Characteristics
Engine ROTAX 912 ULS 100hp 5800 rpm
Fuel tank capacity: 68 litres (18 Gallons)
Propeller: Wooden twin blade, diameter 183 cm (72 in)
 
DIMENSIONS
WING SPAN 935 cm (368 in)
LENGTH 640 cm (252 in)
HEIGHT 203 cm (80 in)
HEIGHT WITH AL.BW 29" AND EXTENDED L. GEAR 223 cm (87.8 in)
WING SURFACE AREA 14,2 m2 (152.85 sq ft)
WING CHORD 156 cm (61.4 in)
CABIN WIDTH 60 cm (23.6 in)
UNDERCARRIAGE WIDTH 182 cm (71.6 in)
UNDERCARRIAGE WIDTH WITH EXTENDED L. GEAR 200 cm (78.7 in)
 
WEIGHTS
MAX TAKE-OFF WEIGHT 472.5 kg (1041 lbs) - 560 kg (1234 lbs) [depends on the market]
WEIGHT UNLOADED ULM-LSA 270 kg (594 lbs)
EFFECTIVE LOAD CAPACITY 202.5 kg (446 lbs) - 290 kg (638.7 lbs)
MAX WING LOADING 472.5kg VERSION 33 kg/mq (7 lb/sqft)
MAX WING LOADING 560kg VERSION 39 kg/mq (8 lb/sqft)
LOAD FACTOR +6 - 3 G
 
 
Performances
Vne 205 km/h (128 mph)
Max speed s.l. 175 km/h (109 mph)
Cruising speed 75% 145 km/h (90 mph)
Climb rate 5 m/s (984 ft/m)
Stall speed with full flaps 55 km/h (34 mph)
Max ceiling 4100 m (13400 ft)
Range 65 % 650 km (404 mi)
Required take-off space <80 m (<260 ft) [depending on the surface]
Required landing space <70 m (<228 ft) [depending on the surface]
Cross wind component (max.) 33 km/h (20 mph)
 
 
 
 

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