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Specification
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Performance
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Wing span
Wing area
Length
Cabin width
Optional cabin width
Height
Empty weight
Maximum take of weight
Load factors
Glide ratio
Luggage capacity
Fuel tank capacity
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8,10 m
9,48 m2
5,98 m
1,04 m
1,18 m
2,34 m
264 êã
450 kg
+6g/-3g
10
15 kg
65 l
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Engine
Never exceed speed
Maximum level speed
Cruising speed
Stall speed
Rate of climb
Service ceiling
Take of roll
Take of distance
Landing roll
Landing distance
Average fuel consumption
Range
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Rotax 912 ULS
100 HP
270 km/h
245 km/h
200 km/h
65 km/h
8,0 m/s
5000 m
100 m
200 m
90 m
300 m
14 l/h
750 km
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Rotax 912
80 H
270 km/h
225 km/h
180 km/h
65 km/h
5,5 m/s
5000 m
145 m
280 m
90 m
300 m
11 l/h
750 km
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All performances quoted at 450 kg a.u.w
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