Puneet Varma (Editor)

Bell 400 TwinRanger

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Range
  
730 km

Cruise speed
  
259 km/h

Engine type
  
Allison Model 250

Manufacturer
  
Bell Helicopter

Wingspan
  
11 m

Weight
  
1,400 kg

First flight
  
April 4, 1984

Bell 400 TwinRanger httpsuploadwikimediaorgwikipediaenthumb8

The Bell 400 TwinRanger was a prototype four-bladed, twin-engine civil helicopter developed by Bell Helicopter in the 1980s. Both the TwinRanger and another planned version, the Bell 440, were attempts to market a twin-engine development of the Model 206L LongRanger. The Bell 400A was a planned single-engine version of the 400. TwinRanger, however development was canceled when Bell could not acquire enough orders for production. The TwinRanger name was later used for a twin-engine version of the LongRanger produced from 1994 to 1997.

Contents

Development

Bell has tried several incarnations of a twin-engine version of its successful Bell 206 series. The TwinRanger name dates back to the mid-1980s when Bell first considered developing a twin-engine version of the LongRanger.

The Bell 400 TwinRanger featured a reprofiled fuselage, two Allison 250 turboshafts, the OH-58D Kiowa's four-bladed main rotor, and a new shrouded tail rotor. Bell also planned the single-engine 400A, and the 440 twin with a larger fuselage made possible by a high degree of composites. The Bell 400 first flew on April 4, 1984. Bell suspended development of the 400/440 family in the late 1980s as it felt unable to achieve a profitable production rate of 120 units a year.

Successors

After the success of Tridair's Gemini ST twin-engine conversions of the 206L in the early 1990s, Bell produced the equivalent Bell 206LT TwinRanger based on the 206L-4. Only 13 206LTs were built between 1994 and 1997. The 206LT was replaced in Bell's lineup by the Bell 427, a mostly-new development of the Bell 407, itself a four-bladed single-engine derivative of the 206L.

Variants

Bell 400 
Bell 400A 
Projected model to be powered by one PW209T turboshaft of 937 shp.
Bell 440 

Specifications (Bell 400)

Data from The Illustrated Encyclopedia of Helicopters

General characteristics

  • Crew: one pilot
  • Capacity: five passengers
  • Length: ft in (m)
  • Rotor diameter: 35 ft 0 in (10.60 m)
  • Height: ft in (m)
  • Disc area: 2 ft² (m²)
  • Empty weight: 3,075 lb (1,400kg)
  • Useful load: lb (kg)
  • Loaded weight: lb (kg)
  • Max. takeoff weight: 5,500lb (2,495 kg)
  • Powerplant: 2 × Allison 250-C20P turboshaft, 420 hp (kW) each
  • Performance

  • Never exceed speed: knots (mph, km/h)
  • Maximum speed: knots (172 mph, 278 km/h)
  • Cruise speed: knots (mph, 259 km/h)
  • Stall speed: knots (mph, km/h)
  • Range: 394 nm (mi, 730 km)
  • Service ceiling: 10,000 ft (3,048 m)
  • Rate of climb: 2,000 ft/min (m/s)
  • Disc loading: lb/ft² (kg/m²)
  • Power/mass: hp/lb (W/kg)
  • References

    Bell 400 TwinRanger Wikipedia