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Sivel SD28

From Wikipedia, the free encyclopedia
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

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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

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Notes

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  1. ^ a b c d Taylor 1996, p. 407

Bibliography

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  • Taylor, Michael J. H. (1996). Brassey's World Aircraft & Systems Directory. London, England: Brassey's. ISBN 1-85753-198-1.