MSW Votec 221

Votec 221 is a single-engine, single-seat mid-wing monoplane. The light aircraft was developed in Switzerland and manufactured by the MSW Aviation AG in Wohlen. The Votec 221 is approved in the category normal and aerobatics. First flight took place in 2011.

Specifications

The fuselage consists of an inert-gas welded frame made of high strength steel tubes, which is covered with shells made of carbon fiber reinforced plastic ( Kf K ). The wing cross and tail are made in sandwich construction with Kf K - surface layers. The rudder has an aerodynamic balance. The rudder pedals are electrically verstellbar.Die cover the cockpit is made ​​in one piece and side folding.

  • Length: 6.00 m
  • Wingspan: 6.30 m
  • Height: 1.65 m
  • Wing area: 7.10 m²
  • Wing loading: 84.54 kg / m²
  • Empty mass: 420 kg
  • Max take off weight: 600 kg
  • Take-off distance: about 110 meters
  • Engine: Lycoming AEIO -390 four-cylinder engine with fuel injection, 160 kW ( 210 hp ) with redundant electric ignition.
  • Propeller: 3-blade variable pitch MT-Propeller Type: MTV -12 -BC, 1.85 m diameter
  • Tankkazität: 120 liters in the hull, optional surface auxiliary tanks possible
  • Range: 740 kilometer depending on the tank system
  • Höchgeschindigkeit: 435 km / h
  • Stall speed: 104 km / h
  • G limits: 10 / -10
  • Suspension: tailwheel, tailwheel controlled by rudder pedals
  • Crew: 1 pilot

Swell

  • Paul A. Jackson, (2012 ). Jane's All the World 's Aircraft: development & production: 2012-13. IHS Global. ISBN 978-0-7106-3000-1.
Wohlen, Aargau Shielding gas Rudder#Aircraft rudders
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