//FS9 FD Files Ver 1.1 16 Oct 09 //Ref 1: Bingo Specs from ICP (www.icp-avio.com) //Ref 2: Engine Specs from HKS Aviation //Ref 3: Bingo 3-view drawing //Ref 4: Various Web pages containing Bingo information [fltsim.0] title = ICP Bingo 4S (Italy) sim = Bingo model = panel = sound = texture= 1 visual_damage= 0 kb_checklists= Bingo_check kb_reference = Bingo_REF atc_heavy = 0 atc_airline = atc_flight_number= atc_id_enable = 1 atc_id = I-8216 atc_parking_types= ramp ui_manufacturer= ICP Italy ui_type = Bingo 4S ui_variation = 1. I-8216 Description=The ICP Bingo, a lightened down Savannah, is one of the top selling ultralights in Europe. It is dependable and easy to fly. It's STOL performance makes it easy to operate from any airfield. The Bingo is also a very good airplane for cross-country flights during which one can appreciate it's great stability. This FS aircraft represents an Italian civil user version.\n\nAircraft design:\nMassimo Taccoli (maxtaccoli@maxtac.it)\nSounds: Mike Hambly\n [fltsim.1] title = ICP Bingo 4S (Spain) sim = Bingo model = panel = sound = texture= 2 visual_damage= 0 kb_checklists= Bingo_check kb_reference = Bingo_REF atc_heavy = 0 atc_airline = atc_flight_number= atc_id_enable = 1 atc_id = EC-EP2 atc_parking_types= ramp ui_manufacturer= ICP Italy ui_type = Bingo 4S ui_variation = 2. EC-EP2 Description=The ICP Bingo,, a lightened down Savannah is one of the top selling ultralights in Europe. It is dependable and easy to fly. It's STOL performance makes it easy to operate from any airfield. The Bingo is also a very good airplane for cross-country flights during which one can appreciate it's great stability. This FS aircraft represents a Spanish civil user version.\n\nAircraft design:\nMassimo Taccoli (maxtaccoli@maxtac.it)\nSounds: Mike Hambly\n [General] Performance=Length: 6.10 m (20.01 ft).\nHeight: 2.45 m (8.04 ft).\nWing Span: 9.00 m (29.53 ft).\nWing Area: 12.86 sq m (138.42 sq ft).\nEngine: HKS 700E 2-cyl 4-stroke air-cooled.\nMax Power: 60 hp at 6,200 RPM at sea level.\nProp: 5.67 ft 3-bladed fixed pitch.\nEmpty Weight: 255 kg (562 lb).\nMTO Weight: 450 kg (992 lb).\nMax Speed: 140 kph (87 mph) at sea level.\nCruise Speed: 120 kph (74.6 mph).\nnStall Speed (clean): 56 kph (35 mph) IAS.\Stall Speed (full flaps): 45 kph (28 mph) IAS.\nInitial Climb Rate: 500 fpm at 80 kph.\nMax Op Altitude: 2,438 m (8,000 ft).\nRange: 880 km (547 mi).\nFuel consumption (cruise): 9 l/h (2.38 gph) at 4,750 RPM. atc_type = ICP atc_model= Bingo 4S editable = 0 [Flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.0 aileron_effectiveness = 1.0 rudder_effectiveness = 1.0 pitch_stability = 1.0 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness= 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 hi_alpha_on_roll = 1.0 hi_alpha_on_yaw = 1.0 p_factor_on_yaw = 1.0 torque_on_roll = 0.3 gyro_precession_on_roll = 0.3 gyro_precession_on_yaw = 0.3 [Weight_and_balance] reference_datum_position= 0.527, 0.0, 1.65 //FS Datum wrt Mdl Datum empty_weight_CG_position= 0.270, 0.0, -1.74 //At C of Lift and on Thrust Line CG_forward_limit= 0.5 CG_aft_limit = -0.5 empty_weight = 562.2 //Ref 1 max_gross_weight= 992.1 //Ref 1 empty_weight_roll_MOI = 222.9 //MOIs calc as per Goodrick empty_weight_pitch_MOI = 275.5 empty_weight_yaw_MOI = 413.6 empty_weight_coupled_MOI= 0.0 max_number_of_stations= 2 station_load.0= 170.0, -1.0, -0.6, -2.5, L Seat //Ref 3 station_load.1= 170.0, -1.0, 0.6, -2.5, R Seat //Ref 3 station_load.2= 0.0, -2.0, 0.0, -2.5, Luggage //Max 44 lb Ref 1 [Fuel] fuel_type = 1 number_of_tank_selectors= 1 electric_pump = 1 LeftMain = 0.0, -3.0, 0.00, 9.51, 0.6 //Ref 1 RightMain= 0.0, 3.0, 0.00, 