| model | VIRUS SW 100 EASA LSA |
| ENGINE ROTAX | Rotax EASA certified engine 912S3 100 hp, |
| max power(with 2 carb.) | 100 Hp, 73,5 kW take off power |
| PROPELLER | 2 blade Hydraulic CS MTV-33-1-A/170-200 EASA certified |
| SIZES | |
| length | 6.45 m, 26.5 ft. |
| span | 10.70 m, 21.15 ft. |
| height | 2.06 m, 6.75 ft. |
| wing area | 9.51 m², 102.4 ft² |
| wing span | 10.71 m, 35.10 ft. |
| mean wing chord | 0.898 m, 2.95 ft. |
| horizontal tail area | 1.02 m², 10.9 ft² |
| span | 2.18 m, 7.15 ft. |
| vertical tail area | 1.24 m², 13.3 ft² |
| height | 1.19 m, 3.90 ft. |
| aspect ratio | 11,3 |
| positive flaps | 0°, +9°, +20°; marked (0), (+1), (+2) respectively |
| negative flaps | 5-° marked as (-) |
| center of gravity | 25% – 33% MAC |
| WEIGHTS | |
| Design empty weight | 349 kg, 768 lb |
| max take off weight (MTOW) | 600 kg, 1323 lb |
| Design useful load | 251 kg, 522 lbs |
| max baggage weight | 25 kg, 55 lb |
| fuel tanks capacity | 2 x 50 l |
| useful fuel | 2 x 49 l |
| PERFORMANCES | |
| Vne – Never Exceeded Speed | 163 KTAS |
| Vno – Max Structural Cruising Speed except in smooth air | 120 KIAS |
| Va- Max Operating Maneuvering Speed | 100 KIAS |
| Vfe- Max Flap Extended Speed | 81 KIAS |
| Vae- Max Airbrakes Extended Speed | 100 KIAS |
| stall without flaps | 50 KCAS |
| Towing limitations | glider up to 600 kg (to meet 500 m total take off distance (over 15 m obstacle) |
| best climb speed | 78 KIAS |
| max climb rate | 1050 ft./min |
| take off distance at SL | 160 m |
| take off distance over 15 m obstacle at SL | 320 m |
| Maximum take-off altitude | 10,000 ft. MSL |
| Maximum operating altitude | 16,000 ft. MSL |
| Permitted fuel | AVGAS, MOGAS or car fuel (min RON 95; EN228 Premium or Premium plus with max. 10% Ethanol) |
| fuel consumption at 2000 ft. 75% PWR cruise speed | 18,4 l/min |
| endurance @4000 ft., 65 % power) | 5h 33 min (+30 min reserve) |
| range distance (+ 30 min reserve, @4000 ft., 65 % power) | 1189 km / 642 nm |
| Noise level (ICAO Annex 16, Chapter 10) | 70 dB(A) (measured) |
| Flight Load Factor Limits | 4.0 g+, 2.0 g- |
