[fltsim.0] title=Tucano : 207 Sqn RAF sim=Tucano model= panel= sound= texture=207sqn checklists= ui_manufacturer=Shorts ui_type=Tucano(FSDS3) ui_variation=MK.1 207 Sqn RAF description=The Embraer Tucano is one of the world's most successful turbo-prop trainers. Originaly from Brazil the Tucano was manufactured under licence by Shorts of Belfast for the Britsh Royal Air Force. The two seater basic trainer was fitted with an uprated turbo prop engine and stronger airframe. Created by Simshed with FSDS3. Author Brian Franklin (www.simshed.co.uk) atc_airline=RAF atc_id=train atc_flight_number=139 prop_anim_ratio=1.15 atc_heavy=0 [fltsim.1] title=Tucano : 72 Sqn RAF sim=Tucano model= panel= sound= texture=72sqn checklists= ui_manufacturer=Shorts ui_type=Tucano(FSDS3) ui_variation=MK.1 72 Sqn RAF description=The Embraer Tucano is one of the world's most successful turbo-prop trainers. Originaly from Brazil the Tucano was manufactured under licence by Shorts of Belfast for the Britsh Royal Air Force. The two seater basic trainer was fitted with an uprated turbo prop engine and stronger airframe. Created by Simshed with FSDS3. Author Brian Franklin (www.simshed.co.uk) atc_airline=RAF atc_id=train atc_flight_number=203 prop_anim_ratio=1.1 atc_heavy=0 [fltsim.2] title=Tucano : 7FTS RAF sim=Tucano model= panel= sound= texture=7fts checklists= ui_manufacturer=Shorts ui_type=Tucano(FSDS3) ui_variation=MK.1 7FTS RAF description=The Embraer Tucano is one of the world's most successful turbo-prop trainers. Originaly from Brazil the Tucano was manufactured under licence by Shorts of Belfast for the Britsh Royal Air Force. The two seater basic trainer was fitted with an uprated turbo prop engine and stronger airframe. Created by Simshed with FSDS3. Author Brian Franklin (www.simshed.co.uk) atc_airline=RAF atc_id=train atc_flight_number=202 prop_anim_ratio=1.1 atc_heavy=0 [General] atc_type=Tucano 3 atc_model=RAF performance=Max Level Speed : 320 kts \nInitial ROC: 4,000 ft\/min\nMax weight: 7,076lb.\nGarrett TPE331-12B turboprop engine developing 1100 shp. Category=airplane [pitot_static] vertical_speed_time_constant = 2 pitot_heat=1.000000 [WEIGHT_AND_BALANCE] max_gross_weight = 4826.000 empty_weight = 2990.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = 0.000, 0.000, 0.000 CG_forward_limit = 0.000 CG_aft_limit = 1.000 max_number_of_stations = 2 station_load.0 =200.000000, 0.000000, 0.000000, 0.000000, Pilot station_load.1 =0.000000, 0.000000, 0.000000, 0.000000, co-pilot empty_weight_pitch_MOI = 18665.000 empty_weight_roll_MOI = 3623.000 empty_weight_yaw_MOI = 16500.000 empty_weight_coupled_MOI = 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 [GeneralEngineData] engine_type = 5 Engine.0 = 10.235, 0, 0 fuel_flow_scalar = 0.8 min_throttle_limit = -80.00 [TurbineEngineData] fuel_flow_gain = 0.08 inlet_area = 0.1 rated_N2_rpm = 32920 static_thrust = 20 afterburner_available = 0 reverser_available = 1 [turboprop_engine] power_scalar = 1 maximum_torque = 5000 [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) //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) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) [contact_points] // 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 //GEAR point.0=1.00, 8.0, 0.00, -5.75 1574.8, 0.0, 0.551195, 35.0, 0.278, 1.75, 0.90, 4.00, 4.00, 0, 0.0, 0.0 point.1=1.00, -2.48, -6.82, -5.85, 1574.8, 1.0, 0.745050, 0.0, 0.369, 1.55, 0.50, 5.00, 5.00, 2, 0.0, 0.0 point.2=1.00, -2.48, 6.82, -5.85, 1574.8, 2.0, 0.745050, 0.0, 0.369, 1.55, 0.50, 6.00, 6.00, 3, 0.0, 0.0 point.3= 2.000, -1.200, 16.500, 0.000, 1500.000, 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, -1.200, -16.500, 0.000, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.5= 2.000, -1.200, 0.000, -1.800, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.6= 2.000, -16.700, 0.000, -1.100, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.7= 2.000, 9.500, 0.000, -1.000, 1500.