9.51, 0.6 //Ref 1 Center1 = 2.0, 0.0,-1.73, 1.59, 0.0 //Reserve Ref 1 [Contact_points] static_pitch = -1.0 static_cg_height= 4.1 gear_system_type= 4 //Fixed tailwheel_lock = 0 max_number_of_points= 7 point.0= 1, 3.42, 0.00, -5.700, 1575, 0, 0.6, 33.0, 0.249, 2.514, 0.95, 0.0, 0.0, 0, 0.0, 0.0 point.1= 1, -1.24, -2.95, -5.851, 1575, 1, 0.6, 0.0, 0.390, 1.277, 0.60, 0.0, 0.0, 2, 0.0, 0.0 point.2= 1, -1.24, 2.95, -5.851, 1575, 2, 0.6, 0.0, 0.390, 1.277, 0.60, 0.0, 0.0, 3, 0.0, 0.0 point.3= 2, 0.30, -15.10, 0.400, 1575, 0, 0.0, 0.0, 0.000, 0.000, 0.00, 0.0, 0.0, 5, 0.0, 0.0 point.4= 2, 0.30, 15.10, 0.400, 1575, 0, 0.0, 0.0, 0.000, 0.000, 0.00, 0.0, 0.0, 6, 0.0, 0.0 point.5= 2, -14.50, 0.00, -0.580, 1575, 0, 0.0, 0.0, 0.000, 0.000, 0.00, 0.0, 0.0, 9, 0.0, 0.0 point.6= 2, 5.52, 0.00, -1.750, 1575, 0, 0.0, 0.0, 0.000, 0.000, 0.00, 0.0, 0.0, 4, 0.0, 0.0 [Brakes] parking_brake = 1 auto_brakes = 0 toe_brakes_scale = 0.5 differential_braking_scale= 0.5 [Views] eyepoint= -1.13, -0.6, -0.9 [Airplane_geometry] wing_winglets_flag = 0 spoilerons_available = 0 spoiler_handle_available= 0 auto_spoiler_available = 0 wing_area = 138.420 //Ref 1 wing_span = 29.530 //Ref 2 wing_root_chord = 4.692 //Ref 4 wing_dihedral = 1.000 //ACM wing_incidence = 0.000 //Guess wing_twist = 0.000 //Guess oswald_efficiency_factor = 0.597 //Perfect wing= 1.0 wing_sweep = 0.000 //Ref 3 wing_pos_apex_lon = 1.173 //Defined (1/4-chord fwd of FS Datum) wing_pos_apex_vert = 0.000 //Defined htail_area = 19.270 //ACM htail_span = 7.750 //ACM htail_pos_lon = -11.180 //ACM htail_pos_vert = 0.000 //ACM htail_incidence = 0.000 //Guess htail_sweep = 0.000 //Ref 3 vtail_area = 12.960 //ACM vtail_span = 3.210 //ACM vtail_sweep = 40.400 //ACM vtail_pos_lon = -11.180 //ACM vtail_pos_vert = -0.220 //ACM elevator_area = 10.910 //ACM aileron_area = 10.010 //ACM rudder_area = 5.940 //ACM elevator_up_limit = 24.000 //No info on actual values elevator_down_limit = 18.000 //Set to values for similar aircraft aileron_up_limit = 21.000 aileron_down_limit = 15.000 rudder_limit = 30.000 elevator_trim_limit = 60.000 spoiler_limit = 0.000 spoiler_extension_time = 0.000 aileron_to_spoileron_gain = 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons = 0.000 [Flaps.0] type = 1 system_type = 3 lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar = 1.0 span-outboard = 1.0 extending-time= 2.0 damaging-speed= 54.7 blowout-speed = 62.6 flaps-position.0= 0.0 //Ref 1 flaps-position.1= 20.0, 52.0 //Ref 1 flaps-position.2= 40.0, 52.0 //Ref 1 [GeneralEngineData] engine_type = 0 fuel_flow_scalar = 0.71 //Set for 2.64 gph at 75% power min_throttle_limit= 0.00 engine.0= 5.1, 0.0, -1.74 //ACM [Piston_engine] power_scalar = 1.0 max_rpm_mechanical_efficiency_scalar = 1.0 idle_rpm_mechanical_efficiency_scalar= 1.0 max_rpm_friction_scalar = 1.0 idle_rpm_friction_scalar = 1.0 fuel_metering_type = 1 //Ref 2 cooling_type = 0 //Ref 2 turbocharged = 0 emergency_boost_type = 0 fuel_air_auto_mixture = 0 auto_ignition = 0 number_of_cylinders = 2 //Ref 2 cylinder_displacement = 20.75 //Ref 2 compression_ratio = 11.30 //Ref 2 max_rated_rpm = 6200.00 //Ref 2 max_rated_hp = 60.00 //Ref 2 normalized_starter_torque = 0.35 max_design_mp = 0.00 min_design_mp = 3.00 critical_altitude = 0.00 emergency_boost_mp_offset = 0.00 emergency_boost_gain_offset = 0.00 emergency_boost_duration = 0.00 BestPowerSpecificFuelConsumption = 0.50 detonation_onset = 32.91 [Propeller] thrust_scalar = 1.0 rotation = 1 propeller_type = 1 prop_sync_available = 0 prop_deice_available = 0 prop_feathering_available = 0 prop_auto_feathering_available = 0 defeathering_accumulators_available= 0 prop_reverse_available = 0 