|Role||Ultralight civil utility aircraft|
base price EUR 69,000
|Developed from||Pipistrel Sinus|
Design and development
It is a high-wing, cantilever monoplane of pod-and-boom configuration with a T-tail. The cabin has two seats side-by-side. Its fixed undercarriage can be provided in either tricycle or tailwheel configuration. It is available in three models: the Virus 912 with a 12-metre wingspan, the Virus 912 SW 80 (for "short wing" and 80 hp) and the Virus 912 SW 100, both with a 10-metre wingspan. The Virus SW 100 has an uprated Rotax 912 ULS engine producing 100 hp (75 kW). The SW 100 model cruises at 273 km/h (170 mph), which is 24 km/h (15 mph) faster than the long wing 80 hp (60 kW) version.
The aviation journalist Paul Bertorelli has criticized the aircraft's design for lack of cabin occupant crashworthiness, however the manufacturer points out that this kind of issue is typical of aircraft in the LSA category. The design has no history of head trauma during the accidents that have occurred.
By February 2014 Pipistrel had produced more than 600 Sinus/Virus aircraft.
The Virus won the NASA 2007 Personal Air Vehicle (PAV) Challenge and the 2008 General Aviation Technology (GAT) Challenge.
On 8 January 2012, Slovenian pilot Matevž Lenarčič launched an around-the-world flight attempt from Slovenia in a turbocharged Virus SW914. sponsored as the GreenLight World Flight. As part of his flight he flew past Mount Everest at an altitude of 29,344 ft (8,944 m), some 300 ft (91 m) above the peak's height; this portion of the journey was not authorized, as Nepal had cancelled his permit to make the flight right before he took off. He completed the flight on 19 April 2012, returning to Slovenia claiming to be the first person to complete such a flight without a copilot and having flown 62,000 miles (99,839 km) during the journey.
Specifications (Virus SW 100 912)
Data from Manufacturer's specification
- Crew: 2
- Length: 6.05 m (19 ft 10 in)
- Wingspan: 11 m (36 ft 1 in)
- Height: 1.85 m (6 ft 1 in)
- Empty weight: 284 kg (626 lb)
- Max takeoff weight: 600 kg (1,323 lb)
- Fuel capacity: 100l
- Powerplant: 1 × Rotax 912 ULS , 75 kW (100 hp)
- Maximum speed: 300 km/h (186 mph; 162 kn)
- Cruise speed: 274 km/h; 170 mph (148 kn) at 75% power
- Range: 1,420 km (882 mi; 767 nmi)
- Endurance: 5.3 hr
- Service ceiling: 7,000 m (22,966 ft)
- Rate of climb: 8.4 m/s (1,650 ft/min)
|Wikimedia Commons has media related to Pipistrel Virus.|
- Vandermeullen, Richard: 2012 Kit Aircraft Buyer's Guide, Kitplanes, Volume 28, Number 12, December 2011, page 63. Belvoir Publications. ISSN 0891-1851
- Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 70. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- Bertorelli, Paul (12 September 2012). "LSA Crashworthiness". AVweb. Retrieved 13 September 2012.
- "Slovenia's Pipistrel marks 600th ultralight aircraft". Shanghai Daily. 2013-04-18. Retrieved 2014-02-14.
- Manufacturer's site
- "Flying the Pacific on 93 gallons of fuel Pilot to circumnavigate world in Pipistrel motor glider". Retrieved February 23, 2012.
- Grady, Mary (30 March 2012). "Pipistrel LSA Flies Above Mt. Everest". AVweb. Retrieved 31 March 2012.
- Associated Press, "Lofty Achievement," Washington Post Express, April 20, 2012, p. 8.