[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= visual_damage=0 [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= 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] // ACM V2.0 max_gross_weight = 8250 empty_weight = 1000 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 6000 empty_weight_roll_MOI = 4000 empty_weight_yaw_MOI = 10000 empty_weight_coupled_MOI = 1200 max_number_of_stations = 1 station_load.0 = 0.000000,0.000000,0.000000,0.000000 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing 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 , [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 3 fuel_flow_scalar = 1.000 engine.0 = -0.01, 0, 6.55, engine.1 = -25.67, -0.44, 3.98, min_throttle_limit=0.000000 [smokesystem] smoke.0 = -0.00, -5.00, -4.00, fx_flare smoke.1 = -0.00, -5.00, 4.00, fx_flare [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks startup=fx_engstrt [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 Center1 = 0, 0, 0, 91, 0 electric_pump=0 [contact_points] static_pitch = 0 static_cg_height = 2.896 max_number_of_points = 3 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 gear_system_type=0 [keyboard_response] elevator = 100.000, 180.000 aileron = 200.000, 1000.000 rudder = 200.000, 1000.000 [forcefeedback] 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 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 450 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1 crash_magnitude1 = 2000 crash_direction1 = 1000 crash_magnitude2 = 2000 crash_direction2 = 9000 crash_period2 = 7500 crash_duration2 = 2500000 stick_shaker_magnitude = 2000 stick_shaker_direction = 0 stick_shaker_period = 111111 [airplane_geometry] //ACM_AREAW1// 0,0,0,0,0,0,0,0,0,0 //ACM_AREAW2// 0,0,0,0,0,0,0,0,0,0 //ACM_AREAW3// 0,0,0,0,0,0,0,0,0,0 //ACM_AREAW4// 0,0,0,0,0,0,0,0,0,0 //ACM_AREAH1// 0,0,0,0,0,0,0,0,0,0 //ACM_AREAH2// 0,0,0,0,0,0,0,0,0,0 //ACM_AREAH3// 0,0,0,0,0,0,0,0,0,0 //ACM_AREAH4// 0,0,0,0,0,0,0,0,0,0 //ACM_AREAV1// 0,0,0,0,0,0,0,0,0,0 //ACM_AREAV2// 0,0,0,0,0,0,0,0,0,0 //ACM_AREAV3// 0,0,0,0,0,0,0,0,0,0 //ACM_AREAV4// 0,0,0,0,0,0,0,0,0,0 //ACM_CAREAW1// 0,0,0,0,0,0,0,0,0,0 //ACM_CAREAW2// 0,0,0,0,0,0,0,0,0,0 //ACM_CAREAW3// 0,0,0,0,0,0,0,0,0,0 //ACM_CAREAW4// 0,0,0,0,0,0,0,0,0,0 //ACM_CAREAH1// 0,0,0,0,0,0,0,0,0,0 //ACM_CAREAH2// 0,0,0,0,0,0,0,0,0,0 //ACM_CAREAH3// 0,0,0,0,0,0,0,0,0,0 //ACM_CAREAH4// 0,0,0,0,0,0,0,0,0,0 //ACM_CAREAV1// 0,0,0,0,0,0,0,0,0,0 //ACM_CAREAV2// 0,0,0,0,0,0,0,0,0,0 //ACM_CAREAV3// 0,0,0,0,0,0,0,0,0,0 //ACM_CAREAV4// 0,0,0,0,0,0,0,0,0,0 wing_winglets_flag = 0 spoilerons_available = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 electric_always_available = 1 gear_motor = 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 fuel_pump = 0, 5, 17 starter1 = 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 [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 [Reference Speeds] flaps_up_stall_speed=54.000 full_flaps_stall_speed=43.200 cruise_speed=0.000 max_indicated_speed=190.000000 [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 [brakes] toe_brakes_scale=1.000031 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] normal_pressure=0.000000 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0