[fltsim.0] title=Bell222b sim=Bell222b model= panel= sound= texture= kb_checklists= kb_reference= prop_anim_ratio=-1.76 atc_id_color=0xc6eff7ff atc_id=EIBTD atc_model= ui_manufacturer=Bell ui_type=Bell 222b ui_variation=Blue and Grey description=Bell announced development of the all new 222 twin in 1974, following the positive response generated by a mockup proposal displayed at that year's Helicopter Association of America convention. \n\nHaving taken note of potential customers' preferences and suggestions, Bell modified its design accordingly, and the subsequent development effort led to the Model 222's first flight in August 1976. A number of advanced features were designed into the 222, including the Noda Matic vibration reduction system developed for the 214ST, stub wings housing the retractable undercarriage, provision for IFR avionics, and dual hydraulic and electrical systems. \n\nThe 222 was awarded FAA certification in December 1979. Production deliveries commenced in early 1980. Subsequent development led to the more powerful 222B with a larger diameter main rotor, introduced in 1982, and the essentially similar 222UT Utility Twin, which features skid landing gear in place of wheels. \n\n184 Bell 222s built. atc_heavy=0 atc_airline= atc_flight_number= [General] atc_type=BELL editable=1 performance=Country Of Origin: USA \nDesignation: Executive transport helicopter \nAircraft Crew: Two pilots \nTransport Capacity: Seven passengers (current configuraton, 4 passengers)\n\nAircraft Dimensions: \n Length: 42 ft 2 in (12.8 m) \n Rotor Size: 42 ft (12.8 m) \n Height: 11 ft 6 in (3.5 m) \n\nAircraft Weights: \n Empty: 4,900 lb (2,223 kg) \n Max T\/O: 8,250 lb (3,742 kg) \n\nAircraft Performance: \n Max Speed: 172 mph (278 kmh) \n Range: 373 nm (691 km) \n Powerplant: Two Textron Lycoming LTS \n 101-750C-1 turboshafts \n Power: 1,368 shp (1,020 kW) \n\n\n atc_model=222b [turboprop_engine] power_scalar=50.0 [propeller] thrust_scalar=9.0 propeller_type=1 propeller_diameter=6.883000 propeller_blades=2 propeller_moi=5.706520 beta_max=0.000000 beta_min=15.000000 min_gov_rpm=0.000000 prop_tc=0.100000 gear_reduction_ratio=1.000000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 //Dampers are set to our mormal standards of flight [ground_reaction] //main_gear_static_compression = 5.2 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression = 5.2 // (feet), The distance the center gear strut is compressed when at rest on the ground //main_gear_damping_ratio = 0.7 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped center_gear_damping_ratio = 1.0 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight= 1000.000 empty_weight_roll_MOI= 4000.000 empty_weight_pitch_MOI= 6000.000 empty_weight_yaw_MOI= 10000.000 empty_weight_coupled_MOI= 1200.000 max_gross_weight= 8250.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] Center1= 0.000, 0.000, 0.000, 91.000, 0.000 fuel_type=2.000 number_of_tank_selectors=1 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 gear_motor=0, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 //1 Class <0=none,1=wheel, 2=scrape, 3=skid> //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] point.0= 1.000, 3.000, 0.000, -3.100, 2200.000, 0.000, 0.400, 45.000, 0.500, 0.750, 0.850, 2.000, 2.000, 0.000, 0.000, 0.000 point.1= 1.000, -2.900, -4.110, -3.100, 2200.000, 1.000, 0.500, 0.000, 0.500, 0.750, 0.850, 2.000, 2.000, 0.000, 0.000, 0.000 point.2= 1.000, -2.900, 4.110, -3.100, 2200.000, 2.000, 0.500, 0.000, 0.500, 0.750, 0.850, 2.000, 2.000, 0.000, 0.000, 0.000 static_cg_height = 2.896 static_pitch= 0.000 [Views] eyepoint=6, 1.5, 3 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=0, 0 Nav.1=1, 1, 1 Nav.2=0, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [keyboard_response] elevator=100.000, 180.000 aileron=200.000, 1000.000 rudder=200.000, 1000.000 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, 0.0, -6.20, 0.2, fx_navred , light.1 = 3, 0.0, 6.20, 0.2, fx_navgre , light.2 = 3, -29, 0.4, 1.5, fx_navwhi , light.3 = 1, -2.35, 0.0, 6.46, fx_beacon , light.4 = 2, -13.76, 0.0, 1.98, fx_beacon , light.5 = 4, 6.00, 0.00, 0.00, fx_vclight , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks [GeneralEngineData] engine_type= 3 Engine.0= 5.000, 0.000, 5.300 fuel_flow_scalar=1.000 [Reference Speeds] flaps_up_stall_speed=54.000 full_flaps_stall_speed=43.200 cruise_speed=0.000 [SMOKESYSTEM] smoke.0=-0.00, -5.00, -4.00, fx_flare smoke.1=-0.00, -5.00, 4.00, fx_flare [exits] number_of_exits=2 exit_rate.0=0.8 exit_rate.1=0.8 [autopilot] autopilot_available=0 flight_director_available=0 [direction_indicators] direction_indicator.0=3,0
