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Bell 214

Lighter-Than-Air Craft and Rotorcraft

The Bell 214 is a medium-lift helicopter derived from Bell Helicopter's UH-1 Huey series, announced in 1970 as the Huey Plus. Its first prototype used a Bell 205 airframe with a 1,900 shp Lycoming engine, and the Bell 214A that followed was evaluated by the Imperial Iranian Armed Forces, who ordered 287 aircraft. Bell delivered 296 Bell 214A and 39 Bell 214C helicopters before the Iranian Revolution of 1979 ended plans for Iranian production, and Bell then turned the type toward the civilian market. A single Lycoming LTC4B-8 engine of 2,930 shp and an upgraded rotor system give the Bell 214 a high lifting capacity and good performance at high temperatures and altitudes. The twin-engined Bell 214ST shares the model number but is a larger, much-modified aircraft.

Facts
Year
1972 1
Engine Class
Turboshaft 1
Power (kW)
2180 1
Mass (kg)
3442 1
Maximum Mass (kg)
6804 1
Engine
Lycoming LTC4B-8D turboshaft 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Of Make

Source Bell 214 (Wikipedia)
Sources
1. Bell 214 (Wikipedia)
  • Variants, 214A and 214C
    The 299 Bell 214As for the Imperial Iranian Army Aviation were built beginning in 1972
  • Specifications (214A), empty weight
    Empty weight: 7,588 lb (3,442 kg)
  • Specifications (214A), maximum takeoff weight
    Max takeoff weight: 15,000 lb (6,804 kg) with slung load
  • Specifications (214A), powerplant
    Powerplant: 1 × Lycoming LTC4B-8D turboshaft engine, 2,930 shp (2,180 kW)
  • Lead, aircraft description
    The Bell 214 is a medium-lift helicopter derived from Bell Helicopter
  • Lead, builder
    The Bell 214 is a medium-lift helicopter derived from Bell Helicopter's prolific UH-1 Huey series.
  • In Group: Light and Commercial Helicopters, Lead, role of the aircraft
    The Bell 214 is a medium-lift helicopter derived from Bell Helicopter's prolific UH-1 Huey series.
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