Toyo TT-10
| Toyo TT-10 | |
|---|---|
| Type: | Trainer aircraft |
| Design country: | |
| Manufacturer: |
Toyo Aircraft Manufacturing Co. |
| First flight: |
December 30, 1952 |
| Number of pieces: |
2 |
The Toyo TT-10 is a trainer aircraft produced by the Japanese manufacturer Toyo Aircraft Manufacturing Co.
History and construction
After the aviation ban was lifted, Toyo Aircraft Manufacturing Co. began developing the TT-10 in 1952 . The aircraft is a two-seater low-wing aircraft with a fixed tail wheel landing gear. Teachers and students sit one behind the other in a closed cockpit. The fuselage of the TT-10 consists of a welded chrome-molybdenum steel frame and, like the wings, which consist of a wooden frame, is covered with fabric. The machine is powered by a Lycoming O-290 -D2 four-cylinder boxer engine with 100 kW. The first prototype flew for the first time on December 30, 1952, the production model on February 11, 1953. Presumably only these two machines were built.
Technical specifications
| Parameter | Data |
|---|---|
| crew | 2 |
| length | 7.15 m |
| span | 8.60 m |
| height | 2.10 m |
| Wing area | 12 m² |
| Empty mass | 568 kg |
| Max. Takeoff mass | 800 kg |
| Cruising speed | 190 km / h |
| Top speed | 235 km / h |
| Service ceiling | 4,300 m |
| Range | 685 km |
| Engines | 1 Lycoming O-290 -D2, 100 kW |
Preserved copies
- One machine is located in the Tokyo Metropolitan Industrial Technology College of Technology
literature
- Jane's All the World's Aircraft 1956/57, pp. 185 ff.
See also
Web links
Individual evidence
- ↑ Jane's All the World's Aircraft 1956/57, pp. 185ff