//Be-200ChS FS9 FD Files Ver 1.2 ( Modificati il 25 Jan 2010 ) Ref 1: Jane's All The World's Aircraft 2002-2003 Ed Ref 2: Be-200 3-view drawing Ref 3: Various Internet sites [fltsim.0] title = Beriev Be-200 sim = be200 model = panel = sound = texture= visual_damage= 0 kb_checklists= kb_reference = atc_heavy = 0 atc_airline = atc_flight_number= 0001 atc_id = 32767 ui_manufacturer= Beriev ui_type = Be-200ChS ui_variation = Russian Emergencies Ministry (MChS) firefighting version Description=The Be-200 is a versatile amphibious platform easily configured for a variety of missions including fire fighting, search and rescue, maritime patrol, cargo and passenger transportation. The prototype's first flight was on September 24, 1998. On July 31, 2003 the first serial aircraft was delivered to Russia's EMERCOM, which will take delivery of seven Be-200 in fire-fighting and rescue variants. [fltsim.1] title = Beriev Be-200 SARV sim = be200 model = panel = sound = texture=SARV visual_damage= 0 kb_checklists= kb_reference = atc_heavy = 0 atc_airline = atc_flight_number= 0002 atc_id = I-EMSC ui_manufacturer= Beriev ui_type = Be-200ChS ui_variation = SAR Virtual Antincendio Description=The Be-200 is a versatile amphibious platform easily configured for a variety of missions including fire fighting, search and rescue, maritime patrol, cargo and passenger transportation. The prototype's first flight was on September 24, 1998. On July 31, 2003 the first serial aircraft was delivered to Russia's EMERCOM, which will take delivery of seven Be-200 in fire-fighting and rescue variants. [General] Performance=Length: 103 ft 1.5 in.\nHeight: 29 ft 2.5 in.\nWing Span: 107 ft 6.5 in.\nWing Area: 1,264.2 sq ft.\nEngines: Two ZMKB Progress D436TP turbofans.\nPower: 16,550 lbst at sea level.\nEmpty Weight: 60,847 lb.\nMTO Weight: 82,011 lb.\nMax Landing Weight: 77,160 lb.\nMax Water capacity: 26,455 lb.\nMax Cruise Speed: 435 mph at 9,840 ft.\nEconomical Cruise Speed: 373 mph at 9,840 ft.\nStall Speed (clean): 134 mph IAS.\nInitial Climb Rate: 2,755 fpm at sea level.\nService Ceiling: 26,240 ft.\nMax Fuel Range: 2,392 mi. atc_type = Beriev atc_model= Be-200 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 elevator_trim_effectiveness= 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 pitch_stability = 1.0 roll_stability = 1.0 yaw_stability = 1.0 hi_alpha_on_roll = 1.0 //At high AoA hi_alpha_on_yaw = 1.0 //At high AoA p_factor_on_yaw = 0.0 //Prop induced torque_on_roll = 0.0 //Prop induced gyro_precession_on_roll = 0.0 //Prop induced gyro_precession_on_yaw = 0.0 //Prop induced [Weight_and_balance] reference_datum_position= 2.10, 0.0, 2.0 //FS Datum wrt Mdl Datum empty_weight_CG_position= -7.48, 0.0, 0.0 //At C of Lift CG_forward_limit= 1.0 CG_aft_limit = -1.0 empty_weight = 60847.0 //Ref 3 max_gross_weight= 94800.0 //Ref 1 (after water scooping) empty_weight_roll_MOI = 323108.0 //MOIs calc as per Goodrick empty_weight_pitch_MOI = 683395.0 empty_weight_yaw_MOI = 1031164.0 empty_weight_coupled_MOI= 0.0 max_number_of_stations= 3 station_load.0= 170.0, 31.0, 1.0, -4.8, Pilot station_load.1= 170.0, 31.0, -1.0, -4.8, Co-pilot station_load.2= 0.0, 0.0, 0.0, 0.0, Payload [Fuel] fuel_type = 2 number_of_tank_selectors= 2 electric_pump = 1 Center1 = -7.3, 0.0, 0.0, 539.6, 3.0 //Max fuel wgt 27,025 lb - Ref 1 LeftMain = -7.3, -14.0, -0.6, 1747.0, 3.0 RightMain= -7.3, 14.0, -0.6, 1747.0, 3.0 [Contact_points] static_pitch = -1.5 static_cg_height= 14.5 gear_system_type= 1 tailwheel_lock = 0 max_number_of_points= 14 //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 //________0_____1_______2______3______4____5___6_____7_____8_____9____10_____11____12___13___14____15 //wheels corrected value point.0 = 1, 25.49, 0.00, -15.73, 2200, 0, 1.10, 45.0, 0.525, 2.00, 0.90, 10.0, 10.0, 0, 