[fltsim.0]
title=Grumman  G21A  Goose N873BH
sim=Grumman_G21A
model=
panel=
sound=
texture=N873BH
kb_checklists=GrummanGooseG21A_check
kb_reference=GrummanGooseG21A_ref
atc_id=N873BH
ui_manufacturer="Grumman"
ui_type="G21A Goose"
ui_variation="N873BH"
ui_typerole="Twin Engine Prop"
ui_createdby="Microsoft Corporation"
description="Rugged, roomy, powerful, and amphibian, the Grumman Goose can go just about anywhere. Its flying-boat hull and retractable landing gear provide the ability to take off from and land on a runway or the water, so the Goose can get to places most aircraft can’t. The story of aviation in Alaska and western Canada would not be the same if this sturdy flying boat had never gotten off Grumman’s drawing board. In its seventy years of reliable service, the Goose has never fallen out of favor; it still transports people and delivers goods where few modern aircraft can."

[fltsim.1]
title=Grumman G21A Goose N93GS
sim=Grumman_G21A
model=
panel=
sound=
texture=N93G
kb_checklists=GrummanGooseG21A_check
kb_reference=GrummanGooseG21A_ref
atc_id=N93G
ui_manufacturer="Grumman"
ui_type="G21A Goose"
ui_variation="N93GS"
ui_typerole="Twin Engine Prop"
ui_createdby="Microsoft Corporation"
description="Rugged, roomy, powerful, and amphibian, the Grumman Goose can go just about anywhere. Its flying-boat hull and retractable landing gear provide the ability to take off from and land on a runway or the water, so the Goose can get to places most aircraft can’t. The story of aviation in Alaska and western Canada would not be the same if this sturdy flying boat had never gotten off Grumman’s drawing board. In its seventy years of reliable service, the Goose has never fallen out of favor; it still transports people and delivers goods where few modern aircraft can."

[fltsim.2]
title=Grumman G21A Goose white
sim=Grumman_G21A
model=
panel=
sound=
texture=white
kb_checklists=GrummanGooseG21A_check
kb_reference=GrummanGooseG21A_ref
atc_id=N329
ui_manufacturer="Grumman"
ui_type="G21A Goose"
ui_variation="white"
ui_typerole="Twin Engine Prop"
ui_createdby="Microsoft Corporation"
description="Rugged, roomy, powerful, and amphibian, the Grumman Goose can go just about anywhere. Its flying-boat hull and retractable landing gear provide the ability to take off from and land on a runway or the water, so the Goose can get to places most aircraft can’t. The story of aviation in Alaska and western Canada would not be the same if this sturdy flying boat had never gotten off Grumman’s drawing board. In its seventy years of reliable service, the Goose has never fallen out of favor; it still transports people and delivers goods where few modern aircraft can."

[fltsim.3]
title=Grumman G21A Goose navy-cream
sim=Grumman_G21A
model=
panel=
sound=
texture=1
kb_checklists=GrummanGooseG21A_check
kb_reference=GrummanGooseG21A_ref
atc_id=N327
ui_manufacturer="Grumman"
ui_type="G21A Goose"
ui_variation="Navy-Cream"
ui_typerole="Twin Engine Prop"
ui_createdby="Microsoft Corporation"
description="Rugged, roomy, powerful, and amphibian, the Grumman Goose can go just about anywhere. Its flying-boat hull and retractable landing gear provide the ability to take off from and land on a runway or the water, so the Goose can get to places most aircraft can’t. The story of aviation in Alaska and western Canada would not be the same if this sturdy flying boat had never gotten off Grumman’s drawing board. In its seventy years of reliable service, the Goose has never fallen out of favor; it still transports people and delivers goods where few modern aircraft can."


[General]
atc_type=Grumman
atc_model=G21
editable=0
performance="Cruise Speed\n191 mph		165 kts	308 km\/h\n\nEngines\nPratt & Whitney R-985-AN-6 radials, 450 hp each\n\nPropeller\nHartzell 3-blade constant speed\n\nMaximum Range\n556 nm		1,030 km\n\nService Ceiling\n21,300 ft		6,492 m\n\nFuel Capacity\n95 gal		360 L\n\nEmpty Weight\n2,850 lb		1,295 kg\n\nMaximum Gross Weight\n5,425 lb		2,466 kg\n\nLength\n38 ft, 6 in		11.7 m\n\nWingspan\n49 ft		14.9 m\n\nHeight\n16 ft, 2 in		4.9 m\n\nSeating\n7\n\nUseful Load\n1,595 lb		725 kg"
Category = airplane

