Yakovlev Yak-50 Aerostars G-HAMM
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Aircraft Data
The Yak-50 evolved from the Yak-18 family to compete in the 8th World Aerobatic Championships, where it dominated. Built for unrestricted manoeuvres of +9/-6g, it was produced until 1985. The Yak-50 designation was previously used for an earlier fighter.
| Country of Origin | First Flight | No. Built | No. In Service | Crew | Passengers |
|---|---|---|---|---|---|
| Soviet Union | 1975 | 312 | 0 | 1 | 0 - 0 |
Power
Used the M-14P, M-14PF or M-14R ranging from 269kW/360hp - 336kW/450hp
| Engine Count | 1 | |
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* Was originally designed by Ivchenko, but production taken over ny Vedeneyev.
Dimensions
| Length | 7.8 m. 25 ft. 7 in. |
| Wing Span | 9.5 m. 31 ft. 2 in. |
| Height | 3.2 m. 10 ft. 6 in. |
| Empty Weight | 750 kg. 1653 lbs. |
| Max Weight | 911 kg. 2006 lbs. |
Performance
| Max Speed | 401 kph 249 mph |
| Cruise Speed | 270 kph 168 mph |
| Ceiling | 3999.89 m. 13123 ft. |
| Normal Range | nm km. |
| Max Range | 570 308 nm km. |
Display data using: Metric Imperial
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