Sukhoi Su-26M Private EC-HYU
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Aircraft Data
The Sukhoi Su-26 is a single-seater aerobatics plane of composite-intensive construction powered by a single radial reciprocating engine and has mid-mounted straight wings and fixed landing gear, the main gear is mounted on a solid titanium arc.
The Su-26M has refined tail surfaces and a 3-bladed Hoffman prop. Su-26MKh with wing external fuel tanks. Su-26M2 with smoke flight tracer and has an additional fuel tank.
| Country of Origin | First Flight | No. Built | No. In Service | Crew | Passengers |
|---|---|---|---|---|---|
| Russia | 1984 | 80 | 80 | 1 | 0 - 0 |
Power
The modified Su-26M3 uses the M9F 430-hp engine.
| Engine Count | 1 | |
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* Was originally designed by Ivchenko, but production taken over ny Vedeneyev.
Dimensions
| Length | 6.83 m. 22 ft. 5 in. |
| Wing Span | 7.8 m. 25 ft. 7 in. |
| Height | 2.92 m. 9 ft. 7 in. |
| Empty Weight | 735 kg. 1619 lbs. |
| Max Weight | 1204 kg. 2653 lbs. |
Performance
| Max Speed | 452 kph 281 mph |
| Cruise Speed | 311 kph 193 mph |
| Ceiling | 3694.18 m. 12120 ft. |
| Normal Range | 833 450 nm km. |
| Max Range | 926 500 nm km. |
Display data using: Metric Imperial
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