[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
//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
[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]
