| Bell 222 - Twin Engine Helicopter Services Provider in Asia and Middle East | • Bell 222 | ||||||
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Type Twin engine light utility helicopter. General Information Bell announced development of the all new 222 twin in the year 1974, following the encouraging response generated by a conjure up proposal displayed at that year’s Helicopter Association of America convention. Having taken note of potential clientele preferences and suggestions. Bell customized its design accordingly, and the successive development effort led to the Model 222’s first flight in August 1976. A number of advance features were designed in to 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. The 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 2222UT Utility Twin, which feature skid landing gear in place of wheels. Capacity Standard sealing for eight, including pilot, in four rows. Alternatively four in main cabin in club configuration. |
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