[fltsim.0] title=Emb 314 ALX SIVAM sim=Emb 314 model=ALX panel= sound= texture=Sivam kb_checklists=Emb314_check kb_reference=Emb314_ref description=The EMB-314 Super Tucano is an enhanced version, with faster speed and higher altitude, of the EMB-312 Tucano trainer aircraft, which is operational in the Air Forces of 15 countries. The prototype of the Super Tucano first flew in 1992. Both Tucano and Super Tucano have been developed and built by Embraer of Brazil. ui_manufacturer=Embraer ui_type=ALX T29 ui_variation=SIVAM atc_heavy=0 atc_id=5700 atc_airline=Air Force atc_flight_number=5700 [fltsim.1] title=Emb 314 AFA sim=Emb 314 model=AFA panel= sound= texture=AFA kb_checklists=Emb314_check kb_reference=Emb314_ref description=The EMB-314 Super Tucano is an enhanced version, with faster speed and higher altitude, of the EMB-312 Tucano trainer aircraft, which is operational in the Air Forces of 15 countries. The prototype of the Super Tucano first flew in 1992. Both Tucano and Super Tucano have been developed and built by Embraer of Brazil. ui_manufacturer=Embraer ui_type=ALX T29 ui_variation=AFA atc_heavy=0 atc_id=5542 atc_airline=Air Force atc_flight_number=5542 [General] atc_type=ALX atc_model=T29 editable=1 performance=Maximum Speed\n303 kts (TAS) 560 km\/hr\nCruise Speed\n286 kts (TAS) 530 km\/hr at 20,000 ft\n\nEngine\nPratt & Whitney Canada, Inc., PT6A-68-3 \n1.600 shp\nPropeller\nFive-Bladed, Constant Speed, Full Feathering, Reversible Hartzell, 96-inch diameter\n\nMaximum range\nInt. tanks - 809 nm ( 1,500 km )\nWith external tanks - 1,242 nm ( 2,300 km )\nService Ceiling\n32,860 ft 10,668 m\n\nFuel Capacity\n180 gal (internal) 695 L\n\nEmpty Weight 5,330 lb\nMaximum Gross Weight 10,837 lb\nLength 37.1 ft \nWingspan 36.1 ft\n [WEIGHT_AND_BALANCE] max_gross_weight = 10837.000 empty_weight = 5330.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = 0.000, 0.000, 0.000 max_number_of_stations = 50 ;Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.0 =170.000000, -1.000000, 0.000000, 0.000000, Pilot ;station_load.1 ="500.00, 1.50,-7.00,-1.00, pylon LI" //Max 800 lb (bomb) or 582 lb (fuel) ;station_load.2 ="500.00, 1.50, 7.00,-1.00, pylon RI" //Max 800 lb (bomb) or 582 lb (fuel) station_load.3 ="190.00, 0.50,-8.50,-1.00, pylon LE" //Max 500 lb station_load.4 ="190.00, 0.50, 8.50,-1.00, pylon RE" //Max 500 lb ;Moments of Inertia empty_weight_pitch_MOI = 8730.000 empty_weight_roll_MOI = 4880.000 empty_weight_yaw_MOI = 8530.000 empty_weight_coupled_MOI = 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =1.000 induced_drag_scalar =1.000 elevator_effectiveness =1.000 aileron_effectiveness =1.500 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 p_factor_on_yaw = 0.5 torque_on_roll = 0.5 [GeneralEngineData] engine_type = 5 Engine.0 = 6.000, 0.000, 0.000 fuel_flow_scalar = 0.750 min_throttle_limit = -0.25 //Min percent throttle. negative for turb revsr [propeller] thrust_scalar =1.201 propeller_type = 0 propeller_diameter = 7.800 propeller_blades = 5 propeller_moi = 24.000 beta_max = 45.000 beta_min = 10.000 min_gov_rpm = 25000.000 prop_tc = 0.004 gear_reduction_ratio = 15.550 fixed_pitch_beta = 0.000 low_speed_theory_limit = 80.000 prop_sync_available = 0 prop_deice_available = 1 prop_feathering_available= 1 prop_auto_feathering_available= 1 min_rpm_for_feather = 700.000 beta_feather = 88.000 power_absorbed_cf = 0.400 defeathering_accumulators_available= 0 prop_reverse_available = 1.000 minimum_on_ground_beta = 0.000 minimum_reverse_beta = -14.000 [TurbineEngineData] fuel_flow_gain = 0.011 inlet_area = 1.000 rated_N2_rpm = 33000.000 static_thrust = 190.000 afterburner_available = 0 [turboprop_engine] power_scalar =1.000 maximum_torque = 4451.400 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 [pitot_static] vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 0 Com.2 = 1, 0 Nav.1 = 1, 0, 1 Nav.2 = 1, 0, 0 Adf.1 = 1 Transponder.1 = 1 Marker.1 = 1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, -0.58, -17.99, -0.05, fx_navred light.1 = 3, -0.58, 17.99, -0.05, fx_navgre light.2 = 3, -24.00, 0.00, -1.77, fx_navwhi light.3 = 2, -0.60, -18.10, -0.05, fx_strobe light.4 = 2, -0.60, 18.10, -0.05, fx_strobe