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Virus SW

VIRUS UL Aircraft technical data
       

Virus SW

SW 80 (472.5kg)

SW 100 (472.5kg)

 SW 100 (600kg)

ENGINE ROTAX ROTAX 912 UL ROTAX 912 ULSROTAX 912 ULS
max power 80 hp at 5800 RPM
100 hp at 5800 RPM100 hp at 5800 RPM
PROPELLER Pipistrel VARIO
Variable pitchVariable pitch
SIZES  

wing span 10,71 m 10,71 m10,71 m
length 6,5 m 6,5 m6,5 m
height 1,85 1,851,85
wing area 9,51 m2 9,51 m29,51 m2
rudder area 1,1 m2 1,1 m21,1 m2
tail area 1,08 m2 1,08 m21,08 m2
aspect ratio 11,3 11,311,3
positive flaps 9 deg, 19 deg  9 deg, 19 deg9 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 kg289 kg
max take off weight (MTOW) 472.5 kg
472.5 kg
600 kg
fuel tanks capacity 2 x 50 l 2 x 50 l2 x 50 l
useful fuel 2 x 47 l 2 x 47 l2 x 47 l
PERFORMANCES DATA for TOM 472.5 kgDATA for TOM 600 kg
stall with flaps 64 km/h 64 km/h74 km/h
stall without flaps 79 km/h 79 km/h84 km/h
cruising speed (75% power) 246 km/h 273 km/h264 km/h
max. horizontal speed 264 km/h 283 km/h275 km/h
VNE 302 km/h 302 km/h302 km/h
max speed with airbrakes
205 km/h 205 km/h205 km/h
max speed with flaps
130 km/h 130 km/h130 km/h
turbulence penetration speed Vb
250 km/h 250 km/h250 km/h
best climb speed 140 km/h 140 km/h148 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/h123 km/h
best glide 1:17 1:15 1:15
take off run
140 m  95 m140 m
take off over 15 m obstacle 225 m 175 m230 m
service ceiling
6200 m  6800 m5800 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/hour18.0 l/hour
endurance 6,9 hours  5,3 hours5.3 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 1.875minumum 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.

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