220.0, 270.0 point.1 = 1, -12.45, -7.47, -16.80, 2200, 1, 1.68, 0.0, 1.397, 1.25, 0.90, 11.0, 15.0, 2, 220.0, 270.0 point.2 = 1, -12.45, 7.47, -16.80, 2000, 2, 1.68, 0.0, 1.397, 1.25, 0.90, 11.0, 15.0, 3, 220.0, 270.0 //float point.3 = 4, -32.50, 3.00, -9.10, 3000, 0, 0.00, 0.0, 0.95, 2.50, 0.65, 0.0, 0.0, 1, 0.0, 0.0 point.4 = 4, -32.50, -3.00, -9.10, 3000, 0, 0.00, 0.0, 0.95, 2.50, 0.65, 0.0, 0.0, 1, 0.0, 0.0 point.5 = 4, 38.00, 3.00, -11.30, 3000, 0, 0.00, 0.0, 0.95, 2.50, 0.65, 0.0, 0.0, 1, 0.0, 0.0 point.6 = 4, 38.00, -3.00, -11.30, 3000, 0, 0.00, 0.0, 0.95, 2.50, 0.65, 0.0, 0.0, 1, 0.0, 0.0 point.7 = 4, -15.05, -41.85, -6.35, 3000, 0, 0.00, 0.0, 0.95, 2.50, 0.65, 0.0, 0.0, 1, 0.0, 0.0 point.8 = 4, -15.05, 41.85, -6.35, 3000, 0, 0.00, 0.0, 0.95, 2.50, 0.65, 0.0, 0.0, 1, 0.0, 0.0 //water rudder point.9 = 5, -51.54, 0.00, -7.84, 1800, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.5, 0.5, 1, 0.0, 0.0 //scrape point.10= 2, -21.55, -53.62, -0.50, 1800, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.0, 0.0, 5, 0.0, 0.0 point.11= 2, -21.55, 53.62, -0.50, 1800, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.0, 0.0, 6, 0.0, 0.0 point.12= 2, -61.80, 0.00, 15.40, 1800, 0, 0.00, 0.0, 0.00, 0.00 0.00, 0.0, 0.0, 9, 0.0, 0.0 point.13= 2, 41.45, 0.00, -7.30, 1800, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.0, 0.0, 4, 0.0, 0.0 [Brakes] parking_brake = 1 toe_brakes_scale = 1.0 differential_braking_scale= 1.0 [Views] eyepoint= 33.3, -1.8, -3.2 //ACM [Airplane_geometry] wing_winglets_flag = 1 spoilerons_available = 0 spoiler_handle_available= 1 wing_area = 1264.20 //Ref 1 wing_span = 107.54 //Ref 1 wing_root_chord = 19.75 //Ref 2 wing_dihedral = 0.00 //Ref 2 wing_incidence = 1.30 // wing_twist = -1.30 // oswald_efficiency_factor = 0.88 //1.0 for theoretical perfect wing wing_sweep = 23.22 //Ref 1 wing_pos_apex_lon = 4.92 //Ref 2 wing_pos_apex_vert = 0.00 //On FS Datum htail_area = 268.25 //Ref 1 htail_span = 33.19 //Ref 1 htail_pos_lon = -47.92 //Ref 2 htail_pos_vert = 13.67 //Ref 2 htail_incidence = 0.00 // htail_sweep = 25.10 //Ref 2 vtail_area = 185.15 //Ref 1 vtail_span = 15.50 //Ref 2 vtail_sweep = 28.00 //Ref 2 vtail_pos_lon = -40.17 //Ref 2 vtail_pos_vert = 0.00 //Ref 2 elevator_area = 74.92 //Ref 1 aileron_area = 38.32 //Ref 1 rudder_area = 49.52 //Ref 1 elevator_up_limit = 30.00 elevator_down_limit = 24.00 aileron_up_limit = 27.00 aileron_down_limit = 24.00 rudder_limit = 24.00 elevator_trim_limit = 22.00 spoiler_limit = 90.00 aileron_to_spoileron_gain = 0.00 min_ailerons_for_spoilerons= 0.00 min_flaps_for_spoilerons = 0.00 [Flaps.0] type = 1 //Outboard Trailing Edge Flaps system_type = 1 lift_scalar = 1.00 drag_scalar = 1.00 pitch_scalar = 1.00 span-outboard = 0.35 //Ref 2 extending-time= 20.00 damaging-speed= 250.00 blowout-speed = 300.00 flaps-position.0= 0.0 flaps-position.1= 10.0, 250.0 flaps-position.2= 15.0, 250.0 flaps-position.3= 20.0, 250.0 flaps-position.4= 40.0, 250.0 [Flaps.1] type = 1 //Inboard Trailing Edge Flaps system_type = 1 lift_scalar = 1.00 drag_scalar = 1.00 pitch_scalar = 1.00 span-outboard = 0.23 //Ref 2 extending-time= 20.00 damaging-speed= 250.00 blowout-speed = 300.00 flaps-position.0= 0.0 flaps-position.1= 10.0, 250.0 flaps-position.2= 15.0, 250.0 flaps-position.3= 20.0, 250.0 flaps-position.4= 40.0, 250.0 [Flaps.2] type = 2 //Leading Edge Slats system_type = 1 lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar = 1.0 span-outboard = 0.8 //Ref 2 extending-time= 10.0 damaging-speed= 250.0 blowout-speed = 300.0 flaps-position.0= 0.0 flaps-position.1= 18.0, 250.0 flaps-position.2= 22.0, 250.0 flaps-position.3= 22.0, 250.0 flaps-position.4= 22.0, 250.0 [GeneralEngineData] engine_type = 1 fuel_flow_scalar = 0.60 min_throttle_limit= -0.25 engine.0= -27.1, -8.0, 3.75 //Ref 2 engine.1= -27.1, 8.0, 3.75 //Ref 2 [Jet_engine] thrust_scalar= 1.0 [TurbineEngineData] afterburner_available= 0 reverser_available = 1 fuel_flow_gain = 0.003 inlet_area = 18.500 rated_N2_rpm = 29920.000 static_thrust = 16550.000 //Ref 1 [Electrical] electric_always_available = 0 engine_generator_map = 1,1,0,0 max_battery_voltage = 24.