[fltsim.0] title=RAF_Tucano sim=MG_Tucano_Multiplayer model=Shorts_Tucano_Multiplayer texture= prop_anim_ratio=0.2 atc_airline= atc_parking_types=MIL_COMBAT atc_parking_codes= ui_manufacturer=MG_Shorts_Tucano ui_type=Shorts_Tucano_RAF_Multi-Player ui_variation=Multi-Player Version description=Turboprop basic trainer atc_id_font=Verdana,-11,1,600,0 [fltsim.1] title=RAF_Tucano_ZF200 sim=MG_Tucano_Multiplayer model=Shorts_Tucano_Multiplayer texture=RAF_ZF200 prop_anim_ratio=0.2 atc_airline= atc_parking_types=MIL_COMBAT atc_parking_codes= ui_manufacturer=MG_Shorts_Tucano ui_type=Shorts_Tucano_RAF_Multi-Player_ZF200 ui_variation=Multi-Player Version description=Turboprop basic trainer atc_id_font=Verdana,-11,1,600,0 [General] atc_type=silent atc_model=Tucano editable=1 performance=Model Designer: Mark Griggs\nFlight model\ Mike MacIntyre\nFDE, General characteristics Crew: 1-2 Length: 32 ft 4 in (9.85 m) Wingspan: 37 ft 0 in (11.28 m) Powerplant: 1 × Garrett TPE331-12B turboprop, 1,100 shp (820 kW) [WEIGHT_AND_BALANCE] max_gross_weight = 7220 empty_weight = 4447 reference_datum_position = 14.1, 0, 0 empty_weight_CG_position = -13.6, 0, 0 empty_weight_pitch_MOI = 18665.000 empty_weight_roll_MOI = 3623.000 empty_weight_yaw_MOI = 16500.000 empty_weight_coupled_MOI = 0.000 max_number_of_stations = 0 station_load.0 = 0, -10.3, 0.0, 0 station_load.1 = 0, -14.3, 0.0, 0 [GeneralEngineData] engine_type = 5 Engine.0 = -3.865, 0, 0 fuel_flow_scalar = 0.8 min_throttle_limit = 0.0 [TurbineEngineData] fuel_flow_gain = 0.08 inlet_area = 0.1 rated_N2_rpm = 32920 static_thrust = 20 afterburner_available = 0 reverser_available = 0 [turboprop_engine] power_scalar = 1 maximum_torque = 5000 [Reference Speeds] flaps_up_stall_speed = 75.600 full_flaps_stall_speed = 64.300 cruise_speed = 240 max_indicated_speed = 290 //max_mach = 0.45 //0 Class <0=none,1=wheel, 2=scrape, 3=float> //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) max_mach=0.550000 //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at [contact_points] static_pitch = -1.100 static_cg_height = 0.40 gear_system_type =0 max_number_of_points = 4 point.0 = 1, -4.6, 0.00, -0.28, 1181.1, 0, 0.6349, 46.8, 0.4, 1.2, 0.91, 5.0, 5.0, 0, 260, 260 point.1 = 1, -14.9, -6.25, -0.44, 1574.8, 1, 0.9349, 0.0, 0.4, 1.2, 0.60, 4.0, 4.0, 2, 260, 260 point.2 = 1, -14.9, 6.25, -0.44, 1574.8, 2, 0.9349, 0.0, 0.4, 1.2, 0.60, 4.0, 4.0, 3, 260, 260 point.3 = 5, 13.7, 0000, -0.28, 1181.1, 0, 0.0000, 50.0, 0.0, 0.0, 1.00, 1.0, 1.2, 0, 0, 0 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -12.8, -18, 4.80, fx_f16_navredm light.1 = 3, -12.8, 18, 4.80, fx_f16_navgrem light.2 = 3, -34.5, 0, 4.35, fx_f16_navwhih light.3 = 2, -12.8, -18, 4.80, Marks_White_Fighter_WingStrobe.fx light.4 = 2, -12.8, 18, 4.80, Marks_White_Fighter_WingStrobe.fx light.5 = 2, -12.8, -18.2, 4.8, fx_Vortices light.6 = 2, -12.8, 18.2, 4.8, fx_Vortices [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_nicks_tchdwn_s, 1 windshield_rain_effect_available = 0 [brakes] parking_brake = 1 //Parking brake availabl toe_brakes_scale = 1.00 //Brake scalar [Flaps.0] type=1 span-outboard=0.5 // Percent span for flap position extending-time=5.7 // Seconds, time to fully extend system_type=0 // 0 = electrical damaging-speed = 185 // KIAS blowout-speed = 195 // KIAS flaps-position.0= 0 // degrees flaps-position.1=10,140 // degrees flaps-position.2=25,120 // degrees flaps-position.3=40,100 // degrees [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 electric_pump = 1 LeftMain = -15.3, -1.1, 2.9, 91, 1.2 RightMain = -15.3, 1.1, 2.9, 91, 1.2 [airplane_geometry] wing_area = 208.000 wing_span = 37.000 wing_root_chord = 7.860 wing_dihedral = 5.000 wing_incidence = 0.000 wing_twist = 0.000 oswald_efficiency_factor = 0.897 wing_winglets_flag = 0 wing_sweep = 0.000 wing_pos_apex_lon = 1.965 wing_pos_apex_vert = 0.000 htail_area = 21.900 htail_span = 12.600 htail_pos_lon =-19.900 htail_pos_vert = 0.000 htail_incidence = 0.000 htail_sweep = 0.000 vtail_area = 13.000 vtail_span = 5.900 vtail_sweep = 0.000 vtail_pos_lon =-20.400 vtail_pos_vert = 0.000 elevator_area = 12.100 aileron_area = 30.000 rudder_area = 10.500 elevator_up_limit = 25.000 elevator_down_limit = 16.000 aileron_up_limit = 29.000 aileron_down_limit = 18.000 rudder_limit = 25.000 elevator_trim_limit = 24.000 spoiler_limit = 75.000 spoilerons_available = 0 aileron_to_spoileron_gain = 0.000 min_ailerons_for_spoilerons = 0.000 min_flaps_for_spoilerons = 0.000 [flight_tuning] cruise_lift_scalar = 0.500 parasite_drag_scalar = 0.850 induced_drag_scalar = 0.500 pitch_stability = 1.800 roll_stability = 1.000 yaw_stability = 1.750 elevator_trim_effectiveness = 1.500 aileron_trim_effectiveness = 6.200 rudder_trim_effectiveness = 3.002 aileron_effectiveness = 1.5 elevator_effectiveness = 1.5 hi_alpha_on_roll = 1 hi_alpha_on_yaw = 1 p_factor_on_yaw = 0 torque_on_roll = 0 gyro_precession_on_roll = 0 gyro_precession_on_yaw = 0 [propeller] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type = 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter = 8.0 //Propeller Diameter, (feet) propeller_blades = 4 //Number of propeller blades propeller_moi = 10.0 //Propeller moment of inertia beta_max = 45 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min = 5.0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm = 25520 //Miminum governed RPM prop_tc = 0.004 //Prop time-constant gear_reduction_ratio = 16.5 //Propeller gear reduction ratio fixed_pitch_beta = 0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit = 80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available = 1 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available = 1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available = 1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available = 1 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather = 700 //Minimum RPM for prop feathering beta_feather = 79.3 //Feathering pitch angle (degrees) power_absorbed_cf = 0.9 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available = 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available = 1 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta = 1.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta =-10.0 //Minimum pitch angle in reverse, (degrees) [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 engine_generator_map = 1 electric_always_available = 0 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 5, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 2, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 [gear_warning_system] gear_warning_available = 2 //Amphib pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 20.1 //Flap angle that activates warning at idle flap_limit_power = 13.0 //Flap angle that activates warning at above idle [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,0,0,0 //pump on Eng1 [Views] eyepoint = -10.3, 0.0, 4.4 //13, 0, 6.4 //(feet) longitudinal, lateral, vertical distance from reference datum [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 [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 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0=1,0 [airspeed_indicators] airspeed_indicator.0 = 1.16, -22.0 [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second [stall_warning] type=2 [keyboard_response] elevator = 100, 180 aileron = 200, 1000 rudder = 200, 1000 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.0 autothrottle_available=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=1.5 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=9.00 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] gear_bump_nose_magnitude = 3000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2700 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2700 gear_bump_right_direction = 00500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1300 ground_bumps_angle1 = 08900 ground_bumps_intercept1 = 3.0 ground_bumps_slope1 = 0.20 ground_bumps_magnitude2 = 200 ground_bumps_angle2 = 09100 ground_bumps_intercept2 = 1.075 ground_bumps_slope2 = 0.035 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000
