Bell 212 Twin Huey

Bell Helicopter · United States · first flew 1969 · helicopter

The Bell 212 is a twin-engine evolution of the UH-1 Huey, retaining the iconic two-blade semi-rigid rotor while adding a coupled PT6T Twin Pac powerplant for improved performance and single-engine safety.

Recognition (WEFT)

W — WingsHigh-mounted, rotary
E — Engines2 × turboshaft, fuselage-mounted
F — Fuselage17.46 m fuselage
T — TailConventional

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Essentially a wider-bodied Huey with a twin-engine cowling under the mast; distinguished from the Bell 412 by its two-blade semi-rigid rotor rather than the 412's four-blade composite system, and from the UH-1 by the broader Twin Pac engine fairing.

Specifications

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

History

Developed in 1968 in response to a Canadian Forces requirement for a twin-engine utility helicopter, the 212 was certificated in 1970 and adopted by the US military as the UH-1N. Civilian variants proved popular in the oil and gas industry worldwide, and licence production continued in Italy as the Agusta-Bell 212.

Variants

The military UH-1N serves the US Navy and Marine Corps; the AB 212 ASW built by Agusta added dipping sonar and torpedoes for the Italian and other navies; the AB 212 naval variant remains in service across the Mediterranean.

Where you'll see it

The RAF operated 212-based types via the Agusta-Bell AB 212; several overseas operators supplied or trained with UK assistance flew the type extensively in the Middle East and North Africa.

Related aircraft

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