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Kawasaki KAL-2

General Aviation and Light Aircraft

The Kawasaki KAL-2 was a Japanese four or five seat single-engine aircraft designed in the mid-1950s for both military and civil markets, as the successor to Kawasaki's first postwar design, the KAL-1 cabin monoplane. It was a cantilever low-wing monoplane with two metal spars and stressed aluminium skin, hydraulic split flaps and a retractable tricycle undercarriage, and it shared layout and components with the KAT-1 primary trainer. The broad cabin held two seats in front with dual controls and a bench seat for two or three passengers behind. A 240 horsepower Lycoming GO-435 flat-six engine drove a two-blade variable-pitch propeller. Only two prototypes were completed, one serving with the Japan Air Self-Defense Force and the other with the Japan Maritime Self-Defense Force; serial 20001 is displayed at the Tokorozawa Aviation Museum.

Facts
Engine Class
Piston 1
Units Built
2 1
Top Speed (km/h)
293 1
Mass (kg)
1110 1
Engine
Lycoming GO-435 flat-six engine, 179 kW (240 hp) 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Kawasaki KAL-2 (Wikipedia)

Of Make

Source Kawasaki KAL-2 (Wikipedia)
Sources
1. Kawasaki KAL-2 (Wikipedia)
  • Lead
    The Kawasaki KAL-2 is a Japanese four/five seat, single engine aircraft
  • Design and development
    240 hp (179 kW) Lycoming GO-435 flat-six engine installed in the nose
  • Lead, units built
    Only two were completed.
  • Specifications
    Empty weight: 1,110 kg (2,447 lb)
  • Specifications, top speed
    Maximum speed: 293 km/h (182 mph, 158 kn) at sea level
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