[fltsim.0]
title=WACO Model ATO NC143W
sim=WACO Model ATO
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer = Waco Aircraft Corporation
ui_type = WACO ATO 
ui_variation = NC143W
description=1929 WACO ATO Taperwing: The WACO Taperwing is every pilot's dream. Designed in 1928, the Taperwing was a racer that set speed records and won competitions on the racing circuit. As impressive as its speed was, it was its ability to dance that made the Taperwing a legend. For nearly two decades, this craft was the dean of aerobatics and airshows, becoming the plane of choice for many of the world's top performance pilots. Excelling at everything it set out to do, this little biplane remains a legend to this day, although, unfortunately, few remain.
 
[General]
atc_type=biplane
atc_model=
editable=0
performance=Maximum Speed 135mph, Cruise Speed 115mph, Stall speed 47mph, Range 330 miles.

[fltsim.1]
title=WACO Model ATO Flying Farmer
sim=WACO Model ATO
model=
panel=
sound=
texture=Flying Farmer
kb_checklists=
ui_manufacturer = Waco Aircraft Corporation
ui_type = WACO ATO 
ui_variation = Flying Farmer
description=1929 WACO ATO Taperwing: The WACO Taperwing is every pilot's dream. Designed in 1928, the Taperwing was a racer that set speed records and won competitions on the racing circuit. As impressive as its speed was, it was its ability to dance that made the Taperwing a legend. For nearly two decades, this craft was the dean of aerobatics and airshows, becoming the plane of choice for many of the world's top performance pilots. Excelling at everything it set out to do, this little biplane remains a legend to this day, although, unfortunately, few remain.
[General]
atc_type=biplane
atc_model=
editable=0
performance=Maximum Speed 135mph, Cruise Speed 115mph, Stall speed 47mph, Range 330 miles. Textures by Leon Louis

[fltsim.2]
title=WACO Model ATO Flying School
sim=WACO Model ATO
model=
panel=
sound=
texture=Flying School
kb_checklists=
ui_manufacturer = Waco Aircraft Corporation
ui_type = WACO ATO 
ui_variation = Flying School
description=1929 WACO ATO Taperwing: The WACO Taperwing is every pilot's dream. Designed in 1928, the Taperwing was a racer that set speed records and won competitions on the racing circuit. As impressive as its speed was, it was its ability to dance that made the Taperwing a legend. For nearly two decades, this craft was the dean of aerobatics and airshows, becoming the plane of choice for many of the world's top performance pilots. Excelling at everything it set out to do, this little biplane remains a legend to this day, although, unfortunately, few remain.

[General]
atc_type=biplane
atc_model=
editable=0
performance=Maximum Speed 135mph, Cruise Speed 115mph, Stall speed 47mph, Range 330 miles. Textures by Leon Louis

[fltsim.3]
title=WACO Model ATO Irish Eyes Pub
sim=WACO Model ATO
model=
panel=
sound=
texture=Irish Eyes Pub
kb_checklists=
ui_manufacturer = Waco Aircraft Corporation
ui_type = WACO ATO 
ui_variation = Irish Eyes Pub
description=1929 WACO ATO Taperwing: The WACO Taperwing is every pilot's dream. Designed in 1928, the Taperwing was a racer that set speed records and won competitions on the racing circuit. As impressive as its speed was, it was its ability to dance that made the Taperwing a legend. For nearly two decades, this craft was the dean of aerobatics and airshows, becoming the plane of choice for many of the world's top performance pilots. Excelling at everything it set out to do, this little biplane remains a legend to this day, although, unfortunately, few remain.

[fltsim.4]
title=WACO Model ATO Black and Red
sim=WACO Model ATO
model=
panel=
sound=
texture=1
kb_checklists=
ui_manufacturer = Waco Aircraft Corporation
ui_type = WACO ATO 
ui_variation = black and red
description=1929 WACO ATO Taperwing

[WEIGHT_AND_BALANCE]
max_gross_weight=3127                         // (pounds)
empty_weight=2500                            // (pounds)

reference_datum_position=0, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-0.1, 0, 0        // (feet) longitudinal, lateral, vertical 

max_number_of_stations=50


station_load.0= 170.0, -2.625, 0.0, -3.8, passenger		
station_load.1= 170.0, -5.625, 0.0, -3.8, pilot		
	 

;Moments of Inertia
empty_weight_pitch_MOI=8346
empty_weight_roll_MOI=8948
empty_weight_yaw_MOI=8367
empty_weight_coupled_MOI=0.0

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.5
induced_drag_scalar=1.5
elevator_effectiveness=2.0
aileron_effectiveness=1.25
rudder_effectiveness=1.2
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=2.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[Flaps.0]
type=0
span-outboard=0.5
extending-time=0.0
system_type=0
flaps-position.0=0.0, 0.0
flaps-position.1=0.0, 0.0

[GeneralEngineData]
engine_type=0                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=8.3, 0.0, 0.5                        //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000

[piston_engine]
power_scalar=1.0                              //Piston power scalar
cylinder_displacement=109                     //Cubic inches per cylinder
compression_ratio=6.0                          //Compression ratio
number_of_cylinders=9                           //Number of cylinders
max_rated_rpm=2400                             //Max rated RPM
max_rated_hp=275                               //Max rated HP
fuel_metering_type=2                           //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter
cooling_type=0                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3                  //Starter torque factor
turbocharged=0                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=0                                //Max design manifold pressure, (inHg)
min_design_mp=0                                //Min design manifold pressur x x xH{)
critical_altitude=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                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=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



