inc."
description=""

[fltsim.2]
title=C182_D-EXSW
sim=C182
model=
panel=
sound=
texture=3
kb_checklists=C182_check
kb_reference=C182_ref
atc_id=D-EXSW
ui_manufacturer=A2A Cessna
ui_type="C182T Skylane"
ui_variation="D-EXSW"
ui_typerole="Single Engine Prop"
ui_createdby="A2A Simulations Inc."
description=""

[fltsim.3]
title=C182_N516DM
sim=C182
model=
panel=
sound=
texture=4
kb_checklists=C182_check
kb_reference=C182_ref
atc_id=N516DM
ui_manufacturer=A2A Cessna
ui_type="C182T Skylane"
ui_variation="N516DM"
ui_typerole="Single Engine Prop"
ui_createdby="A2A Simulations Inc."
description=""

[fltsim.4]
title=C182 THW Aviation Academy
sim=C182
model=
panel=
sound=
texture=thw academy
kb_checklists=C182_check
kb_reference=C182_ref
atc_id=N516DM
ui_manufacturer=A2A Cessna
ui_type="C182T Skylane"
ui_variation="N516DM"
ui_typerole="Single Engine Prop"
ui_createdby="A2A Simulations Inc."
description=""

[fltsim.5]
title=C182 THW VFR club
sim=C182
model=
panel=
sound=
texture=thw vfr club
kb_checklists=C182_check
kb_reference=C182_ref
atc_id=N516DM
ui_manufacturer=A2A Cessna
ui_type="C182T Skylane"
ui_variation="N516DM"
ui_typerole="Single Engine Prop"
ui_createdby="A2A Simulations Inc."
description=""

[General]
atc_type=Cessna
atc_model=C182
editable=1
performance=""
Category=airplane

[CameraDefinition.0]
Title = "Pitot Tube Heat Test"
Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0A88ED}
Description = Preflilght inspection
Origin = Virtual Cockpit
SnapPbhAdjust = FALSE
SnapPbhReturn = FALSE
PanPbhAdjust = FALSE
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -0.5, -0.05, 0.15
InitialPbh = -7, 0, 283
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum
HotKeySelect = 4

[CameraDefinition.1]
Title = "Verify Baggage Door is Locked"
Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0B88ED}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -1.98, 0.5, -2.05
InitialPbh = 18, 0, 62
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.2]
Title = "Tail"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -1.5, 1.5, -9
InitialPbh = 8, 0, 20
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum


[CameraDefinition.3]
Title = "Right Flap"
Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 3, 1, -2.6
InitialPbh = 6, 0, 325
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.4]
Title = "Right Aileron"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 7, 0, 0.2
InitialPbh = -18, 0, 246
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.5]
Title = "Right Wing Tie Down"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64B}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 3.3, 0.3, 2
InitialPbh = -11, 0, 205
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.6]
Title = "Right Main Tire"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64C}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 3.5, -0.6, -0.4
InitialPbh = 8, 0, 265
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum


[CameraDefinition.7]
Title = "Right Fuel Tank Sump Quick Drain Valves"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC11B}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 2.0, 0.3, 1.5
InitialPbh = -14, 0, 205
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum


[CameraDefinition.8]
Title = "Right Fuel Tank Level
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC12B}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 0.9, 1.8, 1.3
InitialPbh = 35, 0, 184
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.9]
Title = "Right nose static air source opening"
Guid = {D8D67915-2E9B-4e75-9D8B-8EFFBBFAC64D}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 2, 0.2, 1.8
InitialPbh = 11, 0, 235
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.10]
Title = "Nose Fuel Strainer and tire"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64D}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 2.2, -0.75, 1.4
InitialPbh = 3, 0, 260
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum


[CameraDefinition.11]
Title = "Propeller Check"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64E}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 0, 0.2, 5.6
InitialPbh = 3, 0, 180
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum


[CameraDefinition.12]
Title = "Engine inlets and air filter"
Guid = {D8D67755-2E9B-4e75-9D8B-8EFFBBFAC64E}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = 0, 0.2, 4
InitialPbh = 8, 0, 180
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.13]
Title = "Engine Oil Check"
Guid = {D8D67956-2E9B-4e75-9D8B-8EFFBBFAC64F}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -2.6, 0.6, 1.4
InitialPbh = 11, 0, 90
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.14]
Title = "Left Fuel Tank Level
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC13B}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -0.9, 1.8, 1.3
InitialPbh = 35, 0, 176
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum



