[fltsim.0] title=WACO CTO Mailwing sim=WACO CTO Mailwing model= panel= sound= texture= kb_checklists= ui_manufacturer = Waco Aircraft Corporation ui_type = WACO CTO Mail Wing ui_variation = North West Airlines Inc. description=1929 WACO CTO Mailwing [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 CTO Mailwing US Air Mail sim=WACO CTO Mailwing model= panel= sound= texture=Air Mail kb_checklists= ui_manufacturer = Waco Aircraft Corporation ui_type = WACO CTO Mail Wing ui_variation = US Air Mail. description=1929 WACO CTO Mailwing [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 [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=1.7 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=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_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