Manshū Hayabusa
# Manshū Hayabusa

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 (Production aircraft)

Data from Japanese Aircraft, 1910-1941

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 $m^2$ (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)
