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Bell 212

By Wikipedia,
the free encyclopedia,

http://en.wikipedia.org/wiki/Bell_212

For an overview of the whole Huey family of aircraft see Bell Huey
Bell 212 Twin Huey
Bell 212 operated by Kachina for the California Department of Forestry departs from the Mojave Spaceport
Role Helicopter
Manufacturer Bell Helicopter
Introduced 1968
Primary user CHC Helicopter
Developed from Bell 204/205
Variants UH-1N Twin Huey
Bell 412

The Bell 212 Twin Huey (also known as the Twin Two-Twelve) is a two-bladed, twin-engined, medium helicopter that first flew in 1968. Originally manufactured by Bell Helicopter in Mirabel, Quebec, Canada, the 212 is marketed to civilian operators and has a fifteen-seat configuration, with one pilot and fourteen passengers. In cargo configuration the 212 has an internal capacity of 220 ft³ (6.23 m³). An external load of up to 5,000 lb (2,268 kg) can be carried.

Development

Based on the stretched fuselage Bell 205, the Bell 212 was originally developed for the Canadian Forces as the CUH-1N and later redesignated as the CH-135. The Canadian Forces took delivery of 50 starting in May, 1971. At the same time the United States military services ordered 294 Bell 212s under the designation UH-1N.


German Bell 212 used as air ambulance by the Ministry of the Interior.
German Bell 212 used as air ambulance by the Ministry of the Interior.

By 1971 the 212 had been developed for commercial applications. Among the earliest uses of the 212 in civil aviation was by Helicopter Service AS of Norway to be used in support of offshore oil rigs. Today the 212 can be found used in logging operations, maritime rescue and resupply in the Arctic on the Distant Early Warning Line or North Warning System.

The 212's main rotor is powered by a Pratt & Whitney Canada PT6T-3 Twin-Pac made up of two coupled PT6 power turbines driving a common gearbox. They are capable of producing up to 1,800 shp (1,342 kW). Should one engine fail the remaining engine can deliver 900 shp (671 kW) for 30 minutes, or 765 shp (571 kW) continuously, enabling the 212 to maintain cruise performance at maximum weight.


Santa Barbara County helitack crew and a Bell 212 on the Day Fire. USFS photo by Jim Akerman.
Santa Barbara County helitack crew and a Bell 212 on the Day Fire. USFS photo by Jim Akerman.

Early 212s configured with an Instrument Flight Rules (IFR) instrument package were required to have a large and very obvious fin attached to the roof of the aircraft, above and slightly behind the cockpit. This fin was initially determined necessary to alter the turning performance of the aircraft during complex instrument flight maneuvers, but now not required due to revised stipulations of the type certificate. Many aircraft still fly with the modification.

In 1979, with the purchase of eight by the Civil Air Authority, the 212 became the first U.S. helicopter sold in PRC.

The ICAO designator for this aircraft as used in a flight plan is "B212". The Bell 412 is a further development of the Bell 212, the major difference being the composite four-blade main rotor.

Variants


Alpine Helicopters Bell 212 on UN peacekeeping duty in Guatemala, 1998
Alpine Helicopters Bell 212 on UN peacekeeping duty in Guatemala, 1998

Bell 212 (C-FOKV) registered to Canadian Helicopters at Cambridge Bay Airport, Nunavut, Canada
Bell 212 (C-FOKV) registered to Canadian Helicopters at Cambridge Bay Airport, Nunavut, Canada

Bell 212 of the Macedonian Police flying over downtown Skopje, 2008
Bell 212 of the Macedonian Police flying over downtown Skopje, 2008
  • Bell Model 212 - Bell Helicopters company designation for the UH-1N.
  • Twin Two-Twelve - Civil utility transport version. It can carry up to 14-passenger.
  • Agusta-Bell AB 212 - Civil or military utility transport version. Built under license in Italy by Agusta.
  • Bell Model 412 - Bell 212 with a four-bladed semi-rigid rotor system. See Bell 412 for further information.

Operators


Civil operators

 Brazil
 Canada
 Faroe Islands
 Greenland
 Philippines

Government operators

 Canada
 Germany
 Croatia
 Japan
 Macedonia
  • Police
 Mexico
  • various police forces
 Philippines
 Slovenia
  • Police
 Serbia
 United States


Specifications (Bell 212)


Cockpit
Cockpit

Data from Bell 212 Rotorcraft Flight Manual

General characteristics

  • Crew: 1 (two for IFR operation)
  • Capacity: 14
  • Length: 57 ft 1.68 in (17.43 m)
  • Rotor diameter: 48 ft (14.64 m)
  • Height: 12 ft 6.83 in (3.83 m)
  • Disc area: 1,809.5 ft² (168.3 m²)
  • Empty weight: 6529.4 lb (2961.7 kg)
  • Max takeoff weight: 11,200 lb (5,080 kg)
  • Powerplant:Pratt & Whitney Canada PT6T-3 or -3B turboshaft, 1,800 shp (1,342 kW)

Performance

See also

Related development

Related lists

External links




Text from Wikipedia is available under the Creative Commons Attribution/Share-Alike License; additional terms may apply.


Published - July 2009














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