[fltsim.0]
title=Airbus A321 Paint2
sim=Airbus_A321
model=
panel=
sound=
texture=2
kb_checklists=AirbusA321_check
kb_reference=AirbusA321_ref
atc_id=F-MSAB
atc_airline=World Travel
atc_flight_number=
ui_manufacturer="Airbus"
ui_type="A321"
ui_variation="World Travel Airlines"
ui_typerole="Commercial Airliner"
ui_createdby="Microsoft Corporation"
description="The Airbus A321 is a stretched version of Airbus’ best-selling short- and medium-range A320. The A321 has a slightly increased wing area, stronger landing gear with larger tires, and engines with increased thrust. When the A321 entered service in 1988, it pioneered the use of “glass cockpit” instrumentation, the first digital fly-by-wire control system used in an airliner, and sidestick controllers."

[fltsim.1]
title=Airbus A321 Paint4
sim=Airbus_A321
model=
panel=
sound=
texture=4
kb_checklists=AirbusA321_check
kb_reference=AirbusA321_ref
atc_id=I-HKSN
atc_airline=Orbit
atc_flight_number=
ui_manufacturer="Airbus"
ui_type="A321"
ui_variation="Orbit Airlines"
ui_typerole="Commercial Airliner"
ui_createdby="Microsoft Corporation"
description="The Airbus A321 is a stretched version of Airbus’ best-selling short- and medium-range A320. The A321 has a slightly increased wing area, stronger landing gear with larger tires, and engines with increased thrust. When the A321 entered service in 1988, it pioneered the use of “glass cockpit” instrumentation, the first digital fly-by-wire control system used in an airliner, and sidestick controllers."

[fltsim.2]
title=Airbus A321 Paint5
sim=Airbus_A321
model=
panel=
sound=
texture=5
kb_checklists=AirbusA321_check
kb_reference=AirbusA321_ref
atc_id=JA-3297
atc_airline=Pacifica
atc_flight_number=
ui_manufacturer="Airbus"
ui_type="A321"
ui_variation="Pacifica Airlines"
ui_typerole="Commercial Airliner"
ui_createdby="Microsoft Corporation"
description="The Airbus A321 is a stretched version of Airbus’ best-selling short- and medium-range A320. The A321 has a slightly increased wing area, stronger landing gear with larger tires, and engines with increased thrust. When the A321 entered service in 1988, it pioneered the use of “glass cockpit” instrumentation, the first digital fly-by-wire control system used in an airliner, and sidestick controllers."

[fltsim.3]
title=Airbus A321
sim=Airbus_A321
model=
panel=
sound=
texture=
kb_checklists=AirbusA321_check
kb_reference=AirbusA321_ref
atc_id=F-X395
atc_airline=
atc_flight_number=
ui_manufacturer="Airbus"
ui_type="A321"
ui_variation="White"
ui_typerole="Commercial Airliner"
ui_createdby="Microsoft Corporation"
description="The Airbus A321 is a stretched version of Airbus’ best-selling short- and medium-range A320. The A321 has a slightly increased wing area, stronger landing gear with larger tires, and engines with increased thrust. When the A321 entered service in 1988, it pioneered the use of “glass cockpit” instrumentation, the first digital fly-by-wire control system used in an airliner, and sidestick controllers."

[General]
atc_type=AIRBUS
atc_model=A321
editable=0
performance="Cruise Speed\n0.80 Mach		530 mph	828 km\/h\n\nEngine options\nGeneral Electric CFM56-5B3 30,000 lb thrust\n\nMaximum Range\n2,454 nm		4,352 km\n\nService Ceiling\n41,000 ft		12,497 m\n\nFuel Capacity\n52,500 lb		198,675 kg\n\nEmpty Weight\n105,906 lb		48,139 kg\n\nMaximum Gross Weight\n205,000 lb		93,181 kg\n\nLength\n146 ft		44.51 m\n\nWingspan\n111 ft, 10 in	34.09 m\n\nHeight\n38 ft, 7 in		11.76 m\n\nSeating (typical configuration)\n186"
Category = airplane

