| Virus SW (Short Wing) |
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- 10.7 m (35' 1½") wingspan
- Glide ratio 20:1
- 120 to 125 knot cruise with Rotax 912
- 3.6 gph at 120 knots
- Up to 7.5 hours endurance
- Available in tail dragger or nosewheel configuration
- LSA Version supplied with 3 blade fixed pitch propeller
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- Great for thermalling, slope soaring or just having fun
- Fantastic touring aircraft
- Feathering propeller (not on LSA)
- Large luggage capacity
- Easy to hangar being 35 ft wingspan
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The Virus SW 912 is identical to the Virus except it's wingspan, at 10.7 m (35' 1½"), is smaller than the standard Virus making this aircraft easier to hanger. Performance is slightly up with the aircraft flying faster but the compromise is a reduced glide ratio.
The Virus SW is equipped with steerable nose wheel or tailwheel as an option.
The Virus SW is a very capable touring aircraft. With long range tanks it has 7 hours endurance at 120 knots and with a higher wing loading it cuts through heavy turbulence with ease.
From A-to-B the Virus SW is certainly an efficient and economical aircraft, but dont let this fool you - slope soaring is a breeze in the Virus SW. The fast roll rate and excellent visibility make it a substantial wave or slope soaring aircraft and with a glide ratio of 20:1 it can still be thermaled. Overall, the Virus SW is an extremely nice package which will fit in most hangars because of the shorter wingspan.


| MODEL |
VIRUS 912 SW
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| ENGINE ROTAX |
ROTAX 912 UL2 |
| max power(with 2 carb.) |
80 hp at 5500 rpm |
| PROPELLER |
Pipistrel VARIO |
| SIZES |
| wing span |
10.7 m
35' 1½" |
| length |
6.4 m
20.99 ft |
| height |
2.00 m
6.56 ft |
| wing area |
TBA m2
TBA ft2 |
| rudder area |
1.1 m2
11.84 ft2 |
| tail area |
1.63 m2
17.55 ft2 |
| aspect ratio |
13.1 |
| positive flaps |
10 deg. 18 deg |
| negative flaps |
5 deg |
| center of gravity |
25% - 37% |
| WEIGHTS |
| empty weight |
285 kg
628 pounds |
| max take off weight (MTOW) |
560 kg
1235 Pounds |
| fuel tanks capacity |
2 x 30 l or 2 x 50 l
2x7.93 or 2x13.2 US G
2x6.6 or 2x11 Imp G |
| useful fuel |
57 litres or 97 litres |
| PERFORMANCES |
| stall with flaps |
64 km/h
34.6 Knots
39.8 MPH |
| stall without flaps |
74 km/h
39.9 Knots
46.0 MPH |
| cruising speed |
225 km/h
121.5 Knots
139.8 MPH |
| max speed with airbrakes out |
160 km/h
86.4 Knots
99.4 MPH |
| max speed with flaps down |
130 km/h
70.2 Knots
80.8 MPH |
| manoeuvring speed |
135 km/h
73.0 Knots
83.9 MPH |
| max. horizontal speed |
238 km/h
128.5 Knots
147.9 MPH |
| VNE |
250 km/h
135.0 Knots
155 MPH |
| best climb speed |
130 km/h
70.2 Knots
80.8 MPH |
| max climb rate (MTOW) |
6.2 m/sec
1220 fpm |
| climb rate at 140 km/h |
7.0 m/sec
1378 fpm |
| min.sink speed |
96 km/h
48.6 Knots
60.0 MPH |
| min.sink (prop. 90 deg.) |
1.72 m/sec
338 fpm |
| max. sink with airbrakes |
5.5 m/sec
1082 fpm |
| best glide ratio speed |
110 km/h
59.4 Knots
68.4 MPH |
| best glide (prop. 90 deg.) |
1:20 |
| glide at 150 km/h (prop 90 deg) |
1:13.5 |
| take off run MTOW |
96 m
315 ft |
| take off over 15 m MTOW |
155 m
508 ft |
| service ceiling MTOW |
8100 m
26500 ft |
| 45°- 45° roll time |
3.1 sec |
| endurance |
5.6 hours |
| range distance |
1260 km
680 N Miles |
| max load factor permitted (x1.8) |
+4g - 2g |
| max load factor tested |
+ 7.2g - 7.2g |
| fuel consumption at cruise speed |
9.7 l/hour |
| ERGONOMICS |
| cabin width |
110 cm
43 1/3 inches |
| Max Pilot Height |
+195 cm
+ 6' 4" |
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