Bell Helicopter Bell 214ST

Medium Transport Helicopter

Bell 214ST PHI © RotorImage.com
Photo ©: RotorImage.com RotorImage.com
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.
Crew2
Passengers16 - 17
Propulsion2 Turboshaft Engines
Engine ModelGeneral Electric CT7-2
Engine Power (each)1212 kW1625 shp
Speed296 km/h160 kts
  184 mph
Service Ceiling3.840 m12.600 ft
Range750 km405 NM
466 mi.
Empty Weight4.300 kg9.480 lbs
max. Takeoff Weight7.938 kg17.500 lbs
Rotor Blades (main/tail)2/2
Main Rotor Diameter15,85 m52 ft 0 in
Tail Rotor Diameter2,95 m9 ft 8 in
Rotor Disc Area197,3 m2124 ft
Length (Fuselage)15,03 m49 ft 4 in
Length18,95 m62 ft 2 in
Height4,84 m15 ft 11 in
First Flight02/1977
Production Statusout of production
Production Range1979 - 1991
Total Production100
Developed fromBell 214 / Bell 205
ICAO CodeB214 BSTP
FAA TCDSH10SW
Data for (Version)Bell 214ST

[Photo-ID: 5870] Karsten Palt 2012-06-13
Bell Helicopter 214ST, Iraqi Air Force, 5722, c/n 28166, Karsten Palt, 2012Bell 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, 5722, c/n 28166, Karsten Palt, 2012Bell Helicopter
214ST
Iraqi Air Force
Reg.: 5722
c/n: 28166
 
captured in 1991
Flying Leatherneck Aviation Museum [San Diego, CA]