[CameraDefinition.0]
Title = "Right Side Window"
Guid = {54F54B8A-3EC2-2D4E-8D10-B8F9D0F16ACC}
Description = View of the right wing from the passenger cabin
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.9
ShowWeather = Yes
InitialXyz = 3.2, 1.8, -5
InitialPbh = 5, 0, 100
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.1]
Title = "Left Side Window"
Guid = {0ae3f864-da10-4e5a-977c-b9bba47d6f7a}
Description = View of the left wing from the passenger cabin
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 1.0
ShowWeather = Yes
InitialXyz = -3.2, 1.8, -5
InitialPbh = 5, 0, 260
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.2]
Title = "Landing Gear"
Guid = {96873AAD-621B-4C45-8A58-DEF7B7FCB051}
Description = View of the landing gear and left wing inboard flaps
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .52
ShowWeather = Yes
InitialXyz = -3.6, -1.8, -11
InitialPbh = 0, 0, 18
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.3]
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, 5.5, -52.0
InitialPbh = 5, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.4]
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 = 30.8, 1.6, 4.0
InitialPbh = 6, 0, 280
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[CameraDefinition.5]
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 = -30.8, 1.6, 4.0
InitialPbh = 6, 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 = .7
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=1.35, 0.0, 0.0
InitialPbh=2, 0, 0

[CameraDefinition.002]
Title = "Center Console"
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 = 0.9
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.65, 0.50, -0.2
InitialPbh=70, 0, 0

[CameraDefinition.003]
Title = "Overhead Panel"
Guid = {4ca337db-ae88-4c5f-96ea-ddebbd2a86fe}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.8
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.7, -0.58, -0.31
InitialPbh=-58.0, 0, 0

[WEIGHT_AND_BALANCE]
max_gross_weight = 187392                      // (pounds)
empty_weight = 93662                           // (pounds)

reference_datum_position     =  -4.5, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  -4.0, 0, 0         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0 =   170.0,  52.0, -3.0,	2.0    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)        
station_load.1 =   170.0,  52.0,  3.0,	2.0    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.2 =  3500.0,  18.5, -3.0,	2.0    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.3 =  3500.0,  18.5,  3.0,	2.0    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.4 =  3500.0, -26.0, -3.0,	2.0    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.5 =  3500.0, -26.0,  3.0,	2.0    //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 

station_name.0 = "Pilot"            
station_name.1 = "Co-Pilot"         
station_name.2 = "First Class A-C"      
station_name.3 = "First Class D-F"      
station_name.4 = "Coach A-C"       
station_name.5 = "Coach D-F"      

;Moments of Inertia
empty_weight_pitch_MOI   = 835131.26     
empty_weight_roll_MOI    = 198749.02
empty_weight_yaw_MOI     = 806087.52
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

[GeneralEngineData]
engine_type = 1                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 5.2, -18.6, -4.6                    //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 5.2,  18.6, -4.6                    //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1                            //Scalar for fuel flow efficiency
min_throttle_limit = -0.25                      //Minimum percent throttle.  Generally negative for turbine reverser
max_contrail_temperature = -30                  //Temperature (deg C) below which contrails may appear

[TurbineEngineData]
fuel_flow_gain = 0.002                          //Gain on fuel flow
inlet_area = 19.6                               //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920                            //RPM, second stage compressor rated value
static_thrust = 30000                           //Lbs, max rated static thrust at Sea Level
afterburner_available = 0                       //Afterburner available?
reverser_available = 1                          //Thrust reverser available?

[jet_engine]
thrust_scalar = 1.0

[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 30.0
max_generator_alternator_amps = 400.0

        //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,  43.00,   0.00,  -9.70, 1600, 0, 1.442, 55.92, 0.6, 2.5, 0.9, 4.0, 4.0, 0, 220.0, 250.0
point.1=1, -11.20, -12.45, -10.30, 1600, 1, 1.442,  0.00, 1.0, 2.5, 0.9, 6.9, 6.9, 2, 220.0, 250.0
point.2=1, -11.20,  12.45, -10.30, 1600, 2, 1.442,  0.00, 1.0, 2.5, 0.9, 7.1, 7.1, 3, 220.0, 250.0
point.3=2, -19.00, -55.00,  4.00,  1000, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -19.00,  55.00,  4.00,  1000, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -51.00,   0.00, -2.00,  1000, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6=2,  54.00,   0.00, -2.00,  1000, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
point.7=2, -75.00,   0.00, 31.00,  1000, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0

max_number_of_points = 21

static_pitch=0.3        //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=9.2    //feet, altitude of CG when at rest on the ground
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    =  5.0     //Flap angle that activates warning at idle
flap_limit_power   = 25.5     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1         //Parking brake available
toe_brakes_scale = 0.885  //Brake scalar
auto_brakes = 3
hydraulic_system_scalar = 1  //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure

