[fltsim.0]
title=Wright's Flyer
sim=03flyer
model=
panel=
sound=
texture=
checklists=
atc_id=W1
ui_manufacturer=Wright Bros
ui_type=Flyer
description=Orville and Wilber Wright were the first to demonstrate powered (and controlled) flight to the world.
ui_variation=
atc_heavy=0
atc_airline=
atc_flight_number=

[forcefeedback]
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=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[fltsim.1]
title=
sim=
panel=
sound=
texture=
model=

[fltsim.2]
title=
sim=
panel=
sound=
texture=
model=

[fltsim.3]
title=
sim=
panel=
sound=
texture=
model=

[fltsim.4]
title=
sim=
panel=
sound=
texture=
model=

[fltsim.5]
title=
sim=
panel=
sound=
texture=
model=

[fltsim.6]
title=
sim=
panel=
sound=
texture=
model=

[fltsim.7]
title=
sim=
panel=
sound=
texture=
model=

[fltsim.8]
title=
sim=
panel=
sound=
texture=
model=

[fltsim.9]
title=
sim=
panel=
sound=
texture=
model=

[General]
performance=Length: 19 ft 9 in\nSpan: 40 ft 4 in\nWeight: 750 lbs\nPower: 12 hp @ 400 rpm\nRange: not very far\nDate: December 1903\nDetails:\nDesigner: Orville and Wilber Wright (model by Paul B. KSMS\/KSSC)
atc_type=
atc_model=

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight= 600.000
empty_weight_roll_MOI= 5000.000
empty_weight_pitch_MOI= 6000.000
empty_weight_yaw_MOI= 9000.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 750.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[fuel]
Center1= -1.667, 0.000, 0.000, 1.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area= 510.000
wing_span= 40.000
wing_root_chord= 6.500
wing_dihedral= 2.999
wing_incidence= 0.000
wing_twist= -1.000
oswald_efficiency_factor= 0.250
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 48.000
htail_span= 12.000
htail_pos_lon= -10.000
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 20.000
vtail_span= 6.270
vtail_sweep= 0.000
vtail_pos_lon= -11.220
vtail_pos_vert= 0.000
elevator_area= 48.000
aileron_area= 18.300
rudder_area= 20.000
elevator_up_limit= 20.000
elevator_down_limit= 20.000
aileron_up_limit= 15.000
aileron_down_limit= 15.000
rudder_limit= 20.000
elevator_trim_limit= 20.000
spoiler_limit= 0.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

[contact_points]
point.0= 1.000, -9.500, 0.000, -5.300, 1574.803, 0.000, 0.507, 36.840, 0.571, 2.500, 0.834, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, 4.167, -2.250, -5.000, 1574.803, 1.000, 0.507, 0.000, 0.293, 2.500, 0.786, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, 4.167, 2.250, -5.000, 1574.803, 2.000, 0.507, 0.000, 0.293, 2.500, 0.786, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, 0.000, -20.000, -5.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, 0.000, 20.000, -5.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -13.000, 0.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 2.417, 0.000, 0.000, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 0.000
static_cg_height= 4.900

[GeneralEngineData]
engine_type= 0
Engine.0= -4.000, -2.000, 0.000
Engine.1= -4.000, 2.000, 0.000
fuel_flow_scalar= 1.000

[piston_engine]
max_rpm_mechanical_efficiency_scalar=0.842
idle_rpm_mechanical_efficiency_scalar=0.640
max_rpm_friction_scalar=1.262
idle_rpm_friction_scalar=0.610
cylinder_displacement= 81.800
compression_ratio= 8.000
number_of_cylinders= 4
max_rated_hp= 12.000
max_rated_rpm= 1025.000
fuel_metering_type= 1
cooling_type= 1
normalized_starter_torque= 0.300
turbocharged= 0
max_design_mp= 0.000
min_design_mp= 0.000
critical_altitude= 0.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
power_scalar=0.780


[propeller]
propeller_type= 1
propeller_diameter= 8.000
propeller_blades= 2
propeller_moi= 4.003
beta_max= 5.565
beta_min= 15.000
min_gov_rpm= 100.000
prop_tc= 0.100
gear_reduction_ratio= 1.750
fixed_pitch_beta= 20.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.000
beta_feather= 0.000
power_absorbed_cf= 0.000
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
thrust_scalar=1.000

[flight_tuning]
cruise_lift_scalar=0.920
parasite_drag_scalar=1.500
induced_drag_scalar=0.958
elevator_effectiveness=1.849
aileron_effectiveness=1.000
rudder_effectiveness=4.000
pitch_stability=1.318
roll_stability=0.958
yaw_stability=0.920
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000


[Reference Speeds]
flaps_up_stall_speed= 24.000
full_flaps_stall_speed= 24.000
cruise_speed= 45.000

[keyboard_response]
elevator=200.000000,1000.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000

[Views]
eyepoint=-1, -1, 1.6

[autopilot]
autopilot_available=0
flight_director_available=0

[direction_indicators]
direction_indicator.0=1,0


[SMOKESYSTEM]
smoke.0=-0.5,-2.333,-3.833, fx_smoke_r 
smoke.1=-0.5,-2.333,3.833, fx_smoke_w
smoke.2=-0.5,-2.333,-8.833, fx_smoke_w 
smoke.3=-0.5,-2.333,8.833, fx_smoke_r
smoke.4=-0.5,-2.333,-14.833, fx_smoke_r 
smoke.5=-0.5,-2.333,14.833,  fx_smoke_w
smoke.6=-0.5,-2.333,-22.833, fx_smoke_w 
smoke.7=-0.5,-2.333,22.833,  fx_smoke_r
[Flaps.0]
type= 0
span-outboard= 0.500
extending-time= 0.100
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000