MSW VOTEC 322
Two-seat aerobatic aircraft

Wing span
Length
Hight
Wing surface
Engine
Power
RPM
Propeller

7.30 m
6.50 m
2.50 m
10.50 m²
Lycoming AEIO 540
260-400 PS
2500 U/Min max.
MTV-14 4 Blade
Constant Speed

Max. Speed
Stall Speed
G-Limits
Climb performance
Main fuel tank
Wing tanks
Endurance
Empty weight

220 kt
55 kt
± 10 G
ca. 3400 ft/min.

110 L
2 x 43 L Optional
ca. 750 NM (196 L)
630 kg

Spacious cockpit
ergonomic seating position
easy maintenance
Noise category D (Switzerland), with MSW Aviation muffler system

Wings
One piece all wood (Douglas fir) with Okume plywood skin covered with carbon fibre

Fuselage
Welded 4130 tubing with carbon fiber exterior panels

Rudders
Carbon fiber composites

Ailerons
Carbon fiber composites