L-15A / JL-10/15 Lead-in Fighter Trainer (LIFT)
| Specifications | |
|---|---|
| Builder | HIAG with assistance from Yakolev OKB |
| Wing Span | 11 m |
| Length | 15 m |
| Height | |
| normal TO weight | 6,500kg |
| max TO Weight | 9,500kg (takeoff) |
| Engine | 2 x DV-2F or AI-222-25F |
| Maximum speed | Mach 1.4 |
| Cruising speed | |
| max climb rate | 150m/s |
| g-load | +8/-3 |
| Range | |
| Service Ceiling | 16,000 m |
| loitering time | 2 hr |
| Armament | various air-to-air and air-to-ground weapons |
| Crew | 2 |
| Cost | |
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