[fltsim.0] title=BT-14 sim=BT-14 model= panel= sound= texture= checklists= description=First flown in prototype form in April 1935, the BT-9 was the end result of North American Aviation's private-venture NA-16 single engine basic trainer for the US Army Air Corps. A total of 226 BT-9s were ordered in three different models providing excellent training for a student and instructor under a tandem glass canopy. The US Navy also took delivery of 40 of the aircraft, which they fitted with a more powerful 600-hp engine and designated the NJ-1. Initially, the aircraft had a fabric skin, but NAA then produced a metal-covered fuselage with a more powerful 450 hp Wright engine, designated the BT-14. 251 aircraft of this variant were bought by the Army Air Corps. Several nations also purchased the BT-14, among them France, which ordered 230, designated the NA-57. An updated version of the NA-57 was designated the NA-64. When France fell to the Germans, 1199 undelivered aircraft were sold to Britain; issued to Canada as the Yale-1. Its lines and overall size are similar to North American's later T-6 / SNJ / Harvard trainer, and the two are often confused. The BT-9 / BT-14 / Yale is easily identified by its fixed landing gear and wheel spats. ui_manufacturer=North American ui_type=BT-14 ui_variation=US Army Air Corps atc_heavy=0 atc_id=NX55903 atc_airline= atc_flight_number= [General] performance=Length: 29 feet\nWing span: 40 feet\nWeight: 4500 lbs\nPower: Pratt & Whitney R-985-25, 450 Hp\nCeiling: 21,650\nMax Speed: 180 mph\nCruise Speed: 146 mph\nStall: 69 mph clean\nRange: 882 miles\n\n\n atc_type=EXPERIMENTAL atc_model= [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=2, 4.6, -21.3, 0.1, fx_strobe , light.1=2, 4.6, 21.3, 0.1, fx_strobe , light.2=4, 5.7, 0, 3.3, fx_vclight , light.0=3, 4.6, -21.3, 0.1, fx_navred , light.1=3, 4.6, 21.3, 0.1, fx_navgre, [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 max_pitch= 10.000 max_pitch_acceleration= 1.000 max_pitch_velocity_lo_alt= 2.000 max_pitch_velocity_hi_alt= 1.500 max_pitch_velocity_lo_alt_breakpoint= 20000.000 max_pitch_velocity_hi_alt_breakpoint= 28000.000 max_bank= 25.000 max_bank_acceleration= 1.800 max_bank_velocity= 3.000 max_throttle_rate= 0.100 nav_proportional_control= 9.000 nav_integrator_control= 0.250 nav_derivative_control= 0.000 nav_integrator_boundary= 2.500 nav_derivative_boundary= 0.000 gs_proportional_control= 9.520 gs_integrator_control= 0.260 gs_derivative_control= 0.000 gs_integrator_boundary= 0.700 gs_derivative_boundary= 0.000 yaw_damper_gain= 0.000 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [Views] eyepoint=4,0.000000,3.9 [SMOKESYSTEM] smoke.0=3, -0.80, 1.40, fx_smoke_w [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= 3314.000 empty_weight_roll_MOI= 8027.000 empty_weight_pitch_MOI= 5230.000 empty_weight_yaw_MOI= 13000.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 4500.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] Center1= 0.000, 0.000, 0.000, 0.000, 0.000 External1= 0.000, 0.000, 0.000, 0.000, 0.000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump= 0 LeftMain= 0.000, 0.000, 0.000, 55.000, 2.000 LeftTip= 0.000, 0.000, 0.000, 0.000, 0.000 RightMain= 0.000, 0.000, 0.000, 55.000, 2.000 RightTip= 0.000, 0.000, 0.000, 0.000, 0.000 [airplane_geometry] wing_area= 248.000 wing_span= 40.000 wing_root_chord= 6.000 wing_dihedral= 2.862 wing_incidence= 0.000 wing_twist= -1.000 oswald_efficiency_factor= 3.759 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 46.000 htail_span= 12.750 htail_pos_lon= -18.083 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 72.000 vtail_span= 9.675 vtail_sweep= 0.000 vtail_pos_lon= -18.083 vtail_pos_vert= 1.500 elevator_area= 19.780 aileron_area= 25.400 rudder_area= 25.200 elevator_up_limit= 27.502 elevator_down_limit= 20.626 aileron_up_limit= 19.481 aileron_down_limit= 14.897 rudder_limit= 23.491 elevator_trim_limit= 19.481 spoiler_limit= 59.989 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, -16.167, 0.000, -0.417, 1574.803, 0.000, 0.542, 61.640, 0.321, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, 2.833, -4.500, -4.333, 1574.803, 1.000, 0.542, 0.000, 0.428, 2.500, 0.701, 0.000, 0.000, 2.000, 0.000, 0.000 point.2= 1.000, 2.833, 4.500, -4.333, 1574.803, 2.000, 0.542, 0.000, 0.428, 2.500, 0.701, 0.000, 0.000, 3.000, 0.000, 0.000 point.3= 2.000, -1.000, -20.917, 1.167, 1574.803, 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, -1.000, 20.917, 1.167, 1574.803, 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, -16.167, 0.000, -0.083, 1574.803, 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, 7.667, 0.000, -0.333, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= 11.646 static_cg_height= 4.001 gear_system_type= 0 [GeneralEngineData] engine_type= 0 Engine.0= 8.333, 0.000, 2.000 fuel_flow_scalar= 1.000 min_throttle_limit= 0.000 [piston_engine] 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 cylinder_displacement= 109.444 compression_ratio= 8.000 number_of_cylinders= 9 max_rated_rpm= 2250.000 max_rated_hp= 450.000 fuel_metering_type= 1 cooling_type= 0 normalized_starter_torque= 0.300 turbocharged= 1 max_design_mp= 36.000 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=1.000 [propeller] propeller_type= 0 propeller_diameter= 9.000 propeller_blades= 2 propeller_moi= 19.136 beta_max= 36.571 beta_min= 15.000 min_gov_rpm= 1400.000 prop_tc= 0.100 gear_reduction_ratio= 1.000 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= 0.000 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 thrust_scalar=1.000 [Reference Speeds] flaps_up_stall_speed= 62.000 full_flaps_stall_speed= 49.600 cruise_speed= 140.000 max_indicated_speed= 209.180 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [direction_indicators] direction_indicator.0=1,0 [brakes] toe_brakes_scale= 1.000 parking_brake= 1 [gear_warning_system] gear_warning_available= 0 pct_throttle_limit= 0.000 flap_limit_power= 0.000 flap_limit_idle= 0.000 [hydraulic_system] normal_pressure= 0.000 [stall_warning] type= 1 [attitude_indicators] attitude_indicator.0= 1 [turn_indicators] turn_indicator.0= 1, 0 [flight_tuning] cruise_lift_scalar=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.185 aileron_effectiveness=1.325 rudder_effectiveness=1.000 elevator_trim_effectiveness=2.002 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 5.000 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= 10.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 30.000, 0.000 flaps-position.4= 45.000, 0.000