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The Bell Model 206 JetRanger is one of the most successful helicopter designs in the world. The design originated in the mid-1960s as an entry in a US Army competition for a light observation (scout) helicopter. Although Bell lost the contract, the Model 206 "JetRanger" entered the civilian market in 1967. The Model 206 has been overhauled three times, the basic shape and design are unchanged since 1967. The JetRanger is popular with news media for traffic and news reporting. In a twist, the US Army eventually selected the 206 for use as the OH-58 Kiowa , fulfilling its original role. The US Navy , Marines , and Coast Guard use 206 variants known as the TH-57 "Sea Ranger" in the Navy and Marines and the TH-67 Creek in the Army as a trainer for helicopter students.

The Bell 206 is a two-rotor, turbine powered helicopter with a conventional, two-bladed tail rotor. The aircraft uses hydraulic flight controls. The Model 206-B3 is the "original" five-seat model, while the '''206-L4''' is the "stretch" seven-seat version (a.k.a., "LongRanger"). Both versions have two individual seats up front and a three seat bench in the back; the LongRanger adds two rear-facing seats in between the front and rear seats. The model 206s is typically flown by a single pilot, who sits in the front right seat.

The Model 206 design has yielded a number of derivative aircraft, including the 407 and military OH-58 Kiowa. The 407 and OH-58D use a newer, 4-bladed Articulated Rotor System that offers improved performance while reducing vibration and noise.

The ICAO designator for both the JetRanger and the LongRanger as used in Flight Plan s is B06.


SPECIFICATIONS (206-B3)

  plane Or Copter copter
  jet Or Prop prop
  crew 1
  capacity 4
  length Main 39 ft 1 in
  length Alt 119 m
  span Main 33 ft 4 in
  span Alt 1016 m
  height Main 283 m
  height Alt 9 ft 4in
  area Main 872 ft&2
  area Alt 811 m&2
  empty Weight Main 1,632 lb
  empty Weight Alt 742 kg
  loaded Weight Main 3,200 lb
  loaded Weight Alt 1,452 kg
  max Takeoff Weight Main 3,350 lb
  max Takeoff Weight Alt 1,520 kg
  engine (prop) Allison 250 -C20J
  type Of Prop Turboshaft
  number Of Props 1
  power Main 420 shp
  power Alt 313 kW
  max Speed Main 139 mph
  max Speed Alt 224 km/h
  range Main 437 miles
  range Alt 704 km
  ceiling Main 13,500 ft
  ceiling Alt 4,115 m
  climb Rate Main 1,280 ft/min
  climb Rate Alt 65 m/s
  loading Main 4 lb/ft&2
  loading Alt 18 kg/m&2
  power/mass Main 026 hp/lb
  power/mass Alt 042 kW/kg




MILITARY OPERATORS

  • Australia, Austria, Bangladesh, Brazil, Bulgaria, Burma/Myanmar, Brunei, Cameroon, Canada, Chile, Colombia, Croatia, Cyprus, Ecuador, Ethiopia, Finland, Greece, Guatemala, Guyana, Indonesia, Iran, Israel, Italy, Ivory Coast, Jamaica, Kuwait, Libya, Malta, Mexico, Morocco, Oman, Pakistan, Peru, Philippines, Saudi Arabia, South Korea, Spain, Sri Lanka, Sweden, Taiwan, Tanzania, Thailand, Turkey, Uganda, United Arab Emirates, United States (Army, Navy), Venezuela, Yemen.