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- |