[fltsim.0]
title=WACO ATO NC 7446
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)
description=

[fltsim.1]
title=WACO JYM NR42M early
sim=WACO_R-975
model=
panel=
sound=
texture=NR42M_old
kb_checklists=
ui_manufacturer = Waco Aircraft Company
ui_type = WACO JYM
ui_variation =Northwest Airways Inc. #7  (NR42M) early
description=

[fltsim.2]
title=WACO JYM NR42M late
sim=WACO_R-975
model=1
panel=
sound=
texture=NR42M
kb_checklists=
ui_manufacturer = Waco Aircraft Company
ui_type = WACO JYM
ui_variation =Northwest Airways Inc. #7 (NR42M) late

[fltsim.3]
title=WACO JYM NC991H
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)

[fltsim.4]
title=WACO JYM NC731K
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)

[fltsim.5]
title=WACO JYM NC631N
sim=WACO_R-975
model=1
panel=
sound=
texture=NC631N
kb_checklists=
ui_manufacturer = Waco Aircraft Company
ui_type = WACO JYM
ui_variation =Northwest Airways Inc. #9 (NC631N)





[General]
atc_type=biplane
atc_model=
editable=0
performance=Empty Weight:1700 pounds\Useful Load:900 pounds\Gross Weight:2600 pounds\nEngine\s Wright J6-9 Whirlwind \n330 HP at 2000 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=5.10                          //Compression ratio
number_of_cylinders=9                           //Number of cylinders
max_rated_rpm=2000                             //Max rated RPM
max_rated_hp=330                               //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{)
supercharged=1                                  ; on/off
supercharger_boost_low_end=1.00                 //multiplier on manifold pressure at low RPM
supercharger_boost_high_end=2.2          //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
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= 22.5                            
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, 0
Com.2=0, 0
Nav.1=0, 0, 0
Nav.2=0, 0, 0
Adf.1=0
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=3,-9.48,   0.00, 4.75, fx_navwhi
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