light.5 = 1, -12.49, 0.00, 0.96, fx_beacon light.6 = 4, 1.58, 0.00, 2.25, fx_vclight light.7 = 5, 1.25, -11.40, -0.80, fx_landing light.8 = 5, 1.25, 11.40, -0.80, fx_landing ;light.9 = 5, 9.75, 0.00, -3.01, fx_landing [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 = 100, 180 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=3,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 2 attitude_indicator.1 = 2 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0=0,0 [airspeed_indicators] airspeed_indicator.0 = 1.183, -24.75 [electrical] max_battery_voltage = 12.0 generator_alternator_voltage = 13.8 max_generator_alternator_amps = 40.0 ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus = 0, 5 , 9.5 avionics = 1, 5 , 9.5 additional_system = 0, 2 , 9.5 marker_beacon = 1, 2 , 9.0 fuel_pump = 0, 5 , 9.0 //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= 1.0, 9.14, 0.00, -5.45, 1900.00, 0.00, 0.55, 40.00, 0.30, 2.20, 0.80, 3.50, 3.50, 0.00, 0.00, 0.00 point.1= 1.0, -1.54, -6.00, -5.70, 2000.00, 1.00, 0.90, 0.00, 0.30, 2.00, 0.70, 3.50, 3.50, 2.00, 0.00, 0.00 point.2= 1.0, -1.54, 6.00, -5.70, 2000.00, 2.00, 0.90, 0.00, 0.30, 2.00, 0.70, 3.50, 3.50, 3.00, 0.00, 0.00 point.3= 2.0, -1.00,-18.00, 0.00, 800.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00 point.4= 2.0, -1.00, 18.00, 0.00, 800.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00 point.5= 2.0,-22.00, 0.00, -2.45, 800.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00, 0.00, 0.00 point.6= 2.0, 0.00, 0.00, -2.45, 800.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00 point.7= 2.0,-22.80, 0.00, 5.78, 800.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00 max_number_of_points = 21 static_pitch = -1.955 static_cg_height= 5.38 gear_system_type= 0 [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.68 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,0,0,0 //pump on Eng1 [Views] eyepoint= -1.4, 0.0, 2.3 //(feet) longitudinal, lateral, vertical distance from reference datum [fuel] //Long(ft), Lat(ft), Vert(ft), usable(gl), Unusable(gl) LeftMain = 0.000, -1.600, 0.500, 180.000, 0.400 RightMain = 0.000, 1.600, 0.500, 180.000, 0.400 ;LeftAux = 1.500, -7.000, -1.000, 90.000, 0.000 ;RightAux = 1.500, 7.000, -1.000, 90.000, 0.000 ;Fuel type: 1=Avgas, 2=JetA fuel_type = 2 number_of_tank_selectors = 1 electric_pump=1 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second [airplane_geometry] wing_area = 190.500 wing_span = 36.100 wing_root_chord = 7.700 wing_dihedral = 4.100 wing_incidence = 2.000 wing_twist = -1.000 oswald_efficiency_factor= 0.700 wing_winglets_flag = 0 wing_sweep = 0.000 wing_pos_apex_lon = 0.000 wing_pos_apex_vert = 0.000 htail_area = 54.000 htail_span = 15.400 htail_pos_lon = -24.300 htail_pos_vert = 0.000 htail_incidence = -1.500 htail_sweep = 0.000 vtail_area = 36.000 vtail_span = 5.200 vtail_sweep = 18.000 vtail_pos_lon = -24.700 vtail_pos_vert = 0.500 elevator_area = 21.980 aileron_area = 24.300 rudder_area = 16.200 elevator_up_limit = 28.000 elevator_down_limit = 26.000 aileron_up_limit = 23.000 aileron_down_limit = 18.000 rudder_limit = 24.000 elevator_trim_limit = 18.000 spoiler_limit = 0.000 spoilerons_available = 0 aileron_to_spoileron_gain = 1.000 min_ailerons_for_spoilerons = 0.000 min_flaps_for_spoilerons = 0.000 spoiler_handle_available = 0 //Defaults to True if spoiler limit > 0, else False. Should be False for spoilerons only [Reference Speeds] flaps_up_stall_speed = 78.000 full_flaps_stall_speed = 66.800 cruise_speed = 286.000 max_mach = 0.65 max_indicated_speed = 303 ////Red line (KIAS) [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1000.0 autothrottle_available= 1 autothrottle_arming_required= 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga= 0 pitch_takeoff_ga = 8; max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=11.00 nav_integrator_control=0.20 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 = 1.0 [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [stall_warning] type=2 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 5.000 system_type= 0 damaging-speed= 210.000 blowout-speed= 250.000 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