[fltsim.0] title =FN-333 sim = FN-333 model = panel = sound = texture = panel_alias = sound_alias = kb_checklists = FN333_check kb_reference = FN333_Ref atc_id = N95DR atc_id_color = atc_parking_types = atc_parking_code = atc_airline= atc_flight_number= ui_manufacturer = Nardi ui_type = FN-333 Riviera ui_variation = N95DR description = www.mariopilot.6x.to\n\nThe classy looking Riviera amphibian is "Seabee" in Italian style... Built by Nardi and Siai-Marchetti, supposedly only 23 were built during the early 1960ies by Siai-Marcheti, the majority of them being sold to America. As every italian design, it is built to go fast. It seats 4 people including the pilot, the reversible propeller gives it superb manouverability in water (and taxi). It is a high-wing anphibian aircraft with double tailfin and pusher propeller.\nRead notes before flying! visual_damage = 1 [General] atc_type = Nardi atc_model = FN333 performance = ***BASED ON REAL DATA***\n\nEmpty Weight: 2137 lbs\nPowerplant: 250 Hp Continental IO-470P\nManeuver speed: 127 KIAS\nMax speed @SL: 154 KIAS\nVNe: 178 KIAS\nStall Speed (Clean):50 KIAS\nStall Speed (flaps):40 KIAS\nClimb rate: 1300 ft/min @ 96 KIAS\nPropeller: Hartzell HCA3X20-5L/L8433-6B\nFlight Dynamics By: Mario Noriega Designs Based on Jerry Beckwith's Flight Dynamics Workbook V2005.12 editable = 1 prop_anim_ratio = 1 Category=airplane [pitot_static] vertical_speed_time_constant = 2 pitot_heat=1.000000 [WEIGHT_AND_BALANCE] max_gross_weight = 3270 empty_weight = 2137 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 13 station_load.0 = 117, 4.02, -1.01, -0.36, "Pilot" station_load.1 = 103, 4.02, 1.01, -0.36, "Copilot" station_load.2 = 0, 1.158, -0.869, -0.36, "Passenger 1" station_load.3 = 0, 1.158, 0.869, -0.36, "Passenger 2" station_load.4 = 175, -0.34, 0, -1.44, "Baggage - Max 300 lb" empty_weight_pitch_MOI = 5441 empty_weight_roll_MOI = 1000 empty_weight_yaw_MOI = 2138 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1 elevator_effectiveness = 1 aileron_effectiveness = 1 rudder_effectiveness = 1 pitch_stability = 1 roll_stability = 1 yaw_stability = 1 elevator_trim_effectiveness = 1 aileron_trim_effectiveness = 0 rudder_trim_effectiveness = 0 hi_alpha_on_roll = 1 hi_alpha_on_yaw = 1 p_factor_on_yaw = 1 torque_on_roll = 1 gyro_precession_on_roll = 1 gyro_precession_on_yaw = 1 [GeneralEngineData] engine_type = 0 Engine.0 = -6.33, 0, 1.81 fuel_flow_scalar = 1 min_throttle_limit = -0.25 [piston_engine] power_scalar = 1 cylinder_displacement = 78.3333333333333 compression_ratio = 7.3 number_of_cylinders = 6 max_rated_rpm = 2600 max_rated_hp = 250 fuel_metering_type = 2 cooling_type = 0 normalized_starter_torque = 0.311 turbocharged = 0 max_design_mp = 61 min_design_mp = 9 critical_altitude = 5000 emergency_boost_type = 0 emergency_boost_mp_offset = 0 emergency_boost_gain_offset = 0 fuel_air_auto_mixture = 0 auto_ignition = 0 emergency_boost_duration = 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 propeller_type = 0 propeller_diameter = 6.5 propeller_blades = 3 propeller_moi = 2.5 beta_max = 65 beta_min = 15 min_gov_rpm = 1200 prop_tc = 0.01 gear_reduction_ratio = 1.0 fixed_pitch_beta = 15 low_speed_theory_limit = 80 prop_sync_available = 0 prop_deice_available = 1 prop_feathering_available = 1 prop_auto_feathering_available = 0 min_rpm_for_feather = 700 beta_feather = 88.5 power_absorbed_cf = 0.9 defeathering_accumulators_available = 1 prop_reverse_available = 1 minimum_on_ground_beta = 15 minimum_reverse_beta =10.0 rotation = -1 [folding_wings] wing_fold_system_type = 0 fold_rates = 0.12, 0.11 [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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal //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 = 17 point.0 = 1, 7.46, 0, -4.67, 1500, 0, 0.5, 22, 0.45, 2.0, 0.7, 3.9, 4.1, 0, 101.2, 110 //nose gear point.1 = 1, -1.44, -3.08, -4.77, 3500, 1, 0.7, 0, 0.6, 1.5, 0.7, 4.0, 3.9, 2, 101.2, 110 //left gear point.2 = 1, -1.44, 3.08, -4.77, 3500, 2, 0.7, 0, 0.6, 1.5, 0.7, 4.1, 4.0, 3, 101.2, 110 //right gear point.3 = 2, 7.46, 0, -1.25, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 5 //nose impact point point.4 = 2, -14.73, 4.4, 6.3, 950, 0, 0, 0, 0, 0, 0, 0, 0, 9 //rudders point point.5 = 2, -14.73, -4.4, 6.3, 950, 0, 0, 0, 0, 0, 0, 0, 0, 9 point.6 = 2, 1.515, 16.96, 2.59, 1550, 0, 0, 0, 0, 0, 0, 0, 0, 5 //right wing point.7 = 2, 1.515, -16.96, 2.59, 1550, 0, 0, 0, 0, 0, 0, 0, 0, 5 //left wing point.8 = 4, 5.25, -0.810, -3.40, 1600, 0, 0.00, 0.0, 0.65, 2.5, 0.85, 0, 0, 4, 0, 0 //hull point.9 = 4, 5.25, 0.810, -3.40, 1600, 0, 0.00, 0.0, 0.65, 2.5, 0.85, 0, 0, 4, 0, 0 point.10 = 4, -8.00, -0.810, -3.10, 1600, 0, 0.00, 0.0, 0.65, 2.5, 0.85, 0, 0, 4, 0, 0 point.11 = 4, -8.00, 0.810, -3.10, 1600, 0, 0.00, 0.0, 0.65, 2.5, 0.85, 0, 0, 4, 0, 0 point.12= 5, -12.21, 0.00, -3.10, 1600, 0, 0.00, 25.0, 0.0, 0.0, 1.00, 1.1, 1.5, 4, 0, 0 //water rudder point.13= 4, -0.4,-13.15, -1.78, 1500, 0, 0.0, 0, 0.50, 1.5, 0.70, 2.0, 2.0, 4, 0, 0 //FS-X only wing floats point.14= 4, -0.4, 13.15, -1.78, 1500, 0, 0.0, 0, 0.50, 1.5, 0.70, 2.0, 2.0, 4, 0, 0 static_pitch= 0 static_cg_height= 4.67 gear_system_type = 1 [Views] eyepoint= 4.101, -0.99, 0.85 [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 3 flaps-position.0 = 0 flaps-position.1 = 11, 124 flaps-position.2 = 22, 119 flaps-position.3 = 33, 114 flaps-position.4 = 45, 108 damaging-speed = 109 blowout-speed = 115 system_type = 1 lift_scalar = 1 drag_scalar = 1 pitch_scalar = 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 260 electric_always_available = 0 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, -0.99, -17.01, 2.47, fx_FN333_navred light.1 = 3, -0.99, 17.01, 2.47, fx_FN333_navgre light.2 = 1, -0.91, 0, 3.00, fx_FN333_beacon light.3 = 2, -15.11, -4.43, 1.79, fx_FN333_NAVWHI light.4 = 5, 1.02, 13.87, 2.45, fx_fn333_ll //landing lights effect light.5 = 5, 1.02, -13.87, 2.45, fx_fn333_ll light.6 = 4, 1.868, 0, 1.560, FX_FN333_vclight //Dome light [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 startup = FX_FN333_startup [autopilot] autopilot_available = 0 [fuel] LeftMain = -1.45, -2.64, 2.06, 18.5, 0 RightMain = -1.45, 2.64, 2.06, 18.5, 0 LeftAux = -1.45, -7.07, 2.06, 14, 0 RightAux = -1.45, 7.07, 2.06, 14, 0 fuel_type = 1 number_of_tank_selectors = 1 electric_pump=1 [airplane_geometry] wing_area = 326 wing_span = 34 wing_root_chord = 9.58823529411765 wing_dihedral = 2.5 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.893242859625604 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 2.39705882352941 wing_pos_apex_vert = 0 htail_area = 15.7 htail_span = 8.37 htail_pos_lon = -13.6 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 28.9 vtail_span = 4.43 vtail_sweep = 0 vtail_pos_lon = -13.7 vtail_pos_vert = 0 elevator_area = 10.7 aileron_area = 11.4 rudder_area = 8.78 elevator_up_limit = 25 elevator_down_limit = 20 aileron_up_limit = 25 aileron_down_limit = 18 rudder_limit = 20 elevator_trim_limit = 23 spoiler_limit = 90 spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 auto_spoiler_available=0 spoiler_extension_time=5.000000 positive_g_limit_flaps_up=3.500000 positive_g_limit_flaps_down=3.000000 negative_g_limit_flaps_up=-3.000000 negative_g_limit_flaps_down=-2.000000 [Reference Speeds] flaps_up_stall_speed = 50.4 full_flaps_stall_speed = 40.8 cruise_speed = 141 max_indicated_speed = 179 max_mach = 0.2707 [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 = 0 pct_throttle_limit = 0.1 flap_limit_idle = 33.75 flap_limit_power = 16.875 [brakes] toe_brakes_scale = 0.640888698995941 parking_brake = 1 [stall_warning] // 0 = None, 1 = Suction, 2 = Electric. type = 1 stick_shaker=1 [hydraulic_system] electric_pumps = 0 engine_map = 1, 0, 0, 0 normal_pressure = 1000 [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 = 2, 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=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=2