[CameraDefinition.15]
Title = "Left Fuel Tank Sump Quick Drain Valves"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC18B}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -2.0, 0.3, 1.5
InitialPbh = -14, 0, 155
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum


[CameraDefinition.16]
Title = "Left Main Tire"
Guid = {D8D67959-2E9B-4e75-9D8B-8EFFBBFAC64C}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -3.5, -0.6, -0.4
InitialPbh = 8, 0, 95
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum


[CameraDefinition.17]
Title = "Left Wing Leading Edge"
Guid = {D8D67858-2E9B-4e75-9D8B-8EFFBBFAC64F}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -1.5, 0.5, 1.7
InitialPbh = -3, 0, 217
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum



[CameraDefinition.18]
Title = "Left Aileron"
Guid = {D8D67961-2E9B-4e75-9D8B-8EFFBBFAC64C}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -7, 0, 0.18
InitialPbh = -18, 0, 100
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.19]
Title = "Left Flap"
Guid = {D8D67960-2E9B-4e75-9D8B-8EFFBBFAC64C}
Description = Preflilght inspection
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -3, 1, -2.6
InitialPbh = 6, 0, 35
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum


[CameraDefinition.001]
Title = "Instruments close / IFR"
Guid = {195EAB58-9E4A-3E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.3
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0, 0, 0
InitialPbh=26, 0, 0


[CameraDefinition.002]
Title = "Radio Stack"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.4
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0, 0, 0
InitialPbh=24, 0, 13


[CameraDefinition.003]
Title = "Right Seat"
Guid = {195EAB58-9E4A-1E2A-A34C-A8D9D948F078}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.75
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.5, 0.04, -0.1
InitialPbh=0, 0, 0



[WEIGHT_AND_BALANCE]
max_gross_weight =3110.0
empty_weight =1901.00000       // (feet) longitudinal, lateral, vertical distance from specified datum

reference_datum_position = 0, 0, 0
//empty_weight_CG_position = 0, 0, 0
empty_weight_CG_position = -0.09, 0, -0.6 //Backward set further back
empty_weight_pitch_MOI = 2550
empty_weight_roll_MOI = 1650
empty_weight_yaw_MOI = 3675
empty_weight_coupled_MOI = 0
CG_forward_limit = 0.000
CG_aft_limit = 1.000


max_number_of_stations =30
//st.number +1     lbs,  long,   lat,   vert
station_load.0 =  0.00,  0.40,   -0.05,  0.00, Pilot
station_load.1 =  0.00,  0.40,   0.05,  0.00, Pass. front R
station_load.2 =  0.00, -2.67,   -0.05,  0.00, Pass. rear L
station_load.3 =  0.00, -2.67,   0.05,  0.00, Pass. rear R
station_load.4 =  0.00, -4.50,   0.00,  0.00, Baggage front
station_load.5 =  0.00, -6.8,   0.00,  0.00, Baggage rear
station_load.6 =  0.00,  4.9,   0.00,  0.00, Lubr. Oil
station_load.7 =  0.00,  0.00,   0.00,  0.00, x8
station_load.8 =  0.00,  0.00,   0.00,  0.00, x9
station_load.9 =  0.00,  0.00,   0.00,  0.00, x10
station_load.10 = 0.00,  0.00,   0.00,  0.00, x11
station_load.11 = 0.00,  0.00,   0.00,  0.00, x12
station_load.12 = 0.00,  0.00,   0.00,  0.00, x13
station_load.13 = 0.00,  0.00,   0.00,  0.00, x14
station_load.14 = 0.00,  0.00,   0.00,  0.00, x15
station_load.15 = 0.00,-18.00,   0.00,  0.00, mechanics
station_load.16 = 0.00, 50.00,   0.00,  0.00, used
station_load.17 = 0.00,-50.00,   0.00,  0.00, used
station_load.18 = 0.00,  20.00,   0.00,  0.00, x19
station_load.19 = 0.00,  20.00,   0.00,  0.00, x20

