Engineering:Sivel SD28
From HandWiki
| SD28 | |
|---|---|
| Role | Two-seat aerobatic monoplane |
| National origin | Italy |
| Manufacturer | Sivel Aeronautica |
| First flight | 1995 |
The Sivel SD28 is an Italian two-seat aerobatic monoplane designed and built by Sivel Aeronautica.[1] The SD28 is a low-wing monoplane with side-by-side seating for two and dual controls.[1] The SD28 is powered by a nose-mounted Lycoming AEIO-320-D piston engine and has a fixed nosewheel landing gear.[1]
Specifications
Data from [1]Brassey's World Aircraft & Systems Directory
General characteristics
- Crew: 2
- Length: 6.8 m (22 ft 4 in)
- Wingspan: 8.4 m (27 ft 7 in)
- Height: 2.76 m (9 ft 1 in)
- Wing area: 10.0 m2 (107.6 sq ft)
- Empty weight: 520 kg (1,168 lb)
- Gross weight: 800 kg (1,764 lb)
- Powerplant: 1 × Lycoming AEIO-320-D piston engine , 120 kW (160 hp)
Performance
- Maximum speed: 268 km/h (166 mph, 144 kn)
- Range: 1,019 km (634 mi, 551 nmi)
References
Notes
Bibliography
- Taylor, Michael J. H. (1996). Brassey's World Aircraft & Systems Directory. London, England: Brassey's. ISBN 1-85753-198-1. https://archive.org/details/brasseysworldair0000unse.
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