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The first prototype flew on June 27, 1977. Entered service in 1980.
| MODEL | C-101 |
| CREW | 1-2 |
| ENGINE | 1 x Garrett TFE731-2-25 turbofan |
| WEIGHTS |
| Take-off weight | 5600 kg | 12346 lb |
| Empty weight | 3350 kg | 7386 lb |
| DIMENSIONS |
| Wingspan | 10.6 m | 34 ft 9 in |
| Length | 12.25 m | 40 ft 2 in |
| Height | 4.25 m | 13 ft 11 in |
| Wing area | 20.0 m2 | 215.28 sq ft |
| PERFORMANCE |
| Max. speed | 685 km/h | 426 mph |
| Ceiling | 12500 m | 41000 ft |
| Range w/max.fuel | 3800 km | 2361 miles |
| Range w/max.payload | 370 km | 230 miles |
| ARMAMENT | 1 x 30mm cannon, 2000kg of weapons |
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