[fltsim.0] title=S403 sim=S403 model= panel= sound= texture= kb_checklists= ui_manufacturer=Sai Ambrosini ui_type= S403 ui_variation=Prototype description=Sai Ambrosini S403 "Dardo" (dart)\n Prototype MM 518\n First flight Jan 1943\n For description see file [General] atc_type= atc_model= editable = 1 performance =Weight:Lenth: 8.20m\nWingspan: 9.80 m\nTOW: 2,640 kg\nMax speed : 648 kmh\nCruise speed: 435 Km/h\nEngine:1 Isotta Fraschini Delta RC.40 in line,559 kW(760 cv)\nCeiling: 10,000m\nRange:937 km\n Category=airplane [WEIGHT_AND_BALANCE] empty_weight = 7040 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 max_number_of_stations = 11 station_load.0 = 200, 0, 0, 0, // Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) empty_weight_pitch_MOI = 5833 empty_weight_roll_MOI = 2944 empty_weight_yaw_MOI = 8306 empty_weight_coupled_MOI=0.000 max_gross_weight=8780.00 [flight_tuning] cruise_lift_scalar = 0.5 parasite_drag_scalar =0.77 induced_drag_scalar = 1.5 elevator_effectiveness = 1 aileron_effectiveness =1.6 rudder_effectiveness = 1 pitch_stability =1.4 roll_stability = 1 yaw_stability = 1 elevator_trim_effectiveness =1.1 aileron_trim_effectiveness = 1.4 rudder_trim_effectiveness = 1 [piston_engine] power_scalar = 1 cylinder_displacement = 148.88 compression_ratio = 6 number_of_cylinders = 14 max_rated_rpm = 3000 max_rated_hp = 2100 fuel_metering_type = 1 cooling_type = 1 normalized_starter_torque = 0.07 turbocharged = 1 max_design_mp = 61 min_design_mp = 9 critical_altitude = 5100 emergency_boost_type = 0 emergency_boost_mp_offset = 0 emergency_boost_gain_offset = 0 fuel_air_auto_mixture = 0 auto_ignition = 0 max_rpm_mechanical_efficiency_scalar = 1 idle_rpm_mechanical_efficiency_scalar = 1 max_rpm_friction_scalar = 1 idle_rpm_friction_scalar = 1 [propeller] thrust_scalar =1.3 propeller_type = 0 propeller_diameter = 9 propeller_blades = 3 propeller_moi = 14.1 beta_max = 65 beta_min = 15 min_gov_rpm = 337.5 prop_tc = 0.01 gear_reduction_ratio = 1 fixed_pitch_beta = 30 low_speed_theory_limit = 80 prop_sync_available = 0 prop_deice_available = 1 prop_feathering_available = 0 prop_auto_feathering_available = 0 min_rpm_for_feather = 700 beta_feather = 88.5 power_absorbed_cf = 0.9 defeathering_accumulators_available = 0 prop_reverse_available = 0 minimum_on_ground_beta = 1 minimum_reverse_beta = -14 rotation = 1 [contact_points] //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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) max_number_of_points = 9 point.0 = 1, -10.57, 0, -0.57, 1600, 0, 0.531197, 40.00, 0.551117, 2.5, 0.686607, 5, 5, 0, 0, 0 point.1 = 1, 5.60, -4.34, -3.60, 1600, 1, 0.531197, 0, 0.714684, 2.5, 0.274063, 5, 5, 2, 0, 0 point.2 = 1, 5.60, 4.34, -3.60, 1600, 2, 0.531197, 0, 0.714684, 2.5, 0.274063, 5, 5, 3, 0, 0 point.3 = 2, 2.7, -17.8, 0.71, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 5 point.4 = 2, 2.7, 17.6, 0.71, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 6 point.5 = 2, -15.1, 0, 0.55, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 9 point.6 = 2, 13.10, 0, 1.40, 1600, 0, 0, 0, 0, 0, 0, 0, 0, 4 static_pitch= 12 static_cg_height= 4.90927 gear_system_type=1 [Views] eyepoint=1.35, 0.0, 4.2500 [SMOKESYSTEM] smoke.0=0.00, 0.00, 0.00, fx_smoke_w [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time =10 flaps-position.0=0 flaps-position.1=10 flaps-position.2=15 flaps-position.3=30 flaps-position.4=45 damaging-speed = 126 blowout-speed = 136 [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 light.0=3, 3.70, -17.57, 2.00, fx_navred light.1=3, 3.70, 17.57, 2.00, fx_navgre light.2=4, 2.15, 0.0, 4.20, fx_vclight_s403 [LSO] LSOAdjustSpeed = 1.2 [exits] number_of_exits = 1 exit_rate.0 = 0.4 [fuel] LeftMain=0.00,-2.50,0.00,55.50,0.00 RightMain=0.00,2.50,0.00,55.50,0.00 fuel_type=1.00 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=254.000000 wing_span=42.000000 wing_root_chord=7.500000 wing_dihedral=5.597534 wing_incidence=0.000000 wing_twist=0.000000 oswald_efficiency_factor=0.891323 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=1.510119 wing_pos_apex_vert=0.000000 htail_area=34.000000 htail_span=13.000000 htail_pos_lon=-17.916667 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=19.000000 vtail_span=4.969909 vtail_sweep=0.000000 vtail_pos_lon=-19.500000 vtail_pos_vert=7.250000 elevator_area=26.600000 aileron_area=18.900000 rudder_area=14.900000 elevator_up_limit=28.0 elevator_down_limit=22.00 aileron_up_limit=15.00 aileron_down_limit=15.00 rudder_limit=30.00 elevator_trim_limit=18.0 spoiler_limit=1.00 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 auto_spoiler_available=0 spoiler_extension_time=5.000000 positive_g_limit_flaps_up=7.500000 positive_g_limit_flaps_down=5.000000 negative_g_limit_flaps_up=-6.000000 negative_g_limit_flaps_down=-5.000000 [brakes] toe_brakes_scale=0.63 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=33.750 flap_limit_idle=16.875 [GeneralEngineData] engine_type=0 Engine.0=9.750,0.00,0.00 fuel_flow_scalar=1.00 min_throttle_limit=0.00 [Reference Speeds] flaps_up_stall_speed=73.00 full_flaps_stall_speed=58.40 cruise_speed=270.30 max_indicated_speed=407.00 [keyboard_response] elevator=350.00,500.00 aileron=450.00,1000.00 rudder=200.000,1000.00 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.00 autothrottle_available=0 pitch_takeoff_ga=8.00 max_pitch=10.00 max_pitch_acceleration=1.00 max_pitch_velocity_lo_alt=2.00 max_pitch_velocity_hi_alt=1.50 max_pitch_velocity_lo_alt_breakpoint=20000.00 max_pitch_velocity_hi_alt_breakpoint=28000.00 max_bank=25.000000 max_bank_acceleration=1.80 max_bank_velocity=3.00 max_throttle_rate=0.100 nav_proportional_control=9.00 nav_integrator_control=0.250 nav_derivative_control=0.000 nav_integrator_boundary=2.500 nav_derivative_boundary=0.000 gs_proportional_control=9.5200 gs_integrator_control=0.2600 gs_derivative_control=0.000 gs_integrator_boundary=0.700 gs_derivative_boundary=0.000 yaw_damper_gain=0.000 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=6.930 [stall_warning] type=1 stick_shaker=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0 [pitot_static] vertical_speed_time_constant = 0.5 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=1 electric_backup_pressure=4.900000 engine_map=1,0,0,0 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=0
