Harman Patil (Editor)

Manshū Hayabusa

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Top speed
  
240 km/h

Length
  
9.38 m

Wingspan
  
14 m

First flight
  
April 1937

Manshū Hayabusa aviadejavuruImages6MMMM18210190913jpg

Manufacturer
  
Manchuria Airplane Manufacturing Company

The Manshū MT-1 Hayabusa (Japanese: 隼, "Peregrine Falcon") was an airliner produced by the Japanese Manchuria Airplane Manufacturing Company in Manchukuo in the late 1930s. It was a conventional, low-wing cantilever monoplane with fixed tailwheel undercarriage. The flight deck was fully enclosed and separate from the passenger cabin, which could seat six people. The type equipped Manchukuo National Airways.

Specifications

Data from Japanese Aircraft, 1910-1941

General characteristics

  • Crew: 1 pilot
  • Capacity: 6 passengers
  • Length: 9.38 m (30 ft 9¾ in)
  • Wingspan: 13.60 m (44 ft 7½ in)
  • Height: 3.60 m (11 ft 9¾ in)
  • Wing area: 27.3 m2 (294 ft2)
  • Empty weight: 1,700 kg (3,747 lb)
  • Gross weight: 2,700 kg (5,952 lb)
  • Powerplant: 1 × Nakajima Kotobuki 2-kai-1 nine-cylinder air-cooled radial engine, 343 kW (460 hp) each
  • Performance

  • Maximum speed: 240 km/h (150 mph)
  • Cruising speed: 200 km/h (124 mph)
  • Range: 902 km (560 miles)
  • Service ceiling: 6,000 m (19,700 ft)
  • References

    Manshū Hayabusa Wikipedia