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-