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Contents

   



(Top)
 


1 Design  





2 Specifications (K6K)  





3 References  














Kawanishi K6K






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From Wikipedia, the free encyclopedia
 


K6K
Role Floatplane trainer
Manufacturer Kawanishi Aircraft Company
First flight 30 April 1938
Primary user IJN Air Service
Number built 3

The Kawanishi K6K was a prototype Japanese training aircraft built by the Kawanishi Aircraft Company in the late 1930s.

Design[edit]

The K6K was a 2-seat twin-float biplane with a welded steel-tube fuselage, covered in fabric, light alloy and steel wing covered in fabric and monocoque floats built from light alloy. It was conceived in response to an Imperial Japanese Navy requirement for an intermediate-level training seaplane. The first flight of the K6K occurred on 30 April 1938, but flight tests revealed poor alighting characteristics, so the K6K was not ordered into production.[1]

Specifications (K6K)[edit]

Data from Japanese Aircraft, 1910-1941[1]

General characteristics

Performance

References[edit]

  1. ^ a b Mikesh, Robert C.; Shorzoe Abe (1990). Japanese Aircraft, 1910-1941. Annapolis, MD: Naval Institute Press. p. 140. ISBN 1-55750-563-2.

Retrieved from "https://en.wikipedia.org/w/index.php?title=Kawanishi_K6K&oldid=1101725213"

Categories: 
1930s Japanese military trainer aircraft
Mitsubishi aircraft
Biplanes
Single-engined tractor aircraft
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This page was last edited on 1 August 2022, at 13:59 (UTC).

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