[flight_tuning]
cruise_lift_scalar=1.000 
pitch_stability=2.000 
roll_stability=1.000 
yaw_stability=1.000
parasite_drag_scalar=1.000 
induced_drag_scalar=1.0
elevator_effectiveness=2
aileron_effectiveness=1.00
rudder_effectiveness=1.0
elevator_trim_effectiveness=0
aileron_trim_effectiveness=1.000 
rudder_trim_effectiveness=1.00 
p_factor_on_yaw          = 0 //0.5 //1.755
torque_on_roll           = 0 //2.856
gyro_precession_on_yaw   = 0 //1.0
gyro_precession_on_pitch = 0 //1.0



[GeneralEngineData]
engine_type =0
Engine.0 =6.70, 0.000, -0.000
ThrustAnglesPitchHeading.0 = 0,0                //Thrust pitch and heading angles in degrees (+pitch down, +heading right)
fuel_flow_scalar=1.00000
min_throttle_limit =0.00000                        //Minimum percent throttle.  Generally negative for turbine reverser

[piston_engine]
power_scalar = 1.0                              //Piston power scalar
cylinder_displacement= 80.0                     //Cubic inches per cylinder
compression_ratio= 8.5                          //Compression ratio
number_of_cylinders=4                           //Number of cylinders
max_rated_rpm= 2700                             //Max rated RPM
max_rated_hp= 300                               //Max rated HP
fuel_metering_type= 0                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3                  //Starter torque factor
turbocharged= 1                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 55                                //Max design manifold pressure, (inHg)
min_design_mp= 5                                //Min design manifold pressure, (inHg)
critical_altitude= 30000                            //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0                         //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0                  //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 1                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0                                //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0                   //Scalar on idle RPM friction

[propeller]
thrust_scalar=1.000
propeller_type= 1
propeller_diameter= 9
propeller_blades= 3
propeller_moi= 10.000
beta_max= 75.000
beta_min= 15.000
min_gov_rpm= 500.000
prop_tc= 0.010
gear_reduction_ratio= 2
fixed_pitch_beta= 30
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 1
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.000
beta_feather= 0.000
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 0.000
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000


[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
max_battery_voltage = 28
generator_alternator_voltage = 28
max_generator_alternator_amps = 100
engine_generator_map = 1
electric_always_available = 0
flap_motor         = 0, 1 , 0.0
gear_motor         = 0, 1 , 0.0
autopilot          = 0, 1 , 12.0
avionics_bus       = 0, 1 , 12.0
avionics           = 1, 1 , 12.0
pitot_heat         = 0, 1 , 12.0    //Scalar on heat effectiveness, 0 = not available
additional_system  = 0, 1 , 12.0
marker_beacon      = 1, 1 , 12.0
gear_warning       = 0, 1 , 12.0
fuel_pump          = 0, 1 , 0
starter1           = 0, 1 , 0
light_nav          = 0, 1 , 12.0
light_beacon       = 0, 1 , 12.0
light_landing      = 0, 1 , 12.0
light_taxi         = 0, 1 , 12.0
light_strobe       = 0, 1 , 12.0
light_panel        = 0, 1 , 12.0

        //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]
max_number_of_points =9

static_pitch= 4.6                //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height= 3.80            //feet, altitude of CG when at rest on the ground
gear_system_type=0
tailwheel_lock=0
point.0= 1, 4.056, 0.000, -4.210, 1500, 0, 0.500, 25, 0.112, 2.000, 0.700, 0.000, 0.000, 0
point.1= 1, -1.444, -4.100, -3.790, 3500, 1, 0.500, 0.000, 0.109, 2.000, 0.700, 0.000, 0.000, 2
point.2= 1, -1.444, 4.100, -3.790, 3500, 2, 0.500, 0.000, 0.109, 2.000, 0.700, 0.000, 0.000, 3
point.3= 2, -0.300, -18.000, 3.000, 1800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.4= 2, -0.300, 18.000, 3.000, 1800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.5= 2, -16.620, 0.000, 0.300, 1800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.6= 2, 5.080, 0.000, -2.170, 1800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.7= 2, -19.200, 0.000, 5.830, 1800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7
point.8= 2, -1.300, 0.000, -2.000, 1800, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8

