Bell 214 Biglifter
The Bell 214 BigLifter is a multipurpose helicopter, developed by the American company Bell Helicopter Textron based on the Bell Model 214 Huey Plus. This aircraft was created as a hybrid variant, integrating elements from the UH-1H Huey and the Bell Model 309 KingCobra, specifically utilizing the latter’s transmission and main rotor.
Origins and Development
Optimized for operations in the Middle East, the first prototype of the Bell 214 BigLifter made its maiden flight in December 1972. Serial production for this versatile helicopter officially commenced in April 1975.
Global Service and Variants
The Bell 214 BigLifter saw service with several air forces, including those of Iran, Dubai, Oman, Thailand, the Philippines, and Ecuador. Its robust design and performance made it a preferred choice for various missions.
A notable modification, the Bell 214A, was built by the Italian company Agusta. This variant featured a powerful LTC4B-8D gas turbine engine, delivering 2214 kW, and was supplied to the Air Force of Uganda.
Technical Specifications
| Modification | Bell 214В |
| Main rotor diameter, m | 15.24 |
| Tail rotor diameter, m | 2.95 |
| Length, m | 18.52 |
| Height, m | 4.57 |
| Maximum takeoff weight, kg | 7257 |
| Engine type | 1 Gas turbine engine Textron Lycoming T5508D |
| Power, kW | 1 x 2185 (1528 at takeoff) |
| Cruising speed, km/h | 259 |
| Practical range, km | 1100 |
| Combat radius, km | 420 |
| Service ceiling, m | 4500 |
| Static ceiling, m | 2500 |
| Crew | 2 |
| Payload | 18 passengers or 3175 kg of cargo |
Image and diagram gallery of the Bell 214 Biglifter
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Fuentes y Rigurosidad
La información presentada en esta ficha técnica ha sido compilada a partir de manuales de vuelo desclasificados, archivos históricos y bibliografía especializada. Aunque nos esforzamos por mantener la máxima precisión, algunos datos de rendimiento pueden variar según la variante específica o las condiciones operativas.