type of aircraft
Kawasaki KAL-2
The Kawasaki KAL-2 is a Japanese four/five seat, single engine aircraft, designed for both military and civil markets in the mid-1950s. Only two were completed.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Kawasaki Heavy Industries
- Country of origin
- Japan
- First flight
- 1954-11-25
Specifications
- Cruise speed
- 110 kt
- Max speed
- 158 kt
- Range
- 860 nm
- Service ceiling
- 14,800 ft
- Rate of climb
- 930 ft/min
- Max takeoff weight
- 35,274 lb
- Empty weight
- 2,447 lb
- Fuel capacity
- 79 US gal
- Powerplant
- Lycoming GO-435-C2B
- Engines
- 1
- Seats
- 5
- Length
- 28.9 ft
- Wingspan
- 39.1 ft
- Height
- 8.8 ft
- Number built
- 2
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.