| Technical data | |
|---|---|
| Type | MiG-AT |
| Function | trainer |
| Year | (1996) |
| Crew | 2 |
| Engines | 2*GRTS Larzac 04-R20 |
| Wing Span | 10.6m |
| Length | 11.15m |
| Height | 4.27m |
| Wing Area | 21.0m2 |
| Maximum Weight | 6800kg |
| Speed | 850km/h |
| Ceiling | |
| Range | 1200km |
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New basic jet trainer, selected to replace the L-29 and L-39. The MiG-AT is more conventional than the Yak-130. It has a low-set, straight wing, with the engines on top, and a T-tail. Two prototypes are being built, and orders are hoped to exceed 1200. The MiG-AT has French engines, and is also being developed in cooperation with the South-Korean Daewoo.
In 2001 VVS RF (lobbied by design bureau) decided to delegate representatives to the certification trials. Pre-production series may be ordered for evaluation at the military pilots schools as well.
| Modified January 25, 1996 |
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