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 Top Speed (km/h) EngineLycoming GO-435 flat-six engine, 179 kW (240 hp) 1 Comparison
Body StyleAircraft (no road body style) 1 Connections
Exemplifies
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
View the SourceReader Challenges (0)
No disputes yet. Spotted an error or a better source? Open the first one.
Sign in to dispute this or suggest a correction.