Engineering:Sivel SD27 Corriedale
From HandWiki
| SD27 Corriedale | |
|---|---|
| Role | Two-seat light aircraft |
| National origin | Italy |
| Manufacturer | Sivel Aeronautica |
| First flight | 1994 |
The Sivel SD27 Corriedale is an Italian two-seat light touring or training monoplane designed and built by Sivel Aeronautica.[1] The Corriedale is a low-wing monoplane with side-by-side seating for two, and is powered by a nose-mounted Rotax 912 piston engine.[1] It has a fixed landing gear with a swivelling nosewheel.[1] Five pre-series aircraft were produced in 1994 before production started in 1995 and the aircraft was certified under the JAR-VLA.[1] An aerobatic variant flew in 1995 with a larger 119 kW (160 hp) engine.[1]
Specifications
Data from [1]Brassey's World Aircraft & Systems Directory
General characteristics
- Crew: 2
- Length: 6.57 m (21 ft 7 in)
- Wingspan: 10 m (32 ft 10 in)
- Height: 2.76 m (9 ft 1 in)
- Wing area: 12.5 m2 (134.55 sq ft)
- Empty weight: 370 kg (816 lb)
- Gross weight: 620 kg (1,367 lb)
- Powerplant: 1 × Rotax 912 piston engine , 58 kW (78 hp)
Performance
- Maximum speed: 195 km/h (121 mph, 105 kn)
- Range: 1,000 km (621 mi, 540 nmi)
- Service ceiling: 4,000 m (13,125 ft)
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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