Trainers1962 trainer aircraft model by Fuji
KM-2
The Fuji KM-2 is a Japanese propeller-driven light aircraft, which was developed by Fuji Heavy Industries from the Beechcraft T-34 Mentor which Fuji built under licence. Various versions have been used as primary trainers by the Japan Self-Defense Forces.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Subaru Corporation
- Category
- Trainers
- Country of origin
- Japan
- First flight
- 1962-01-01
- Length
- 312.75 m
- Wingspan
- 394 m
Specifications
- Cruise speed
- 164 kt
- Max speed
- 204 kt
- Range
- 526 nm
- Service ceiling
- 26,800 ft
- Rate of climb
- 1,520 ft/min
- Max takeoff weight
- 3,858 lb
- Empty weight
- 2,500 lb
- Fuel capacity
- 50 US gal
- Powerplant
- Lycoming IGSO-480-A1A6
- Engines
- 1
- Seats
- 2
- Length
- 26 ft
- Wingspan
- 32 ft
- Height
- 9 ft
- Number built
- 64
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.