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps= 200.0 additional_system = 0, 20, 17 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 directional_gyro = 0, 5, 17 fuel_pump = 0, 5, 17 fuel_transfer_pump= 0, 5, 17 gear_warning = 0, 2, 17 hydraulic_pump = 0, 2, 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 marker_beacon = 1, 2, 17 pitot_heat = 0, 2, 17 starter1 = 0, 20, 17 starter2 = 0, 20, 17 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -17.81, -52.56, -0.50, fx_navredm light.1 = 3, -17.81, 52.56, -0.50, fx_navgrem light.2 = 3, -54.60, 0.00, -0.94, fx_navwhi light.3 = 2, -18.10, -52.78, -0.50, fx_strobeh light.4 = 2, -18.10, 52.78, -0.50, fx_strobeh light.5 = 1, -51.90, 0.00, 16.34, fx_beacon light.6 = 4, 34.30, 0.00, -4.20, fx_vclighth light.7 = 4, 33.25, 0.00, -2.57, fx_vclighth light.8 = 5, -9.75, 23.62, -1.73, fx_landing light.9 = 5, -9.75, -23.62, -1.73, fx_landing [Radios] 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 [Hydraulic_system] electric_pumps = 0 engine_map = 1,1,0,0 normal_pressure= 3000.0 //Ref 1 [Effects] windshield_rain_effect_available= 1 wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown= fx_tchdwn_s, 1 [Smokesystem] // effetto scarico acqua smoke.0= -11.96, -17.5, 3.01, fx_water_dump //Vert, Fore-aft, Lat smoke.1= -11.96, -17.5, -3.01, fx_water_dump smoke.2= -12.53, -2.9, 3.01, fx_water_dump smoke.3= -12.53, -2.9, -3.01, fx_water_dump [Exits] number_of_exits= 2 exit_rate.0 = 0.3 exit_rate.1 = 0.5 [TailHook] cable_force_adjust= 1.0 //used for water drop system tailhook_length = 5.0 tailhook_position = -42.5, 0.0, -9.2 [Folding_wings] wing_fold_system_type= 4 //used for folding landing lights fold_rates = 0.08, 0.09 [Gear_warning_system] gear_warning_available= 2 pct_throttle_limit = 0.1 flap_limit_power = 20.1 flap_limit_idle = 13.0 [Stall_warning] type= 1 [Pitot_static] vertical_speed_time_constant= 1.0 //Increasing value causes more // instantaneous VSI reaction [Attitude_indicators] attitude_indicator.0= 1 [Direction_indicators] direction_indicator.0= 3,0 [Turn_indicators] turn_indicator.0= 1,0 [autopilot] // variazioni rispetto aircraft.cfg originale autopilot_available = 1 flight_director_available = 1 default_vertical_speed = 1800.0 autothrottle_available = 1 autothrottle_arming_required = 1 autothrottle_max_rpm = 90 // era 100 autothrottle_takeoff_ga = 0 // era 1 max_throttle_rate =0.10 pitch_takeoff_ga = 8; 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 nav_proportional_control =11.00 //era9.0 nav_integrator_control =0.20 //era 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 = 1.0 [Forcefeedback] stick_shaker_magnitude = 2000 stick_shaker_direction = 0 stick_shaker_period = 111111 gear_bump_nose_magnitude = 1000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2000 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude= 2000 gear_bump_right_direction= 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5.0 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 450 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1.0 crash_magnitude1 = 2000 crash_direction1 = 1000 crash_magnitude2 = 2000 crash_direction2 = 9000 crash_period2 = 7500 crash_duration2 = 2500000 [Keyboard_response] elevator= 150.0, 250.0 aileron = 150.0, 500.0 rudder = 150.0, 500.0 [Reference Speeds] full_flaps_stall_speed= 84.00 //(KTAS) Ref 1 flaps_up_stall_speed = 116.00 //(KTAS) Ref 1 cruise_speed = 383.00 //(KTAS) Ref 1 max_indicated_speed = 350.00 //(KIAS) Ref 1 max_mach = 0.69 //Ref 1