Fuji T-1
Trainer
The Fuji T-1 is a single-engine two-seat jet trainer aircraft produced by the Japanese manufacturer Fuji Heavy Industries.
The version Fuji T-1B is powered by a Ishikawajima-Harima J3-7B turbojet engine.
| Propulsion | 1 Turbojet Engine |
| Engine Model | Bristol Siddeley Orpheus 805 |
| Engine Power | 17,8 kN | 4000 lbf |
| max. Cruise Speed | 620 km/h | 335 kts
386 mph |
| max. Speed (vne) | 924 km/h | 499 kts
574 mph |
| Service Ceiling | 15.900 m | 52.165 ft |
| Range | 1.300 km | 702 NM
808 mi. |
| Empty Weight | 2.420 kg | 5.335 lbs |
| max. Takeoff Weight | 5.000 kg | 11.023 lbs |
| Wing Span | 10,50 m | 34 ft 5 in |
| Wing Area | 22,2 m² | 239 ft² |
| Length | 12,12 m | 39 ft 9 in |
| Height | 4,08 m | 13 ft 5 in |
| First Flight | 08. Jan. 1958 |
| Production Status | out of production |
| Total Production | 63 |
| ICAO Code | T1 |
| Data for (Version) | Fuji T-1A (T1F2) |
| Variants | T-1A (T1F2), T-1B (T1F1) |