[CameraDefinition.0]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing 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 = 17.5, 0.0, 0.0
InitialPbh = 8, 0, 270
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.1]
Title = "Left Wing"
Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED}
Description = View from the left wing 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 = -17.5, 0.0, 0.0
InitialPbh = 8, 0, 90
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.2]
Title = "Tail"
Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.75
ShowWeather = Yes
InitialXyz = 0, 5.0, -23.0
InitialPbh = 11, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

    

[CameraDefinition.001]
Title = "Start-up & taxi"
Guid = {195EAB58-9E4A-1E2A-A34C-A8D9D948F079}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.35
SmoothZoomTime = 6.0
ZoomPanScalar = 2.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=40
HeadingPanRate=70
InitialXyz=-0.025, 0.044, -0.15 //  eyepoint move increment = 0.02 per 1 key stroke
InitialPbh=3, 0, 0

[CameraDefinition.002]
Title = "Right Seat"
Guid = {195EAB58-9E4A-1E2A-A34C-A8D9D948F080}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.35
SmoothZoomTime = 6.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=40
HeadingPanRate=70
InitialXyz=0.8, 0.01, -0.05
InitialPbh=7, 0, 0

[CameraDefinition.003]
Title = "Radio Stack"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F081}
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=0.5, -0.06, 0.0
InitialPbh=18, 0, 0

[CameraDefinition.004]
Title = "Lower left panel"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F082}
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=-0.06, -0.6, 0.0
InitialPbh=0, 0, 0





[WEIGHT_AND_BALANCE]
max_gross_weight = 8700                         // (pounds)
empty_weight = 5425                            // (pounds)

reference_datum_position     =   2.5, 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, -1.3, 0.6        //                Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 170,   0,  1.3, 0.6        //             Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 =   170,  -2.0,  -1.5, 1.1        //  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 =   170,  -2.0,  1.5, 1.1        //  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 =   170,  -5.2,  -1.5, 1.1        //  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 =   170,  -5.2, 1.5, 1.1        //    Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 =   170,  -8.5, -1.5, 1.1        //    Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 =   170,  -8.5, 1.5, 1.1        //    Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8=   0,   5.4,  0.0, 0.0        //     Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9=   331, -14.5,  0.0, 0.0        //         Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10=   110, -16.0,  0.0, 0.0        //         Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_name.0 = "Pilot"     
station_name.1 = "Co-Pilot/Pax"            
station_name.2 = "Pax L 1st Row"  
station_name.3 = "Pax R 1st Row "  
station_name.4 = "Pax L 2d Row"  
station_name.5 = "Pax R 2d Row"  
station_name.6 = "Pax L 3d Row"  
station_name.7 = "Pax R 3d Row" 
station_name.8= "Baggage Nose"    
station_name.9= "Baggage Rear" 
station_name.10= "Repair Kit"   

;Moments of Inertia
empty_weight_pitch_MOI =7500 // 5952
empty_weight_roll_MOI =4028
empty_weight_yaw_MOI =7924
empty_weight_coupled_MOI= 0.0

[airplane_geometry]
wing_area               = 375.0                 //Square feet
wing_span               = 49.0                  //Feet
wing_root_chord         = 8.125                  //Feet
wing_dihedral           = 2.5                   //Degrees
wing_incidence          = 0.0                   //Degrees
wing_twist              = 0.0                   //Degrees
oswald_efficiency_factor= 0.65                  //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 3.0                   //Degrees, wing leading edge
wing_pos_apex_lon       = 1 \\0.0                   //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 4.1                   //Feet, vertical distance from reference point, positive going up
htail_area              = 76.1                  //Square feet           
htail_span              = 17.75                 //Feet
htail_pos_lon           = -19.8                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 5.0                   //Feet, vertical distance from reference point, positive going up
htail_incidence         = -3.0                   //Degrees
htail_sweep             = 15.0                  //Degrees, horizontal tail leading edge
vtail_area              = 21.2                  //Square feet
vtail_span              = 9.2                   //Feet, tip to body
vtail_sweep             = 23.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -19.3                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 3.4                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 36.9                  //Square feet
aileron_area            = 29.64                 //Square feet
rudder_area             = 26.48                 //Square feet
elevator_up_limit       = 28.0                  //Degrees
elevator_down_limit     = 20.0                  //Degrees
aileron_up_limit        = 20.0                  //Degrees
aileron_down_limit      = 20.0                  //Degrees
rudder_limit            = 27.0                  //Degrees
elevator_trim_limit     = 20.0                  //Degrees
spoiler_limit           = 0.0                   //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  =  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= -2.0               //Design G load tolerance (negative, flaps down) 
load_safety_factor         =  1.5               //Design G load safety factor 