[brakes]
parking_brake = 1.0        //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
auto_brakes =0
hydraulic_system_scalar=0.00000
differential_braking_scale=1

[hydraulic_system]
normal_pressure =0.00000    //PSI

[Views]
eyepoint= -0.35, -0.85, 1.98         //(feet) longitudinal, lateral, vertical distance from reference datum

[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, 1
Transponder.1 = 1
Marker.1      = 1

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.1 =9,  1.3,  0.00, 1.40, fx_a2a_c182_vclight
light.2 =10,  1.3,  0.00, 1.40, fx_a2a_c182_vclight_dim

[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                  //Square feet
aileron  = 200, 1000                  //Square feet
rudder   = 200, 1000                   //Square feet

[altimeters]
altimeter.0=1
altimeter.1=1
altimeter.2=1

[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1

[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=1,0

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

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

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

[pneumatic_system]
max_pressure=0   //PSI
bleed_air_scalar=0

[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

[EFFECTS]
wake=fx_wake
water=fx_spray       // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
startup = null

[exits]
number_of_exits = 4
exit.0 = 0.4 // Main
exit.1 = 0.4 // Passenger
exit.2 = 0.4 // Main - Window
exit.3 = 0.4 // Passenger - Window

[fuel]
LeftMain  = -0.4167, -3.500, 3.000, 44.00, 0.000
RightMain = -0.4167, 3.500, 3.000, 44.00, 0.000
fuel_type =1
number_of_tank_selectors =1
electric_pump=1
engine_driven_pump=1
fuel_dump_rate=0.02000
anemometer_pump=0
manual_pump=0

[airplane_geometry]
wing_area               =174.00000                 //Square feet
wing_span               =36.10000                  //Feet
wing_root_chord         =4.9                   //Feet
wing_dihedral           =1.70000                   //Degrees
wing_incidence          =0.00000                   //Degrees
wing_twist              =0.00000                  //Degrees
oswald_efficiency_factor=0.68000                  //Measure of lift effeciency of wing
wing_winglets_flag      =0                     //Are winglets available?
wing_sweep              =0.00000                     //Degrees, wing leading edge
//wing_pos_apex_lon       =1.34                 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_lon       =1.29 /matching model                 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      =2.83                   //Feet, vertical distance from reference point, positive going up
htail_area              =39.00000                  //Square feet
htail_span              =11.33000                  //Feet
htail_pos_lon           =-15.50000                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          =1.20000                   //Feet, vertical distance from reference point, positive going up
htail_incidence         =0.00000                   //Degrees
htail_sweep             =15.00000                  //Degrees, horizontal tail leading edge
vtail_area              =16.00000                  //Square feet
vtail_span              =4.80000                   //Feet, tip to body
vtail_sweep             =40.00000                  //Degrees, vertical tail leading edge
vtail_pos_lon           =-15.20000                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          =3.30000                   //Feet, vertical distance from reference point, positive going up
elevator_area           =16.60000                  //Square feet
aileron_area            =18.30000                  //Square feet
rudder_area             =9.00000                   //Square feet
elevator_up_limit       =28.00000                  //Degrees
elevator_down_limit     =21.00000                  //Degrees
aileron_up_limit        =30.00000                  //Degrees
aileron_down_limit      =20.00000                  //Degrees
rudder_limit            =24.00000                  //Degrees
elevator_trim_limit     =100 //19.50000                 //Degrees
spoiler_limit           =100.00000                   //Degrees
spoilerons_available    =0                     //Spoilerons Available?
aileron_to_spoileron_gain =0.00000                   //Aileron to spoileron gain
min_ailerons_for_spoilerons =0.00000                 //Degrees
min_flaps_for_spoilerons =0.00000                    //Minimum flap handle position when spoilerons activate
auto_spoiler_available   =0
positive_g_limit_flaps_up  =4.00000               //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down=2.80000               //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up  =-3.20000               //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down=-2.40000               //Design G load tolerance (negative, flaps down)
load_safety_factor         =1.50000               //Design G load safety factor
spoiler_extension_time=1
spoiler_handle_available=1


