Bell 222B

Bell Helicopter · United States · first flew 1982 · helicopter

The Bell 222B is an upgraded variant of the original Bell 222 featuring more powerful Lycoming LTS101-750C-1 engines and an enlarged main rotor, improving hot-and-high performance and range while retaining the distinctive retractable wheeled undercarriage.

Recognition (WEFT)

W — WingsHigh-mounted, rotary
E — Engines2 × turboshaft, fuselage-mounted
F — Fuselage12.85 m fuselage
T — TailConventional

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Distinguished from base 222 by the marginally larger main rotor disc; without a direct comparison this is difficult to assess in the field. Retractable wheeled undercarriage (three legs retracting cleanly into the fuselage) distinguishes both 222 and 222B from the skid-gear 222UT.

Specifications

Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.

History

Bell introduced the 222B in 1982 as a performance-improved successor to the base 222, addressing criticisms of marginal single-engine performance under hot-and-high conditions. The rotor diameter was increased by approximately 0.7 m and the engine output raised from 650 to 680 shp. The 222B became the basis for the 222UT skid-gear variant and was eventually superseded by the Bell 230 with Allison 250-C30 engines.

Variants

222B is the direct variant; 222UT is the skid-gear derivative. Bell 230 is the later successor.

Where you'll see it

Corporate, EMS and utility operators worldwide. Canadian and US helicopter operators were primary customers.

Related aircraft

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