Bell Helicopter Bell 214ST
Medium Transport Helicopter
The Bell 214ST is a twin-engined medium utility helicopter produced by the US-American manufacturer Bell Helicopter Company, today Bell Helicopter Textron.
The Bell 214ST is a enlarged development of the Bell 214 BigLifter which itself is a development of the Bell 205.
Crew | 2 | |
Passengers | 16 - 17 |
Propulsion | 2 Turboshaft Engines | |
Engine Model | General Electric CT7-2 | |
Engine Power (each) | 1212 kW | 1625 shp |
Speed | 296 km/h | 160 kts 184 mph |
Service Ceiling | 3.840 m | 12.600 ft |
Range | 750 km | 405 NM 466 mi. |
Empty Weight | 4.300 kg | 9.480 lbs |
max. Takeoff Weight | 7.938 kg | 17.500 lbs |
Rotor Blades (main/tail) | 2/2 | |
Main Rotor Diameter | 15,85 m | 52 ft 0 in |
Tail Rotor Diameter | 2,95 m | 9 ft 8 in |
Rotor Disc Area | 197,3 m² | 2124 ft² |
Length (Fuselage) | 15,03 m | 49 ft 4 in |
Length | 18,95 m | 62 ft 2 in |
Height | 4,84 m | 15 ft 11 in |
First Flight | 02/1977 | |
Production Status | out of production | |
Production Range | 1979 - 1991 | |
Total Production | 100 | |
Developed from | Bell 214 / Bell 205 |
ICAO Code | B214 BSTP | |
FAA TCDS | H10SW | |
Data for (Version) | Bell 214ST |
[Photo-ID: 5870] © Karsten Palt 2012-06-13 | |
Bell Helicopter 214ST Iraqi Air Force Reg.: 5722 c/n: 28166 captured in 1991 | |
Flying Leatherneck Aviation Museum [San Diego, CA] |
[Photo-ID: 5871] © Karsten Palt 2012-06-13 | |
Bell Helicopter 214ST Iraqi Air Force Reg.: 5722 c/n: 28166 captured in 1991 | |
Flying Leatherneck Aviation Museum [San Diego, CA] |