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.[2][3] 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.

MT-1 Hayabusa
Role	Airliner Type of aircraft
National origin	Manchukuo
Manufacturer	Manchuria Airplane Manufacturing Company
First flight	April 1937[1]
Primary user	Manchukuo National Airways
Number built	50-55

Specifications (Production aircraft)

Data from Japanese Aircraft, 1910-1941[1]

General characteristics

• Crew: 1 pilot
• Capacity: 6 passengers
• Length: 9.38 m (30 ft 9 in)
• Wingspan: 13.60 m (44 ft 7 in)
• Height: 3.60 m (11 ft 10 in)
• Wing area: 27.3 m² (294 sq ft)
• Empty weight: 1,700 kg (3,748 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)

Performance

• Maximum speed: 240 km/h (150 mph, 130 kn)
• Cruise speed: 200 km/h (120 mph, 110 kn)
• Range: 902 km (560 mi, 487 nmi)
• Service ceiling: 6,000 m (20,000 ft)

See also

Aircraft of comparable role, configuration, and era

• Airspeed Envoy
• Boeing Monomail
• Breese-Dallas Model 1
• General Aviation/Clarke GA-43
• Heinkel He 70
• Junkers Ju 60
• Kharkiv KhAI-1
• Lockheed Model 9 Orion
• Northrop Delta
• Polikarpov/Rafaelyants PR-12
• Tairov OKO-1
• Vultee V-1

References

Notes

Bibliography

External links

• Mansyu MT-1 Hayabusa ~ A Falcon of Different Feather

На других языках

[fr] Manshū MT-1 Hayabusa