Votec 221
Votec 221 is a single-engine, single-seat mid - decker . The sport aircraft was developed in Switzerland and manufactured by MSW Aviation AG in Wohlen . The Votec 221 is approved in the normal and aerobatic flight category . First flight was in 2011.
Technical specifications
The aircraft fuselage consists of a gas-shielded frame made of high-strength steel tubes, which is clad with shells made of carbon fiber reinforced plastic (KfK). The wings and cross tail are made in sandwich construction with KfK top layers. The rudder has an aerodynamic compensation. The rudder pedals are electrically adjustable. The hood of the cockpit is made in one piece and can be opened to the side.
- Length: 6.00 m
- Span: 6.30 m
- Height: 1.65 m
- Wing area: 7.10 m²
- Wing loading: 84.54 kg / m²
- Empty weight: 420 kg
- Max. Takeoff weight: 600 kg
- Take-off run: approx. 110 m
- Powerplant: Lycoming AEIO-390 four-cylinder engine with injection, 160 kW (210 hp) with redundant electrical ignition.
- Propeller: three-blade controllable pitch propeller MTV-12-BC; 1.85 m diameter
- Tank capacity: 120 l in the fuselage, optional additional area tanks possible
- Range: around 740 km, depending on the tank system
- Top speed: 435 km / h
- Stall speed : 104 km / h
- permissible load factor : + 10 / −10 g
- Landing gear: tail wheel , tail wheel controllable by rudder pedals
- Crew: 1
swell
- Paul A. Jackson, (2012). Jane's All the World's Aircraft : development & production: 2012–13. IHS Global. ISBN 978-0-7106-3000-1 .
Web links
- Website MSW Aviation AG
- Video aerobatic demonstration 2012 , pilot: Markus Ruesch
- Votec 221 with German approval: D-EXBL aerokurier.de, accessed October 17, 2013
Individual evidence
- ^ First flight ( memento of December 11, 2013 in the Internet Archive ) mswaviation.ch, accessed October 15, 2013