[fltsim.0]
title=Ryan STA
sim=STA
panel=
model=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Ryan
ui_type=ST
ui_variation=YPT-16
description=\n The military version of Ryan STA trainer, powered with 125 h.p. Menasco C-4 engine. Starter added.
atc_heavy=0
atc_airline=
atc_flight_number=

[fltsim.1]
title=Ryan STA1
sim=STA
panel=
model=1
sound=
texture=14985
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Ryan
ui_type=STA
ui_variation=NC 14985
description=\n Sport trainer NC 14985, c\/n 117 was built as a 95 h.p. Menasco B-4 powered ST model originally. It became an ST-A later, when a 125 h.p. Menasco D-4 engine was installed. 
atc_heavy=0
atc_airline=
atc_flight_number=

[fltsim.2]
title=Ryan STA2
sim=STA
panel=
model=1
sound=
texture=14987
kb_checklists=
kb_reference=
atc_id=
ui_manufacturer=Ryan
ui_type=STA
ui_variation=NC 14987
description=\n Sport trainer NC 14987, powered with 125 h.p. Menasco C-4. 


[General]
atc_type=
atc_model=
atc_heavy=0
atc_airline=
atc_flight_number=
performance=Specifications:Wing span 30. Length 21 5.37. Height 6 11. Empty weight 1081 lbs. Useful load 565 lbs.Fuel 24 gals. \n
Category = airplane
prop_anim_ratio=0,8


[weight_and_balance]
max_gross_weight = 1570.000
empty_weight = 1081.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = -0.100, 0.000, 0.000
empty_weight_pitch_MOI = 800.000
empty_weight_roll_MOI = 500.000
empty_weight_yaw_MOI = 1050.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit = 0.000
CG_aft_limit = 1.000

max_number_of_stations = 3

station_load.0 =174.000000, -0.500000, 0.000000, 0.000000, Station 1
station_load.1=174.000000, -3.000000, 0.000000, 0.000000, Station 2 



[GeneralEngineData]
engine_type = 0
fuel_flow_scalar = 1.000
min_throttle_limit = 0.05
engine.0 = 5.180, 0.000, -1.500 

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
windshield_rain_effect_available = 1

[fuel]
fuel_type = 1
number_of_tank_selectors = 1
electric_pump = 1

Center1 = 1.620, 0.000, 0.000, 24.000, 0.000


[contact_points]
static_pitch = 13.200
static_cg_height = 5.400
tailwheel_lock = 1
gear_system_type = 0
max_number_of_points = 7

point.0 = 1.000, -12.793, 0.000, -2.300, 2500.000, 0.000, 0.350, 45.000, 0.100, 2.500, 0.800, 0.000, 0.000, 0.000, 0.000, 0.000
point.1 = 1.000, 1.300, -2.850, -5.460, 2500.000, 1.000, 0.800, 0.000, 0.150, 2.500, 0.800, 0.000, 0.000, 2.000, 0.000, 0.000
point.2 = 1.000, 1.300, 2.850, -5.460, 2500.000, 2.000, 0.800, 0.000, 0.150, 2.500, 0.800, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, 0.000, 15.000, -1.300, 2500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.4= 2.000, 0.000, -15.000, -1.300, 2500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000



[keyboard_response]
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000

[airplane_geometry]
wing_area = 124.000
wing_span = 30.000
wing_root_chord = 4.730
wing_dihedral = 4.000
wing_incidence = 0.200
wing_twist = 0.000
oswald_efficiency_factor = 0.680
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = 0.300
wing_pos_apex_vert = -2.050
htail_area = 22.000
htail_span = 9.560
htail_pos_lon = -10.480
htail_pos_vert = -0.330
htail_incidence = 0.000
htail_sweep = 0.000
vtail_area = 11.950
vtail_span = 3.780
vtail_sweep = 0.000
vtail_pos_lon = -10.740
vtail_pos_vert = 0.000
elevator_area = 10.000
aileron_area = 11.386
rudder_area = 7.250
elevator_up_limit = 28.000
elevator_down_limit = 21.000
aileron_up_limit = 20.000
aileron_down_limit = 15.000
rudder_limit = 24.000
elevator_trim_limit = 19.500
spoiler_limit = 45.000
aileron_to_spoileron_gain = 0.000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1
electric_always_available = 0
pitot_heat = 0, 2, 17

[flight_tuning]
cruise_lift_scalar=1.000 
parasite_drag_scalar=1.000 
induced_drag_scalar=1.000 
elevator_effectiveness=1.000 
aileron_effectiveness=2.000 
rudder_effectiveness=1.000 
pitch_stability=1.000 
roll_stability=1.000 
yaw_stability=1.000 
elevator_trim_effectiveness=1.000 
aileron_trim_effectiveness=1.000 
rudder_trim_effectiveness=1.000 

[piston_engine]
power_scalar=1.000 
cylinder_displacement= 82.000 
compression_ratio= 5.500 
number_of_cylinders= 4 
max_rated_rpm= 2170.000 
max_rated_hp= 125.000 
fuel_metering_type= 2 
cooling_type= 0 
normalized_starter_torque= 0.600 
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 
fuel_flow_scalar=1.000
max_rpm_mechanical_efficiency_scalar=1.000 
idle_rpm_mechanical_efficiency_scalar=1.000 
max_rpm_friction_scalar=1.000 
idle_rpm_friction_scalar=1.000 
 
[propeller]
thrust_scalar=1.000 
propeller_type= 1 
propeller_diameter= 6.600 
propeller_blades= 2 
propeller_moi= 5.200 
beta_max= 0.000 
beta_min= 0.000 
min_gov_rpm= 0.000 
prop_tc= 0.000 
gear_reduction_ratio= 1.000 
fixed_pitch_beta= 19.000 
low_speed_theory_limit= 80.000 
prop_sync_available= 0 
prop_deice_available= 0 
prop_reverse_available= 0.000 
minimum_on_ground_beta= 0.000 
minimum_reverse_beta= 0.000 
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 

[brakes]
toe_brakes_scale=0.65
parking_brake=1
differential_braking_scale= 1.000
	
[hydraulic_system]
normal_pressure=0.000000

[Views]
eyepoint=-4.1,0.0,1.10
VIEW_FORWARD_ZOOM=0.50
VIEW_FORWARD_DIR=4.5, 0.0, 0.0

[altimeters]
altimeter.0=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=2,0

[direction_indicators]
direction_indicator.0=1,0 

[vacuum_system]
max_pressure=5.15   //PSI
vacuum_type=1       //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
engine_map=1

[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000

[pitot_static]
vertical_speed_time_constant = 1                
pitot_heat = 1.0    //Scalar on heat effectiveness, 0 = not available

[Reference Speeds]
flaps_up_stall_speed= 46.000 
full_flaps_stall_speed= 38.000 
cruise_speed= 99.000 
max_indicated_speed=190.000000

[stall_warning]
type=1

[deice_system]
structural_deice_type=0


[autopilot]
autopilot_available= 0
flight_director_available= 0

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 4.000
system_type= 3
damaging-speed= 87.000
blowout-speed= 80.000
lift_scalar= 1.600
drag_scalar= 0.500
pitch_scalar= 0.100
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 16.000, 0.000
flaps-position.3= 28.000, 0.000
flaps-position.4= 40.000, 0.000