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The JAI-39 (Russian: ХАИ-39) was designed at SKB JAI in 1978 as a single-seat experimental light aircraft oftwin-engine configuration.
Only one example was built.
Engines: two 4 hp Druzhba
Wingspan: 10.65 m
Wing area: 17.63 m²
Length: 3.62 m
Empty weight: 42.65 kg
Maximum takeoff weight: 140 kg
Maximum speed at sea level: 45 km / h
Landing speed: 22 km / h
Take-off run: 10 m
Accommodation: 1
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