XtremeAir Sbach 300
Sbach 300 | |
---|---|
Role | Aerobatic aircraft |
National origin | Germany |
Manufacturer | XtremeAir |
Designer | Philippe Steinbach |
Status | In production (2012) |
Variants | XtremeAir Sbach 342 |
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]
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 324 hp (242 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)
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, 242 kW (324 hp)
- Propellers: 3-bladed constant speed
Performance
- Maximum speed: 389 km/h; 242 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: 1,482 km; 921 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
External links
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