Characterisctics
ENGINE ROTAX 912 ULS 100hp 5800 rpm *Rotax 582 data to be announced soon
FUEL TANK CAPACITY 68 litres (18 Gallons)
PROPELLER Wooden twin blade, diameter 183 cm (72 in)
 
DIMENSIONS
WING SPAN 906 cm (356.7in)
LENGTH 621 cm (243 in)
HEIGHT 201 cm (79 in)
HEIGHT with Al.Bw 26" and extended l. gear 217,5 cm (85.6 in)
WING SURFACE AREA 14,2 m2 (152.85 sq ft)
WING CHORD 156 cm (61.4 in)
CABIN WIDTH 30,5 cm (12 in)
UNDERCARRIAGE WIDTH 178 cm (70 in)
UNDERCARRIAGE WIDTH WITH 26" B.W. 192 cm (75.6 in)
 
WEIGHTS
MAX TAKE-OFF WEIGHT 472,5 kg (1041 lbs) - 560 kg (1234 lbs)
WEIGHT UNLOADED 260 kg (573 lbs)
EFFECTIVE LOAD CAPACITY 212,5 kg (468.5 lbs) - 300 kg (661 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
 
 
PERFORMANCE
Vne 185 km/h (115 mph)
Max speed s.l. 165 km/h (102.5 mph)
Cruising speed 75% 140 km/h (87 mph)
Climb rate 6 m/s (1181,4 ft/m)
Stall speed with full flaps 46 km/h (28,6 mph)
Max ceiling 4100 m (13451 ft)
Range 65 % 590 km (367 mi)
Required take-off space <65 m (<213 ft) depending on surface
Required landing space <55 m (<180 ft)
Cross wind component (max.) 37 km/h (23 mph)
 
 
 
 

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