Airkraft Sunny

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Sunny
300px
Sunny Sport
Role Ultralight aircraft
National origin Switzerland
Manufacturer Dewald Leichtflugzeugbau Gmbh
Tandem Aircraft KG
Airkraft Gmbh Leichtflugzeugbau
Status In production
Number built 250
Unit cost
21,000 (assembled, 2011)

The Airkraft Sunny is a Swiss ultralight aircraft that was originally produced by the Dewald Leichtflugzeugbau Gmbh of Bad Schönborn, Germany, then Tandem Aircraft KG of Saulgau, Germany and more recently by Airkraft Gmbh Leichtflugzeugbau of Beringen, Switzerland. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly-aircraft.[1][2][3]

Design and development

The aircraft complies with the Fédération Aéronautique Internationale microlight category rules. It features an unusual diamond-shaped biplane, strut-braced closed wing layout, a two-seats-in-tandem enclosed or open cockpit, fixed tricycle landing gear and a single engine in pusher configuration. The upper wing is swept back, while the lower wing is straight, but mounted further aft. The two wings are joined by swept tip rudders. The elevons are mounted to the lower wing only.[1]

The aircraft is made from bolted-together aluminum tubing, with its flying surfaces covered in Dacron sailcloth. Standard engines available include many models of Hirth, Rotax, BMW and Verner 133M powerplants, ranging from 65 to 80 hp (48 to 60 kW).[1]

Variants

Sunny Light
Version with open cockpit[1]
Sunny Sport
Version with enclosed or semi-enclosed cockpit[1][2]
Sunny Amphibian
Version with amphibious floats[1]

Specifications (Sunny Light)

Data from Bayerl[1]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Wingspan: 7 m (23 ft 0 in)
  • Wing area: 17 m2 (180 sq ft)
  • Empty weight: 220 kg (485 lb)
  • Gross weight: 450 kg (992 lb)
  • Fuel capacity: 44 litres (9.7 imp gal; 12 US gal) or optionally 80 litres (18 imp gal; 21 US gal)
  • Powerplant: 1 × Rotax 582 twin cylinder, liquid-cooled, two stroke, 48 kW (64 hp)

Performance

  • Maximum speed: 145 km/h (90 mph; 78 kn)
  • Cruising speed: 100 km/h (62 mph; 54 kn)
  • Stall speed: 55 km/h (34 mph; 30 kn)
  • Rate of climb: 4 m/s (790 ft/min)

References

  1. 1.0 1.1 1.2 1.3 1.4 1.5 1.6 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 23. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. 2.0 2.1 Bertrand, Noel; Rene Coulon; et al: World Directory of Leisure Aviation 2003-04, page 135. Pagefast Ltd, Lancaster UK, 2003. ISSN 1368-485X
  3. Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 266. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1

External links