propeller_blades = 3 propeller_diameter = 5.67 //Ref 4 propeller_moi = 3.65 beta_max = 0.00 beta_min = 0.00 fixed_pitch_beta = 23.00 beta_feather = 0.00 minimum_on_ground_beta = 0.00 minimum_reverse_beta = 0.00 min_gov_rpm = 0.00 prop_tc = 0.10 gear_reduction_ratio = 2.58 //Ref 2 low_speed_theory_limit = 80.00 min_rpm_for_feather = 0.00 power_absorbed_cf = 0.00 [Electrical] engine_generator_map = 1,0,0,0 electric_always_available = 0 max_battery_voltage = 12.0 //Ref 3 generator_alternator_voltage = 13.5 //Ref 3 max_generator_alternator_amps= 18.5 //Ref 3 additional_system= 0, 5.0, 10.0 autopilot = 0, 5.0, 10.0 avionics_bus = 0, 5.0, 10.0 avionics = 1, 2.0, 10.0 flap_motor = 0, 5.0, 10.0 fuel_pump = 0, 5.0, 10.0 light_nav = 0, 5.0, 10.0 light_beacon = 0, 2.0, 10.0 light_landing = 0, 2.0, 10.0 light_taxi = 0, 2.0, 10.0 light_strobe = 0, 2.0, 10.0 light_panel = 0, 2.0, 10.0 marker_beacon = 1, 2.0, 10.0 pitot_heat = 0, 2.0, 10.0 starter1 = 0, 20.0, 10.0 [Lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0= 3, -0.1, -15.12, 0.6, fx_navred light.1= 3, -0.1, 15.12, 0.6, fx_navgre light.2= 3, -13.2, 0.00, 3.0, fx_navwhi light.3= 4, 0.4, 0.00, -1.5, fx_vclight [Radios] Audio.1 = 0 Com.1 = 1, 0 Com.2 = 0, 0 Nav.1 = 0, 0, 0 Nav.2 = 0, 0, 0 Adf.1 = 0, 0 Transponder.1= 0 Marker.1 = 0 [Hydraulic_system] normal_pressure= 0.0 [Effects] windshield_rain_effect_available= 1 wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown= fx_tchdwn_s, 1 startup = fx_engstrt_cub, 1 [Smokesystem] smoke.0= -3.36, 3.17, -0.84, fx_SmokeStack [Exits] number_of_exits= 2 exit_rate.0 = 0.5 ;Percent per second exit_rate.1 = 0.5 ;Percent per second [Gear_warning_system] gear_warning_available = 0 pct_throttle_limit = 0.0 flap_limit_idle = 0.0 flap_limit_power = 0.0 [Stall_warning] type = 1 stick_shaker= 1 [Pitot_static] vertical_speed_time_constant= 2.0 [Airspeed_indicators] airspeed_indicator.0= 1,0 [Altimeters] altimeter.0= 1 [Attitude_indicators] attitude_indicator.0= 1 [Direction_indicators] direction_indicator.0= 1,0 [Turn_indicators] turn_indicator.0= 1,0 [Autopilot] autopilot_available = 1 flight_director_available = 1 default_pitch_mode = 0 default_bank_mode = 0 autothrottle_available = 1 autothrottle_arming_required= 0 autothrottle_takeoff_ga = 1.0 autothrottle_max_rpm = 6200.0 max_throttle_rate = 0.1 default_vertical_speed = 500.0 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 = 3.0 nav_proportional_control = 9.0 nav_integrator_control = 0.25 nav_derivative_control = 0.0 nav_integrator_boundary = 2.5 nav_derivative_boundary = 0.0 gs_proportional_control = 9.52 gs_integrator_control = 0.26 gs_derivative_control = 0.0 gs_integrator_boundary = 0.7 gs_derivative_boundary = 0.0 yaw_damper_gain = 0.0 [Forcefeedback] stick_shaker_magnitude = 5000 //0 - 10000 stick_shaker_direction = 0 //0 - 35999 degrees stick_shaker_period = 111111 //in microseconds ground_bumps_magnitude1 = 3250 //0 - 10000 ground_bumps_angle1 = 8900 //0 - 35999 degrees ground_bumps_intercept1 = 5.00 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 //0 - 10000 ground_bumps_angle2 = 9100 //0 - 35999 degrees ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1.000 crash_magnitude1 = 10000 //0 - 10000 crash_direction1 = 1000 //0 - 35999 degrees crash_magnitude2 = 10000 //0 - 10000 crash_direction2 = 9000 //0 - 35999 degrees crash_period2 = 75000 //in microseconds crash_duration2 =2500000 //in microseconds [Keyboard_response] elevator= 150.0, 250.0 aileron = 150.0, 250.0 rudder = 150.0, 250.0 [Reference Speeds] full_flaps_stall_speed= 24.3 //Ref 1 flaps_up_stall_speed = 30.4 //Ref 1 cruise_speed = 64.8 //Ref 1 max_indicated_speed = 97.1 //(Vne) Ref 1
