[fltsim.0] title=WACO ATO NC 7446 today sim=WACO_R-975 model= panel= sound= texture=7446 kb_checklists= ui_manufacturer = Waco Aircraft Company ui_type = WACO ATO ui_variation =Northwest Airways Inc. #5 (NC 7446) with R-975E-1 description= [fltsim.1] title=WACO JYM NC991H today sim=WACO_R-975 model=1 panel= sound= texture=NC991H kb_checklists= ui_manufacturer = Waco Aircraft Company ui_type = WACO JYM ui_variation =Northwest Airways Inc. #6 (NC991H) with R-975E-1 [fltsim.2] title=WACO JYM NC731K today sim=WACO_R-975 model=1 panel= sound= texture=NC731K kb_checklists= ui_manufacturer = Waco Aircraft Company ui_type = WACO JYM ui_variation =Northwest Airways Inc. #8 (NC731K) with R-975E-1 [General] atc_type=biplane atc_model= editable=0 performance=Empty Weight:1700 pounds\Useful Load:900 pounds\Gross Weight:2600 pounds\nEngine\s Wright R-975E-1 Whirlwind \n365 HP at 2100 RPM\Service Ceiling:19,000\Fuel Capacity:60 U. S. gallons usable Category=airplane [WEIGHT_AND_BALANCE] max_gross_weight=2900 empty_weight=1800 reference_datum_position=0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position= -.500, 0.000, 2.000 max_number_of_stations=4 station_load.0= 170, 0.125, 1.0, -0.800, rt passenger station_load.1= 170, 0.125, -1.0, -0.800, lt passenger station_load.2= 170, -3.125, 0.0, -0.800, pilot station_load.3= 40, -4.625, 0.0, 0.700, baggage ;Moments of Inertia empty_weight_pitch_MOI=2408 empty_weight_roll_MOI=2258 empty_weight_yaw_MOI=2718 empty_weight_coupled_MOI=0.0 [flight_tuning] cruise_lift_scalar=1.15 parasite_drag_scalar=1.1 induced_drag_scalar=1.0 elevator_effectiveness=2.5 aileron_effectiveness=1.0 rudder_effectiveness=1.250 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=1.5 p_factor_on_yaw=1.00000 torque_on_roll=1.00000 gyro_precession_on_roll=1.00000 gyro_precession_on_yaw=1.00000 [GeneralEngineData] engine_type=0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=4.8, 0.000, 0.000 //(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=108.33 //Cubic inches per cylinder compression_ratio=6.1 //Compression ratio number_of_cylinders=9 //Number of cylinders max_rated_rpm=2100 //Max rated RPM max_rated_hp=365 //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=29.92 //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) supercharged=1 ; on/off supercharger_boost_low_end=1.00 //multiplier on manifold pressure at low RPM supercharger_boost_high_end=2.3 //multiplier on manifold pressure at high RPM supercharger_power_cost=0.1 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=1.250 //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 detonation_onset=30.5 BestPowerSpecificFuelConsumption=0.48 [propeller] thrust_scalar = 1.0 propeller_type= 1 propeller_diameter= 8.55 propeller_blades= 2 propeller_moi= 10.0 beta_max= 45.0 beta_min= 15.0 min_gov_rpm= 1250 prop_tc= 0.0045 gear_reduction_ratio= 1.0 fixed_pitch_beta= 22.0 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 = 24.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps = 60.0 electric_always_available =0 ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor = 0, 5 , 17.0 gear_motor = 0, 5 , 17.0 autopilot = 0, 5 , 17.0 avionics_bus = 0, 10, 17.0 avionics = 1, 5 , 17.0 pitot_heat = 0, 2 , 17.0 additional_system = 0, 20, 17.0 marker_beacon = 1, 2 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 17.0 starter1 = 0, 20, 17.0 light_nav = 0, 5 , 17.0 light_beacon = 0, 5 , 17.0 light_landing = 0, 5 , 17.0 light_taxi = 0, 5 , 17.0 light_strobe = 0, 5 , 17.0 light_panel = 0, 5 , 17.0 //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.1=1.000, 6.55, -3.23, -4.85 ,1968.500, 1.000, 1.25, 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.2=1.000, 