VIRUS UL Aircraft
912 & 912SW and SW 100
ENGINE ROTAX
ROTAX 912 UL
max. Horizontal speed
240 (249) km/h
max. power
80 hp at 5800 rpm
manoevring speed
141 km/h
ROTAX SW 100
best climb speed
130 (120) km/h
100 hp at 5800
max climb rate (450 kg)
6,2 (6,1) m/sec
climb rate at 140 km/h
5,9 (5,5) m/sec
PROPELLER
Pipistrel VARIO
Min. sink speed
96 (108) km/h
min sink*
1,8 (2,4) m/sec
SIZES
best glide ratio speed
110 (120) km/h
wing span
12,46 (10,40)m
best glide*
1:24 (1:17)
Wing span SW 100
10.70 m
take off run (450 kg)
90 (140) m
length
6,50 m
take off over 15 m
167 (225) m
height
1,85
service ceiling (450 kg)
8100 (6200) m
wing area
11,0 (9,1) m²
45° - 45° roll time
3,1 (1,6) sec
aspect ratio
13,1 (11,3)
fuel consum @cruis. speed
9,5 (12,5) l/hour
positive flaps
9 deg, 18 deg
endurance
5,7 (4,3) hours
negative flaps
5 deg
range distance
1280 (1050) km
Max. load factor (x1,8)
+4 g-2 g
WEIGHTS
Max. load factor tested
+7,2 g -7,2 g
max. Weight (MTOW)
450kg/472,5kg/544kg
fuel tanks capacity
2 x 30 l /2 x 50 l
* (prop. 90 deg)
PERFORMANCE
stall with flaps
64 (67) km/h
cruising speed (75%)
225 (245) km/h
cruising speed SW 100 (75%)
273 km/h
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