[propeller]
thrust_scalar = 1.0                           
propeller_type= 0                              
propeller_diameter= 9.0                       
propeller_blades= 2                           
propeller_moi= 6.4                        
beta_max= 45.0                                 
beta_min= 15.0                               
min_gov_rpm= 1850                            
prop_tc= 0.0045                                
gear_reduction_ratio= 1.0                 
fixed_pitch_beta= 0                            
low_speed_theory_limit= 80                  
prop_sync_available= 0                       
prop_deice_available= 0                       
prop_feathering_available= 0                 
prop_auto_feathering_available= 0 
min_rpm_for_feather= 0                   
beta_feather= 0                                
power_absorbed_cf= 0                          
defeathering_accumulators_available= 0        
prop_reverse_available= 0                    
minimum_on_ground_beta= 0                   
minimum_reverse_beta= 0 

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
flap_motor         = 3, 0 , 1.0
gear_motor         = 3, 0 , 1.0
autopilot          = 3, 0 , 1.0
avionics_bus       = 3, 0 , 1.0
avionics           = 3, 0 , 1.0
pitot_heat         = 3, 0 , 1.0
additional_system  = 3, 0 , 1.0
marker_beacon      = 3, 0 , 1.0
gear_warning       = 3, 0 , 1.0
fuel_pump          = 3, 0 , 1.0
starter1           = 3, 0 , 1.0
light_nav          = 3, 0 , 1.0
light_beacon       = 3, 0 , 1.0
light_landing      = 3, 0 , 1.0
light_taxi         = 3, 0 , 1.0
light_strobe       = 3, 0 , 1.0
light_panel        = 0, 0 , 1.0
light_cabin        = 3, 0 , 1.0
light_wing         = 3, 0 , 1.0
light_logo         = 3, 0 , 1.0
light_recognition  = 3, 0 , 1.0

//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]
point.0=1.000,-10.200, 0.00,-0.2,2165.300,0.000, 0.000,42.00,0.100,2.500,0.999,0.000, //0.000,0.000000,0.000000,0.000000
point.1=1.000,  6.55, -3.23, -4.85 ,1968.500, 1.000, 0.512,0.000, 0.200, 2.500, 0.900, 0.000, 0.000, 1.000, 0.000, 0.000
point.2=1.000,  6.55,  3.23, -4.85 ,1968.500, 2.000, 0.512,0.000, 0.200, 2.500, 0.900, 0.000, 0.000, 2.000, 0.000, 0.000
point.3=2, 3.0, -15.5, -1.1 ,  1387.40, 0, 0.0000,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2,  3.0,  15.5, -1.1,  1387.40, 0, 0.0000,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2, -7.300,   0.00,  0.2,  1787.40, 0, 0.0000,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2,  10.600,   0.00,  0.2 ,  1787.40, 0, 0.0000,   0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0


static_pitch=15.0
static_cg_height=2.8

[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
Transponder.1=1
Marker.1=1


[LIGHTS]
Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
light.0=3,  4.5, -15.0, 4.00, fx_navred
light.1=3,  4.5,  15.0, 4.00, fx_navgre
light.2=1,-9.48,   0.00, 4.75, fx_navwhi.fx
light.3=4,  1.00,   0.05, 2.00, 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=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=1,0

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

[SMOKESYSTEM]
smoke.0=1.00, 0.00, -14.00, fx_smoke_w
smoke.1=1.00, 0.00,  14.00, fx_smoke_w


[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)

avionics_bus=0, 1, 17.0
avionics=1, .3 , 17.0

fuel_pump=0, .3 , 17.0
starter1=0, 2, 17.0
light_nav=0, .1 , 17.0
light_beacon=0, .1 , 17.0
light_landing=0, .3 , 17.0
light_panel=0,.1 , 17.0

[fuel]
LeftMain=0.0, 0.0, 0.0, 24.0, 0.0       //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=0.0, 0.0, 0.0, 24.0, 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=1

[airplane_geometry]
wing_area=224.0                 //Square feet
wing_span=30.8                  //Feet
wing_root_chord=4.9                   //Feet
wing_dihedral=1.0                   //Degrees
wing_incidence=1.0                   //Degrees
wing_twist=1.0                  //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=1.2                   //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.0                   //Feet, vertical distance from reference point, positive going up
htail_area=40.0                  //Square feet
htail_span=11.7                  //Feet
htail_pos_lon=-24.7                 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0                   //Feet, vertical disô½ô½ô½ô½om reference point, positive going up
htail_incidence=0.0                   //Degrees
htail_sweep=0.0                   //Degrees, horizontal tail leading edge
vtail_area=28.0                  //Square feet
vtail_span=4.8                   //Feet, tip to body
vtail_sweep=0.0                   //Degrees, vertical tail leading edge
vtail_pos_lon=-22.6                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=0.0                   //Feet, vertical distance from reference point, positive going up
elevator_area=16.6                  //Square feet
aileron_area=18.3                  //Square feet
rudder_area=6.7                   //Square feet
elevator_up_limit=28.0                  //Degrees
elevator_down_limit=21.0                  //Degrees
aileron_up_limit=20.0                  //Degrees
aileron_down_limit=15.0                  //Degrees
rudder_limit=24.0                  //Degrees
elevator_trim_limit=19.5                  //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

[Reference Speeds]
flaps_up_stall_speed=44.0                  //Knots True (KTAS)
full_flaps_stall_speed=44.0                  //Knots True (KTAS)
cruise_speed=99.0                  //Knots True (KTAS)
max_indicated_speed=180.000000

[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

//[contact_points]
//static_pitch=0.000000
//static_cg_height=0.000000

[Views]
eyepoint=-0.2500000,0.040000,2.750000

[brakes]
toe_brakes_scale=0.8
parking_brake=1
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0