Bell 206 JetRanger
Country of Origin
United States of America
Light utility helicopter
The JetRanger series has become the definitive turbine powered light utility and corporate helicopter of the past three decades. The JetRanger can trace its lineage back to an unsuccessful contender for a US Army competition for a light observation helicopter, which was won by the Hughes 500. This first Model 206 made its first flight on December 8 1962, while the following civil 206A, powered by a 235kW (317shp) Allison C18A, followed, flying on January 10 1966. Deliveries of the first production JetRangers began late in that same year. In the early 1970s production switched to the Model 206B JetRanger II with a 300kW (400shp) 250C20 turboshaft, while conversion kits to upgrade earlier As to the new standard were made available. The third major variant of the JetRanger is the 315kW (420shp) 250C20B powered JetRanger III, with first deliveries commencing in late 1977. Once again Bell offered a conversion kit to update earlier JetRangers to the new standard. Other features introduced on the JetRanger III were a larger and improved tail rotor and minor modifications. JetRanger production was transferred from Texas to Mirabel in Canada in 1986, where the current production model remains the 206B3 JetRanger III. The JetRanger was also accepted by the US Army as an observation helicopter as the OH58 Kiowa, and variants of the Kiowa remain in production in the USA. Military 206Bs were also built in Australia for the Australian Army, where plans were also held to build civilian 206Bs for the Australian market under license, but these fell through.
206B JetRanger II - One 300kW (400shp) Allison 250C20 turboshaft driving a two blade main rotor and two blade tail rotor. 206B3 JetRanger III - One 315kW (420shp) Allison 250C20J.
206B - Max cruising speed 219km/h (118kt). Initial rate of climb 1540ft/min. Range 702km (379nm). 206B3 - Max speed 225km/h (122kt), max cruising speed 214km/h (115kt). Initial rate of climb 1280ft/min. Range with max fuel and no reserves 732km (385nm).
206B - Empty 660kg (1455lb), max takeoff 1360kg (3000lb). 206B3 - Empty 737kg (1635lb), max takeoff with external load 1521kg (3350lb), with internal load 1451kg (1500lb).
Main rotor diameter 10.16m (33ft 4in), fuselage length 9.50m (31ft 2in), height 2.91m (9ft 7in). Main rotor disc area 81.1m2 (872.7sq ft).
Total accommodation for five, including one pilot and one passenger in the front, and three behind them on the rear bench seat. Max internal payload (Model 206B) 635kg (1400lb), max external sling load 680kg (1500lb).
Over 7700 military and civil versions of the JetRanger have been built by Bell in the USA and Canada, AgustaBell in Italy and other licensees. More than 4400 built for civilian customers.
Bell 206 JetRanger
The backbone of this section is from the The International Directory of Civil Aircraft by Gerard Frawley and used with permission. To get your own copy of the book click here.