6.55, 3.23, -4.85 ,1968.500, 2.000, 1.25, 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 gear_system_type=0 tailwheel_lock=0 [Views] eyepoint=0.210,0.0,2.717 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=0, 0 Nav.1=1, 1, 1 Nav.2=0, 0, 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_beacon.fx light.3=4, 0.5, 0.30, 2.60, fx_vclight light.4=4, 0.5, 0.100, 2.60, fx_vclight light.4=4, 0.5, -0.100, 2.60, fx_vclight light.4=4, 0.5, -0.300, 2.60, 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=fx_sparks startup=fx_ATO_start touchdown=fx_tchdwn_s, 1 [SMOKESYSTEM] smoke.0=0, 4, 0, fx_smoke_w [fuel] Center1 = 1.00, 0.000, 0.0, 60.00, 0.00 fuel_type=1 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=227 wing_span=30.33 wing_root_chord=5.2 wing_dihedral=0.0 wing_incidence=2.5 wing_twist=0.0 oswald_efficiency_factor=0.760 wing_winglets_flag=0 wing_sweep=0.0 wing_pos_apex_lon=1.2 wing_pos_apex_vert=0.0 htail_area=16.10 htail_span=11.10 htail_pos_lon=-13.75 htail_pos_vert=0.0 htail_incidence=0.0 htail_sweep=20 vtail_area=11.9 vtail_span=4.8 vtail_sweep=20 vtail_pos_lon=-13.6 vtail_pos_vert=1.0 elevator_area=14.75 aileron_area=27.6 rudder_area=7.8 elevator_up_limit=28.0 elevator_down_limit=21.0 aileron_up_limit=27.0 aileron_down_limit=22.0 rudder_limit=24.0 elevator_trim_limit=19.5 spoiler_limit=0.0 spoilerons_available=0 aileron_to_spoileron_gain=0.0 min_ailerons_for_spoilerons=0.0 min_flaps_for_spoilerons=0.0 spoiler_handle_available=0 auto_spoiler_available=0 positive_g_limit_flaps_up=4.5 positive_g_limit_flaps_down=3.0 negative_g_limit_flaps_up=-3.5 negative_g_limit_flaps_down=-2.0 [Reference Speeds] flaps_up_stall_speed=44 cruise_speed=130 max_indicated_speed=180 max_mach=1.0 full_flaps_stall_speed=35.200000 [autopilot] autopilot_available=1 flight_director_available=0 autothrottle_available=0 autothrottle_arming_required=0 default_pitch_mode=0 default_bank_mode=0 use_no_default_bank=1 use_no_default_pitch=1 default_vertical_speed=1000 autothrottle_takeoff_ga=1.0 autothrottle_max_rpm=90.0 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=1.50 max_pitch_velocity_lo_alt_breakpoint=20000 max_pitch_velocity_hi_alt_breakpoint=28000 max_bank=25.00000 max_bank_acceleration=1.8 max_bank_velocity=3.0 max_throttle_rate=0.10 nav_proportional_control=9.0 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 [forcefeedback] ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1 crash_magnitude1=10000 crash_direction1=1000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 gear_bump_nose_magnitude=6000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=6000 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=6000 gear_bump_right_direction=500 gear_bump_right_duration=250000 stick_shaker_magnitude=5000 stick_shaker_direction=0 stick_shaker_period=111111 [brakes] toe_brakes_scale=1.20 differential_braking_scale = 1.0 parking_brake=1 [hydraulic_system] normal_pressure=0.00000 [stall_warning] type=1 stick_shaker=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [Flaps.0] type=1 span-outboard=0.0000 extending-time=0.000000 system_type=0 [pitot_static] pitot_heat=1.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=1 electric_backup_pressure=0.000000 engine_map=1,0,0,0 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=0.000000 [deice_system] structural_deice_type=0 [propeller] propeller_type=1 propeller_diameter=8.250000 propeller_blades=2 propeller_moi=5.000000 beta_max=0.000000 beta_min=0.000000 min_gov_rpm=0.000000 prop_tc=0.000000 gear_reduction_ratio=1.000000 fixed_pitch_beta=20.650000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_reverse_available=0.000000 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000