The Kawasaki KAL-2, deigned and built by the Kawasaki-Gifu division of the Kawasaki Aircraft Company, was produced in 1955 as a development of the KAL-1 ns KAT-1.
Of all-metal construction, the KAL-2 seats four.
An initial order for two was placed by the Japanese Air Self-Defence Force.
Engine: Lycoming GO-435-C2B, 260 hp
Span: 39 ft 0.5 in
Wing area: 206.66 sq.ft
Length: 28 ft 8.5 in
Height: 9 ft 6 in
Empty weight: 2315 lb
Loaded weight: 3527 lb
Max speed: 183 mph at 7742 ft
Cruise: 112 mph
Range: 994 mi
Seats: 4
All Aero 