Engineering:Australian Lightwing GR 912

From HandWiki
GR 912 & Sport 2000
Australian LightWing GR 912.jpg
GR 912 model
Role Light-sport aircraft
National origin Australia
Manufacturer Australian Lightwing
Introduction 1986
Status In production

The Australian Lightwing GR 912 and Sport 2000 are a family of Australia n light-sport aircraft, designed and produced by Australian Lightwing and introduced in 1986. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.[1][2]

Design and development

The aircraft series feature a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear or conventional landing gear and a single engine in tractor configuration.[1][2]

The aircraft is made with a welded steel fuselage covered in a combination of fibreglass and doped aircraft fabric. Its 9.50 m (31.2 ft) span wing is made with an aluminum frame and partially covered in aluminum sheet and doped fabric. Standard engines available are the 64 hp (48 kW) Rotax 582 two-stroke, the 80 hp (60 kW) Rotax 912UL, the 100 hp (75 kW) Rotax 912ULS four-stroke powerplant and automotive conversions. The cockpit width is 106 cm (42 in).[1][2]

Variants

Australian LightWing GR 532
GR 532
Initial version with Rotax 532 powerplant
GR 582
Version with Rotax 582 powerplant[1]
GR 912
Tail wheel-equipped version[1]
Sport 2000
Nose-wheel equipped version[1]

Specifications (GR 912)

Data from Jane's All the World's Aircraft 2007–2008[3]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 5.68 m (18 ft 8 in)
  • Wingspan: 9.50 m (31 ft 2 in)
  • Height: 1.90 m (6 ft 3 in)
  • Wing area: 15.35 m2 (165.2 sq ft)
  • Empty weight: 295 kg (650 lb)
  • Gross weight: 544 kg (1,199 lb)
  • Fuel capacity: 60 L (16 US gal; 13 imp gal)
  • Powerplant: 1 × Rotax 912 ULS four cylinder, liquid and air-cooled, four stroke aircraft engine, 73.5 kW (98.6 hp)

Performance

  • Maximum speed: 176 km/h (109 mph, 95 kn)
  • Cruise speed: 148 km/h (92 mph, 80 kn)
  • Stall speed: 74 km/h (46 mph, 40 kn)
  • Range: 400 km (250 mi, 220 nmi)
  • Rate of climb: 4.1 m/s (800 ft/min)

References

  1. ↑ 1.0 1.1 1.2 1.3 1.4 1.5 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 30. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. ↑ 2.0 2.1 2.2 Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 31. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  3. ↑ Jackson 2007, p. 8
  • Jackson, Paul, ed (2007). Jane's All the World's Aircraft 2007–2008. Coulsdon, Surrey, UK. ISBN 978-0-7106-2792-6. 

External links



Retrieved from "https://handwiki.org/wiki/index.php?title=Engineering:Australian_Lightwing_GR_912&oldid=2158674"