XtremeAir Sbach 300

The XtremeAir Sbach 300 is a German aerobatic aircraft, designed by Philippe Steinbach and produced by XtremeAir, of Cochstedt. The aircraft is supplied as a complete ready-to-fly-aircraft.[1]

Sbach 300
Role Aerobatic aircraft
National origin Germany
Manufacturer XtremeAir
Designer Philippe Steinbach
Status In production (2012)
Variants XtremeAir Sbach 342

The aircraft bears the company designation XA41, but is marketed under the name Sbach 300.[1]

Design and development

The Sbach 300 is an all-composite design, predominately constructed of carbon fibre. It features a cantilever low-wing, a single-seat enclosed cockpit under a bubble canopy, fixed conventional landing gear and a single engine in tractor configuration. The aircraft's 7.50 m (24.6 ft) span wing has an area of 11.25 m2 (121.1 sq ft) and mounts full-span ailerons with spades to lighten control forces, which give a roll rate of 450° per second. The standard engine employed is the 315 hp (235 kW) Lycoming IO-580 four-stroke powerplant. The aircraft has an empty weight of 570 kg (1,260 lb) and a gross weight of 850 kg (1,870 lb) for aerobatics and a gross weight of 999 kg (2,202 lb) for non-aerobatic flight.[1][2]

The 300 was later developed into a two-seat version, the XtremeAir Sbach 342, which was introduced in 2007.[1]

Operational history

The Sbach 300 was flown to a German national aerobatic championship in the unlimited class.[1]

Specifications (Sbach 300)
XtremeAir XA-41

Data from Bayerl and XtremeAir[1][2]

General characteristics

  • Crew: one
  • Length: 6.30 m (20 ft 8 in)
  • Wingspan: 7.50 m (24 ft 7 in)
  • Height: 2.3 m (7 ft 7 in) in three-point attitude
  • Wing area: 11.25 m2 (121.1 sq ft)
  • Aspect ratio: 5:1
  • Empty weight: 570 kg (1,257 lb)
  • Gross weight: 850 kg (1,874 lb) for aerobatics
  • Fuel capacity: 245 litres (54 imp gal; 65 US gal)
  • Powerplant: 1 × Lycoming IO-580 six cylinder, air-cooled, four stroke aircraft engine, 235 kW (315 hp)
  • Propellers: 3-bladed constant speed

Performance

  • Maximum speed: 390 km/h (240 mph, 210 kn)
  • Cruise speed: 345 km/h (214 mph, 186 kn)
  • Stall speed: 94 km/h (58 mph, 51 kn)
  • Never exceed speed: 417 km/h (259 mph, 225 kn)
  • Range: 1,500 km (920 mi, 800 nmi)
  • g limits: +/-10
  • Rate of climb: 20.7 m/s (4,070 ft/min)
  • Wing loading: 57.8 kg/m2 (11.8 lb/sq ft) for aerobatics

See also

References
  1. Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 170. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. XtremeAir. "Specification". Retrieved 6 September 2017.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.