Fuji T-7
Fuji T-7 | |
---|---|
Type: | Trainer aircraft |
Design country: | |
Manufacturer: | |
Commissioning: |
2002 |
Number of pieces: |
49 |
The Fuji T-7 is a beginner's trainer aircraft produced by Fuji Heavy Industries for the Japanese Air Self-Defense Forces . The T-7 was developed from the Fuji T-3 and is a low-wing aircraft powered by a turboprop engine with a retractable nose wheel landing gear.
history
The Fuji T-7 was developed to meet a request from the Japanese Air Self-Defense Forces for a new beginner and advanced trainer aircraft to replace the Fuji T-3. For this purpose, an international tender procedure was carried out in 1998. The T-7 won against the Pilatus PC-7 Turbo Trainer. Due to a corruption scandal that cost several Fuji managers their jobs, the tender was carried out again. Again the T-7 (then called T-3 Kai) won. Production started in September 2000 and the first aircraft were handed over in September 2002.
construction
The T-7 is a modified version of the T-3, which itself was a further development of the Fuji KM-2 , which in turn was derived from the Beech T-34 . The airframe of the T-3 was used, in which an Allison 250 turboprop engine was installed in place of the Lycoming boxer engine .
Military users
Technical specifications
Parameter | Data |
---|---|
crew | 2 |
length | 8.59 m |
span | 10.04 m |
height | 2.96 m |
Wing area | 16.50 m² |
Max. Takeoff mass | 1585 kg |
Cruising speed | 296 km / h |
Top speed | 376 km / h |
Service ceiling | 7620 m |
Climb performance | 11.6 m / s |
Range | 1400 km |
Engine | Turboprop Rolls-Royce ( Allison 250 ) -B17F |
power | 336 kW (450 WPS) |
Web links
Individual evidence
- ↑ Data from Paul Jackson (2004). Jane's All the World's Aircraft 2004-2005 p. 374ff