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Kawanishi K6K

Flying Boats and Seaplanes

The Kawanishi K6K was a two-seat, twin-float biplane trainer built by the Kawanishi Aircraft Company in the late 1930s as a prototype for the Imperial Japanese Navy. It was conceived to meet a Navy requirement for an intermediate-level training seaplane and used a welded steel-tube fuselage covered in fabric, a fabric-covered steel wing and light alloy monocoque floats. Power came from a single Nakajima Kotobuki 9-cylinder air-cooled radial engine. Its first flight took place on 30 April 1938, but the flight tests revealed poor alighting characteristics, so the type was not ordered into production and only two prototypes were completed.

Facts
Year
1938 1
Engine Class
Piston 1
Status
Prototype 1
Top Speed (km/h)
232 1
Mass (kg)
1300 1
Comparison
Body Style
Aircraft (no road body style) 1
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Exemplifies

Source Kawanishi K6K (Wikipedia)

Of Make

Source Kawanishi K6K (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Kawanishi K6K (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
built by the Kawanishi Aircraft Company

Originated In

Also in Geography Atlas: where this subject originated.

Source Kawanishi K6K (Wikipedia)Lead
Quote, Lead
prototype Japanese training aircraft
Sources
1. Kawanishi K6K (Wikipedia)
  • Lead
    prototype Japanese training aircraft
  • Lead, status
    was a prototype Japanese training aircraft
  • Design
    The first flight of the K6K occurred on 30 April 1938
  • Specifications
    9-cylinder air-cooled radial piston engine
  • Specifications, mass
    Empty weight: 1,300 kg
  • Specifications, top speed
    Maximum speed: 232 km/h
  • Lead, manufacturer
    built by the Kawanishi Aircraft Company
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