[Reference Speeds]
flaps_up_stall_speed    = 60.0                  //Knots True (KTAS)
full_flaps_stall_speed  = 87.0                  //Knots True (KTAS)
cruise_speed            = 100.0                 //Knots True (KTAS)
max_indicated_speed     = 195.0                 //Red line (KIAS)

[flight_tuning]
cruise_lift_scalar = 1
parasite_drag_scalar = 1.1
induced_drag_scalar = 1
elevator_effectiveness = 0.8
aileron_effectiveness = 0.8
rudder_effectiveness = 1.23
pitch_stability = 1.4
roll_stability = 1
yaw_stability = 1
elevator_trim_effectiveness = 0.7
aileron_trim_effectiveness = 1
rudder_trim_effectiveness = 1
hi_alpha_on_roll = 1
hi_alpha_on_yaw = 1
p_factor_on_yaw = 0.5
torque_on_roll = 0.5
gyro_precession_on_yaw  =0.50
gyro_precession_on_pitch=0.50

[fuel]
LeftMain  = -2.6, -8.2, 4.1, 108.0, 2.0     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -2.6,  8.2, 4.1, 108.0, 2.0     //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 = 1
engine_driven_pump=0

[GeneralEngineData]
engine_type = 0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
//Engine.0 =  3.0, -6.2, 4.6                     //(feet) longitudinal, lateral, vertical distance from reference datum
//Engine.1 =  3.0,  6.2, 4.6                     //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.0 =  2, -6.2, 4.6                     //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 =  2,  6.2, 4.6                     //(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]
power_scalar = 1                            //Piston power scalar
cylinder_displacement= 109.44                    //Cubic inches per cylinder
compression_ratio= 6.0                          //Compression ratio
number_of_cylinders= 9                          //Number of cylinders
max_rated_rpm= 2300.0                           //Max rated RPM
max_rated_hp= 450.0                             //Max rated HP
fuel_metering_type= 1                           //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= 36.5                            //Max design manifold pressure, (inHg)
min_design_mp= 2.0                              //Min design manifold pressure, (inHg)
critical_altitude= 5000.0                       //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= 0.0                  //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0.0                //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0                        //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
magneto_order_left_right_both = 1		//sets the order of the magneto switch direction


[propeller]
thrust_scalar = 1.0                             //Propeller thrust scalar
propeller_type= 0                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 7.96 //8.3                         //Propeller Diameter, (feet)
propeller_blades= 3                             //Number of propeller blades
propeller_moi= 15.0                             //Propeller moment of inertia
beta_max= 38 //45.0                                  //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 15 //17                                  //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1200 //800                                //Miminum governed RPM
prop_tc= 0.1                                    //Prop time-constant
gear_reduction_ratio= 1.0                       //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= 0                          //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 0                         //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 0                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available= 0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather= 0 //500                          //Minimum RPM for prop feathering
beta_feather= 0 //87                                 //Feathering pitch angle (degrees)
power_absorbed_cf= 0                            //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available= 0          //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available= 0                       //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta= 0                       //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0                         //Minimum pitch angle in reverse, (degrees)

