[fltsim.0]
title=Waco Red AI
sim=wacoai
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=N20456
ui_manufacturer=WACO
ui_type=Waco Red
ui_variation=
description=Waco Classic
[fltsim.1]
title=Waco Yellow AI
sim=wacoai
model=
panel=
sound=
texture=1
kb_checklists=
kb_reference=
atc_id=N20474
ui_manufacturer=WACO
ui_type=Waco Yellow
ui_variation=
description=Waco Classic
[General]
atc_type=waco
atc_model=
editable=0
performance=Maximum Speed 135mph, Cruise Speed 115mph, Stall speed 47mph, Range 330 miles
[WEIGHT_AND_BALANCE]
max_gross_weight=3068 // (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=0.000000,0.000000,0.000000,0.000000
;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=1.9
induced_drag_scalar=1.0
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=1.0 //Fuel flow scalar
min_throttle_limit=0.000000
[piston_engine]
power_scalar=1.3 //Piston power scalar
cylinder_displacement=90.3 //Cubic inches per cylinder
compression_ratio=8.5 //Compression ratio
number_of_cylinders=7 //Number of cylinders
max_rated_rpm=2400 //Max rated RPM
max_rated_hp=275 //Max rated HP
fuel_metering_type=1 //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 thrust scalar
propeller_type=1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=7.8 //Propeller Diameter, (feet)
propeller_blades=2 //Number of propeller blades
propeller_moi=1.7 //Propeller moment of inertia
beta_max=41.8 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=0.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=1400.0 //Miminum governed RPM
prop_tc=0.1 //Prop time-constant
gear_reduction_ratio=1.0 //Propeller gear reduction ratio
fixed_pitch_beta=20 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=90 //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 //Minimum RPM for prop feathering
beta_feather=0 //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)
//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, -13.300, 0.00, -2.60, 2165.300, 0.000, 0.538, 42.00, 0.800, 2.500, 0.700, 0.000, 0.000,0.000000,0.000000,0.000000
point.1=1.000, 1.50, -2.920, -5.50, 1968.500, 1.000, 0.512, 0.000, 0.400, 2.500, 0.700, 0.000, 0.000, 1.000, 0.000, 0.000
point.2=1.000, 1.50, 2.920, -5.50, 1968.500, 2.000, 0.512, 0.000, 0.400, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000
point.3=2, -3.0, -16.5, -2.1, 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, 16.5, -2.1, 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, -13.300, 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, 3.300, 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
static_pitch=14.0
static_cg_height=4.840
[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
[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=-0.2500000,1.000000,2.900000
[brakes]
toe_brakes_scale=0.457778
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
