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Virus SW 121

EASA CS-LSA certified

 

ENGINE : 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

 

length : 6.45 m, 26.5 ft.

span : 10.70 m, 35.1 ft 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

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

 

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 / h

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-