[contact_points]
	    //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
        //14 Airspeed limit for retraction (KIAS)
        //15 Airspeed that gear gets damage at (KIAS)
//GEAR
point.0 = 1, -18.5,  0.00, -3.1, 1600, 0, 0.52,  180, 0.42, 4.0, 0.90, 5.0, 4.0, 0, 195, 250
point.1 = 1,  -0.8, -3.75, -5.0, 1600, 1, 1.25,   0, 0.50, 2.5, 0.85, 6.0, 5.0, 2, 195, 250
point.2 = 1,  -0.8,  3.75, -5.0, 1600, 2, 1.25,   0, 0.50, 2.5, 0.85, 7.0, 6.0, 3, 195, 250
//FLOATS
//point.3=  4,   5.1, -1.8,  -3.9, 2500, 0, 0.0,    0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0
//point.4=  4,   5.1,  1.8,  -3.9, 2500, 0, 0.0,    0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0
//point.5=  4, -15.3, -1.8,  -2.1, 2500, 0, 0.0,    0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0
//point.6=  4, -15.3,  1.8,  -2.1, 2500, 0, 0.0,    0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0
//Wing Floats
//point.7=  4,  -2.1,-20.5,  -0.8, 1500, 0, 0.0,    0, 0.50, 2.5, 0.70, 12.0, 12.0, 5, 0, 0
//point.8=  4,  -2.1, 20.5,  -0.8, 1500, 0, 0.0,    0, 0.50, 2.5, 0.70, 14.0, 14.0, 5, 0, 0
//point.9=  5,  -6.5,  0.0,  -6.0,    0, 0, 0.0,   20, 0.00, 0.0, 1.00,  0.0,  0.0, 0, 0, 0
//FLOATS
point.3=4,   5.1, -1.8,  -2.8, 2500, 0, 0.0,    0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0
point.4=4,   5.1,  1.8,  -2.8, 2500, 0, 0.0,    0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0
point.5=4, -15.3, -1.8,  -1.7, 2500, 0, 0.0,    0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0
point.6=4, -15.3,  1.8,  -1.7, 2500, 0, 0.0,    0, 0.50, 2.5, 0.70, 0.0, 0.0, 5, 0, 0
//Wing Floats
point.7=4,  -2.1,-20.5,  -1.0, 1500, 0, 0.0,    0, 0.50, 2.5, 0.70, 12.0, 12.0, 5, 0, 0
point.8=4,  -2.1, 20.5,  -1.0, 1500, 0, 0.0,    0, 0.50, 2.5, 0.70, 14.0, 14.0, 5, 0, 0
point.9=5,  -6.5,  0.0,  -6.0,    0, 0, 0.0,   20, 0.00, 0.0, 1.00,  0.0,  0.0, 0, 0, 0
//Scrapes
point.10= 2,  -2.0, -25.5,  4.5, 2500, 0, 0.0,   20, 0.00, 0.0, 1.00,  0.0,  0.0, 0, 0, 0
point.11= 2,  -2.0,  25.5,  4.5, 2500, 0, 0.0,   20, 0.00, 0.0, 1.00,  0.0,  0.0, 0, 0, 0
point.12= 2, -25.5,   0.0, 11.4, 2500, 0, 0.0,   20, 0.00, 0.0, 1.00,  0.0,  0.0, 0, 0, 0
point.13= 2,  10.0,   0.0,  0.0, 2500, 0, 0.0,   20, 0.00, 0.0, 1.00,  0.0,  0.0, 0, 0, 0
point.14= 2, -25.0,   0.0,  1.8, 2500, 0, 0.0,   20, 0.00, 0.0, 1.00,  0.0,  0.0, 0, 0, 0



static_pitch = 7 \\ 6.5              //Degrees
static_cg_height = 4.5         //Feet
gear_system_type=0              //Electric
tailwheel_lock = 1

[Views]
eyepoint =  -0.3, -1.35, 2.83    //Longitudinal, Lateral, Vertical (feet)

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //Percent throttle that activates warning
flap_limit_idle    =  0.0     //Flap angle that activates warning at idle
flap_limit_power   = 31.5     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 0.80  //Brake scalar
differential_braking_scale = 0.80
auto_brakes = 0

[hydraulic_system]
normal_pressure = 0.0       //PSI
electric_pumps  = 0         //no electric pumps
engine_map      = 0	    //no engine pumps

[flaps.0]
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.5                                  // 0.0 .. 1.0
extending-time   = 4                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 30, 96                                   // degrees
flaps-position.2 = 60, 96                                   // degrees
damaging-speed   = 195                                  // KIAS
blowout-speed    = 250                                  // KIAS
system_type      = 2

[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 25.0
max_generator_alternator_amps = 100.0

[vacuum_system]
max_pressure=5.15  //PSI
vacuum_type=1   //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
electric_backup_pressure=0.000000
engine_map=1,1

[pneumatic_system]
max_pressure     = 21.5
bleed_air_scalar = 5.0

[pitot_static]
vertical_speed_time_constant = 1.0              //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.0    //Scalar on heat effectiveness, 0 = not available

[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
[exits]
number_of_exits = 1
exit_rate.0 = 0.4                               ;Percent per second

[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
Adf.2         =1
Transponder.1 = 1
Marker.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 

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

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 700.0
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=25.0
max_bank_acceleration=1.8
max_bank_velocity=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 = 0.0



[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 1, -15.6,   -0.26,  4.4, fx_beacon ,
light.1 = 2,  1.0, -25,   4.5, fx_strobe,
light.2 = 2,  1.0, 25,   4.5, fx_strobe,
light.3 = 2,  -25.2, 0.0,   11.3, fx_strobe,
light.4 =   3,   1.0, -25,   4.5, fx_navred ,
light.5 =   3,   1.0, 25,   4.5, fx_navgre ,
light.6 = 3,  -28.3,   0.00,  4.7, fx_navwhi
light.7 =   6,   -1.3, -13.45,   4.5, fx_landing ,
light.8 =   6,   -1.3, 13.45,   4.5, fx_landing ,
light.9 =  10,   -0.4,     -1.3,  2.93, fx_vclight,
light.10 =  10,   -0.4,     1.3,  2.93, fx_vclight,
light.11 =  10,   -5.0,     0.0,  2.8, fx_vclight,
light.12 =  10,   -8.0,     0.0,  2.8, fx_vclight,



[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

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