XtremeAir Sbach 342
Sbach 342 | |
---|---|
Role | Aerobatic monoplane |
National origin | Germany |
Manufacturer | XtremeAir GmbH |
Number built | 44+ |
Developed from | XtremeAir Sbach 300 |
The XtremeAir Sbach 342 is a German high performance two-seat aerobatic and touring monoplane designed by Philipp Steinbach with Albert Mylius and built by XtremeAir GmbH of Hecklingen.[1]
The Sbach 342 (a marketing name for the XA42) is a composite structure low-wing monoplane with a fixed conventional landing gear with a tailwheel.[1] It is powered by a 315 hp (235 kW) Lycoming AEIO-580-B1A piston engine driving a three-bladed propeller.[1] It is the tandem version of the single-seater XA 41 (XtremeAir Sbach 300) which was designed by the same team in Speyer in 2004.[1] The XA42 received a type certificate from the European Aviation Safety Agency in March 2011.[1] In November 2012 it received its type certification through the FAA.
Specifications (acrobatic)
Data from [1]Type Certificate Data Sheet
General characteristics
- Crew: 1
- Capacity: 2
- Length: 6.67 m (21 ft 11 in)
- Wingspan: 7.5 m (24 ft 7 in)
- Height: 2.54 m (8 ft 4 in)
- Wing area: 11.25 m2 (121 ft2)
- Empty weight: 670 kg (1477 lb)
- Gross weight: 850 kg (1874 lb)
- Powerplant: 1 × Lycoming AEIO-580-B1A horizontally-opposed six-cylinder piston engine, 245 kW (315 hp)
Performance
- Maximum speed: 416 km/h (256 mph)
- Service ceiling: 4572 m (15000 ft)
- G limits: +/- 10
- Roll rate: 450°/sec
References
Notes
- 1 2 3 4 5 6 "Type Certificate Data Sheet A.507 XA42" (PDF). European Aviation Safety Agency. 18 March 2011. Archived from the original (PDF) on July 28, 2011. Retrieved 15 July 2011.
External links
Wikimedia Commons has media related to XtremeAir XA42. |