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= -2.100 static_cg_height= 5.8 gear_system_type = 1 [Views] eyepoint= 0.8, 0, 2.3 [flaps] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 10, 228 flaps-position.2 = 30, 218 damaging-speed = 240 blowout-speed = 260 system_type = 1 lift_scalar = 1 drag_scalar = 1 pitch_scalar = 0.0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 electric_always_available = 1 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 20, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 starter2 = 0, 20, 17 starter3 = 0, 20, 17 starter4 = 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 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 propeller_deice = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, 1.3, -20.20, 0.1, fx_navred light.1 = 3, 1.3, 20.20, 0.1, fx_navgre light.2 = 2, -1.00, -20.33, -0.0, fx_strobe light.3 = 2, -1.00, 20.33, -0.0, fx_strobe light.4 = 5, +2.1, -10.90, -1.0, fx_navwhih light.5 = 5, +2.1, 10.90, -1.0, fx_navwhih light.6=4, 1.00, 0.0, 1.0, fx_vclighth [Radios] // 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 [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [direction_indicators] direction_indicator.0 = 1, 0 [exits] number_of_exits = 1 exit_rate.0 = 0.4 [EFFECTS] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 [autopilot] autopilot_available = 1 flight_director_available = 0 default_vertical_speed = 1000 autothrottle_available = 0 autothrottle_arming_required = 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga = 1 pitch_takeoff_ga = 8 max_pitch_velocity_hi_alt = 1.5 max_pitch_velocity_lo_alt_breakpoint = 20000 max_pitch_velocity_hi_alt_breakpoint = 28000 max_pitch = 10 max_pitch_acceleration = 1 max_pitch_velocity_lo_alt = 2 max_bank= 60 max_bank_acceleration = 1.8 max_bank_velocity = 3 max_throttle_rate = 0.1 nav_proportional_control = 9 nav_integrator_control = 0.25 nav_derivative_control = 0 nav_integrator_boundary = 2.5 nav_derivative_boundary = 0 gs_proportional_control = 9.52 gs_integrator_control = 0.26 gs_derivative_control = 0 gs_integrator_boundary = 0.7 gs_derivative_boundary = 0 yaw_damper_gain = 0 [fuel] LeftMain = 0.000, -1.100, 0.000, 86.000, 0.000 RightMain = 0.000, 1.100, 0.000, 86.000, 0.000 fuel_type = 2 number_of_tank_selectors = 1 electric_pump=0 [airplane_geometry] wing_area = 225.000 wing_span = 28.625 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 auto_spoiler_available=0 spoiler_extension_time=0.200000 positive_g_limit_flaps_up=5.982906 positive_g_limit_flaps_down=4.807692 negative_g_limit_flaps_up=-3.632479 negative_g_limit_flaps_down=-2.568376 [Reference Speeds] flaps_up_stall_speed = 75.600 full_flaps_stall_speed = 64.300 cruise_speed = 300.000 max_indicated_speed = 370 max_mach = 0.6571 [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 = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 3250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1 crash_magnitude1 = 10000 crash_direction1 = 1000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 stick_shaker_magnitude = 5000 stick_shaker_direction = 0 stick_shaker_period = 111111 [gear_warning_system] gear_warning_available = 1 pct_throttle_limit = 0.1 flap_limit_idle = 33.75 flap_limit_power = 16.875 [brakes] toe_brakes_scale = 1.5 parking_brake=1 parking_brake_scalar = 12 [stall_warning] // 0 = None, 1 = Suction, 2 = Electric. type = 1 stick_shaker=0 [hydraulic_system] electric_pumps = 0 engine_map = 1, 0, 0, 0 normal_pressure = 1250 [attitude_indicators] // 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] // 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0 = 1, 0 [direction_indicators] // 0=None, 1=Vac Gyro, 2=Elec Gyro, 3=EM Slave Compass, 4=Slave to other ind direction_indicator.0 = 1, 0 [airspeed_indicators] airspeed_indicator.0 = 1, 0 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=0.150000 [deice_system] structural_deice_type=2
