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| First flown in 1958, the T1A is an intermediate trainer powered by a 1820kg Bristol Siddeley Orpheus 805 turbojet engine. Forty were built for the JASDF, delivery ending in May 1963. The T1B version was first flown in 1960. Twenty-two were built for the JASDF, each powered by an Ishikawajima-Harima J3-IHI-3 turbojet engine.
| CREW | 2 |
| ENGINE | 1 x BS "Orpheus 80506", 17.8kN |
| WEIGHTS |
| Take-off weight | 5000 kg | 11023 lb |
| Empty weight | 2420 kg | 5335 lb |
| DIMENSIONS |
| Wingspan | 10.5 m | 34 ft 5 in |
| Length | 12.1 m | 40 ft 8 in |
| Height | 4.1 m | 13 ft 5 in |
| Wing area | 22.2 m2 | 238.96 sq ft |
| PERFORMANCE |
| Max. speed | 925 km/h | 575 mph |
| Cruise speed | 620 km/h | 385 mph |
| Ceiling | 15900 m | 52150 ft |
| Range w/max.fuel | 1300 km | 808 miles |
| ARMAMENT | 1 x 12.7mm machine-guns, 2 cannons or 4 missiles or 2 bombs |
| Capitan-Rastrero, 16.09.2020 22:26 What sources did you use to find the armament? reply | | blockhaj, e-mail, 11.11.2015 17:55 Are there any info on the cannons it had? reply |
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