[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 = 53.0, -1.8, 4.3   //(feet) longitudinal, lateral, vertical distance from reference datum

[flaps.0]       //Trailing Edge Flaps
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 20                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 10                                   // degrees
flaps-position.2 = 15                                   // degrees
flaps-position.3 = 20                                   // degrees
flaps-position.4 = 40                                   // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 0.7
drag_scalar = 0.2
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic

[flaps.1]       //Leading Edge Slats
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 10                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 18.0                                 // degrees
flaps-position.2 = 22.0                                 // degrees
flaps-position.3 = 22.0                                 // degrees
flaps-position.4 = 27.0                                 // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 0.3
drag_scalar = 0.2
pitch_scalar= 0.0
system_type = 1                                         //Hydraulic

[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, 5=landing
light.0 = 3, -19.10, -54.15,  5.85, fx_navredm ,
light.1 = 3, -19.10,  54.15,  5.85, fx_navgrem ,
light.2 = 3, -83.60,   0.00,  7.60, fx_navwhih ,
light.3 = 2, -18.60, -53.50,  5.75, fx_strobeh ,
light.4 = 2, -18.60,  53.50,  5.75, fx_strobeh ,
light.5 = 2,   3.70,   0.00, -2.80, fx_beaconb ,
light.6 = 1,  -3.30,   0.00, 11.50, fx_beaconh ,
//light.7 = 4,  53.41,   0.00,  4.50, fx_vclighth ,

[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
direction_indicator.1=3,0

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

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

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

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

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

[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

[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000

[exits]
number_of_exits = 3
exit.0 = 0.4,  45.50, -6.0, 7.0, 0  //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.1 = 0.4, -33.50, 5.85, 0.0, 1  //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.2 = 0.4,  29.90, 6.0,  1.0, 2  //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)

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

[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

[fuel]
Center1   =  -4.0,   0.0, 0.0, 2150, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain  =  -6.4, -16.8, 0.0, 2040, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain =  -6.4,  16.8  0.0, 2040, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftAux   = -15.2, -37.6, 2.0,  780, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux  = -15.2,  37.6, 2.0,  780, 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
fuel_dump_rate = 0.0167                        //Percent of max quantity per second, i.e. about 1 minute for full fuel

[airplane_geometry]
wing_area               = 1320.0                //Square feet
wing_span               = 112.04                 //Feet
wing_root_chord         = 20.0                  //Feet
wing_dihedral           = 6.5                   //Degrees
wing_incidence          = 1.0                   //Degrees
wing_twist              = -0.5                  //Degrees
oswald_efficiency_factor= 0.67                  //Measure of lift effeciency of wing
wing_winglets_flag      = 1                     //Are winglets available?
wing_sweep              = 25.0                  //Degrees, wing leading edge
wing_pos_apex_lon       = 8.4                   //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = -1.6                  //Feet, vertical distance from reference point, positive going up
htail_area              = 280.0                 //Square feet
htail_span              = 39.2                  //Feet
htail_pos_lon           = -69.0                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 3.2                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = 0.0                   //Degrees
htail_sweep             = 34.0                  //Degrees, horizontal tail leading edge
vtail_area              = 288.0                 //Square feet
vtail_span              = 25.6                  //Feet, tip to body
vtail_sweep             = 44.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -35.8                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 12.0                  //Feet, vertical distance from reference point, positive going up
elevator_area           = 70.5                  //Square feet
aileron_area            = 26.9                  //Square feet
rudder_area             = 56.2                  //Square feet
elevator_up_limit       = 22.5                  //Degrees
elevator_down_limit     = 19.5                  //Degrees
aileron_up_limit        = 20.0                  //Degrees
aileron_down_limit      = 20.0                  //Degrees
rudder_limit            = 26.0                  //Degrees
elevator_trim_limit     = 20.0                  //Degrees
spoiler_limit           = 60.0                  //Degrees
spoiler_extension_time  = 2.0			//Seconds
spoilerons_available    = 1                     //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   = 1
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]
flaps_up_stall_speed    = 142.0                 //Knots True (KTAS)
full_flaps_stall_speed  = 113.0                 //Knots True (KTAS)
cruise_speed            = 477.0                 //Knots True (KTAS)
max_mach                = 0.82
max_indicated_speed     = 340                   //Red line (KIAS)

[stall_warning]
type=2
stick_shaker=1

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