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Stanton Sunbird
from Wikipedia

The Sunbird is a single-seater homebuilt motor glider, designed and built in New Zealand by Charles Stanton. It first flew in 1995, and was retired in 2005.[1]

Key Information

Design and development

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Charles Stanton of Nelson, New Zealand had previously built and flown an AmEagle American Eaglet motor glider, registration ZK-GOE (c/n AACA/641).[2] That craft's registration was cancelled in 1992. Stanton then went on to design and build a motor glider, and utilised components from the American Eaglet. Construction took over three years, and was completed by early 1995.

The Sunbird was a self-launching motor glider.[3] It was a high-wing monoplane of conventional configuration, with a pod-and-boom style of fuselage. The cantilevered wing had no dihedral and its planform was of constant chord with a tapered outer section. The pilot was housed in a small faired nacelle. The engine was located at the rear of the nacelle, and powered a two-bladed folding propeller.[1] The engine was a 21 kW (28 hp) Rotax 277, which could be re-started in flight.[4] The empennage was of the standard type arranged in a cruciform configuration. The undercarriage was a fixed monowheel fitted with a wheel spat. The Sunbird met the New Zealand specifications for Class 1 Microlights, and was issued with the registration ZK-JEA.[3]

Operational history

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It first flew on 26 February 1995, with Stanton reportedly making numerous flights in it over the next ten years. On one flight, it reached an altitude of 4,000 m (13,000 ft). Another flight lasted for 3+12 hours. The craft's final flight took place on 16 April 2005. It was donated to the Ashburton Aviation Museum on 4 December 2005, during the Museum's Christmas Party.[3]

Specifications

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Data from NZ Civil Aircraft [3]

General characteristics

  • Crew: one
  • Wingspan: 12.80 m (42 ft 0 in)
  • Wing area: 9.20 m2 (99.0 sq ft)
  • Aspect ratio: 17.80
  • Airfoil: Eppler 748 High Lift
  • Empty weight: 142 kg (313 lb)
  • Max takeoff weight: 239 kg (527 lb)
  • Powerplant: 1 × Rotax 277 two stroke, 21 kW (28 hp)
  • Propellers: 2-bladed

Performance

  • Cruise speed: 90 km/h (56 mph, 49 kn)
  • Stall speed: 51 km/h (32 mph, 28 kn)
  • Never exceed speed: 132 km/h (82 mph, 71 kn)
  • Service ceiling: 3,962 m (12,999 ft)
  • g limits: ±4.4
  • Wing loading: 26.0 kg/m2 (5.3 lb/sq ft)

References

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