Virus SW
SW 80 (472.5kg) SW 100 (472.5kg)  SW 100 (600kg)
ENGINE ROTAX ROTAX 912 UL ROTAX 912 ULS ROTAX 912 ULS
max power 80 hp at 5800 RPM 100 hp at 5800 RPM 100 hp at 5800 RPM
PROPELLER Pipistrel VARIO Variable pitch Variable pitch
SIZES
wing span 10,71 m 10,71 m 10,71 m
length 6,5 m 6,5 m 6,5 m
height 1,85 1,85 1,85
wing area 9,51 m2 9,51 m2 9,51 m2
rudder area 1,1 m2 1,1 m2 1,1 m2
tail area 1,08 m2 1,08 m2 1,08 m2
aspect ratio 11,3 11,3 11,3
positive flaps 9 deg, 19 deg 9 deg, 19 deg 9 deg, 19 deg
negative flaps 5 deg 5 deg 5 deg
center of gravity 25% – 37% 25% – 37% 25% – 37%
WEIGHTS
empty weigh 287 kg 289 kg 289 kg
max take off weight (MTOW) 472.5 kg 472.5 kg 600 kg
fuel tanks capacity 2 x 50 l 2 x 50 l 2 x 50 l
useful fuel 2 x 47 l 2 x 47 l 2 x 47 l
PERFORMANCES DATA for TOM 472.5 kg DATA for TOM 600 kg
stall with flaps 64 km/h 64 km/h 74 km/h
stall without flaps 79 km/h 79 km/h 84 km/h
cruising speed (75% power) 246 km/h 273 km/h 264 km/h
max. horizontal speed 264 km/h 283 km/h 275 km/h
VNE 302 km/h 302 km/h 302 km/h
max speed with airbrakes 205 km/h 205 km/h 205 km/h
max speed with flaps 130 km/h 130 km/h 130 km/h
turbulence penetration speed Vb 250 km/h 250 km/h 250 km/h
best climb speed 140 km/h 140 km/h 148 km/h
max climb rate 6.1 m/sec 8.4 m/sec 6.6 m/sec
best glide ratio speed 118 km/h 118 km/h 123 km/h
best glide 1:17 1:15 1:15
take off run 140 m 95 m 140 m
take off over 15 m obstacle 225 m 175 m 230 m
service ceiling 6200 m 6800 m 5800 m
45° – 45° roll time 1,6 sec 1,6 sec 1.6 s
fuel consum. at cruis. speed 13.6 l/hour 17.8 l/hour 18.0 l/hour
endurance 6,9 hours 5,3 hours 5.3 h
range distance 1650 km 1450 km 1415 km
max load factor permitted ( x 1,8) +4g  -2g +4g  -2g +4g  -2g
design safety factors & tested minumum 1.875 minumum 1.875 minumum 1.875

Pipistrel reserves the right to revise the above data whenever occasioned by product improvement, government/authority regulations or other good cause.
The design basis follow the strictest EASA CS-22, CS-VLA and CS-23 (sections), as well as rules applicable to ultralight/microlight aircraft (LTF-UL 2003, etc.) and ASTM-LSA standards.
Ultralight/Microlight certification basis varies from country to country, therefore the actual certificated data may be different from stated above. Please check the certifications link.