[flaps.0]       //Trailing Edge Flaps
type= 1                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
system_type=0                                         //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
span-outboard= 0.0                                  // 0.0 .. 1.0
extending-time= 999                                    // seconds
damaging-speed=120.0                                  // KIAS
blowout-speed=150.0                                  // KIAS
flaps-position.0=0.00                                    // degrees
flaps-position.1=12.70                                 // degrees
flaps-position.2=25.30                                 // degrees
flaps-position.3=38.00                                   // degrees
lift_scalar=1.15
drag_scalar=0
pitch_scalar=1.00

[Flaps.1]
type= 2
span-outboard= 1
extending-time= 999
system_type= 3
damaging-speed= 999
blowout-speed= 999
lift_scalar= -60
drag_scalar= 200
pitch_scalar= 0
flaps-position.0= 0
flaps-position.1= 0.0001
flaps-position.2= 0.0002
flaps-position.3= 0.0003
flaps-position.4= 0.0004
flaps-position.5= 0.0005
flaps-position.6= 0.0006
flaps-position.7= 0.0007
flaps-position.8= 0.0008
flaps-position.9= 40

[Reference Speeds]
flaps_up_stall_speed    = 53.0                  //Knots True (KTAS)
full_flaps_stall_speed  = 48.0                  //Knots True (KTAS)
cruise_speed            =122.00000                 //Knots True (KTAS)
max_indicated_speed     =162.00000                   //Red line (KIAS)
max_mach=0.5

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=0
autothrottle_available=0
pitch_takeoff_ga=8
max_pitch=10
max_pitch_acceleration=1
max_pitch_velocity_lo_alt=2
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000
max_pitch_velocity_hi_alt_breakpoint=28000
max_bank=20
max_bank_acceleration=1.8
max_bank_velocity=3
max_throttle_rate=0.1
nav_proportional_control=9
nav_integrator_control=0.25
nav_derivative_control=0
nav_integrator_boundary=2.5
nav_derivative_boundary=0
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0
gs_integrator_boundary=0.7
gs_derivative_boundary=0
yaw_damper_gain =0
default_pitch_mode=0
default_bank_mode=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90
yaw_slip_control_gain=0.000000
yaw_control_uses_trim=0.000000


[forcefeedback]
gear_bump_nose_magnitude=6000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=6000           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=6000          ; 0 - 10000
gear_bump_right_direction=500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=3250            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750             ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1
crash_magnitude1=10000                  ; 0 - 10000
crash_direction1=1000                  ; 0 - 35999 degrees
crash_magnitude2=10000                  ; 0 - 10000
crash_direction2=9000                   ; 0 - 35999 degrees
crash_period2=75000                     ; in microseconds
crash_duration2=2500000                 ; in microseconds
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111

[stall_warning]
type=1                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
stick_shaker=0

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

[smokesystem]
//Z(+=forward), X(+=right), Y(+=up)
//Pipe L:  4.0, -1.02, -2.4,
//Pipe R:  4.0, 1.02, -2.4,


smoke.0 = 0.6, 0, 0, fx_a2a_c182_Blacksmoke1_Fast
smoke.1 = 0.6, 0, 0, fx_a2a_c182_Blacksmoke2_Fast
smoke.2 = 0.6, 0, 0, fx_a2a_c182_Blacksmoke3_Fast

smoke.3 = 4.0, 1.02, -2.4, fx_a2a_c182_Bluesmoke
smoke.4 = 4.0, -1.02, -2.4, fx_a2a_c182_Bluesmoke
smoke.5 = 4.0, 1.02, -2.4, fx_a2a_c182_Bluesmoke
smoke.6 = 4.0, -1.02, -2.4, fx_a2a_c182_Bluesmoke

smoke.7 = 4.0, -1.02, -2.4, fx_a2a_c182_Bluesmoke
smoke.8 = 4.0, -1.02, -2.4, fx_a2a_c182_Bluesmoke
smoke.9 = 3.6, 0, 0, fx_a2a_c182_Whitesmoke3_Fast

smoke.10 = 4.0, -1.02, -2.4, fx_a2a_c182_Blacksmoke_Puff_Fast
smoke.11 = 4.0, 1.02, -2.4, fx_a2a_c182_Blacksmoke_Puff_Fast

