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Bell 214 Biglifter

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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

Bell 214 Biglifter
Bell 214 Biglifter
Bell 214 Biglifter
Bell 214 Biglifter
Bell 214 Biglifter
Bell 214 Biglifter
Bell 214 Biglifter
Bell 214 Biglifter
Bell 214 Biglifter
Bell 214 Biglifter
Bell 214 Biglifter
Bell 214 Biglifter
Bell 214 Biglifter
Bell 214 Biglifter

United States

ArchivoAéreo Editorial Team

A group of aviation researchers and enthusiasts dedicated to documenting and preserving global aeronautical history. All articles are reviewed to ensure historical accuracy.

Sources & Accuracy

The information presented in this technical sheet has been compiled from declassified flight manuals, historical archives, and specialized literature. While we strive for maximum accuracy, some performance data may vary depending on the specific variant or operational conditions.