Characteristics
Engine Rotax 912 ULS 100hp
Fuel tank capacity 68lt (18 Gallons - Optional 30 Gallons)
Propeller Two blade wooden prop 183cm (72")
 
Dimensions
Wing span 900cm (354,3")
Length 684cm (269,3")
Height 225cm with Alaskan Bw 29" (88,5")
Wing surface area 15,21mq (163,7sq/ft)
Wing chord 169cm (66,5")
Cabin width 69cm (27,1")
Undercarriage width with Al.Bw 26" 226cm (88,9")
 
Weights
Max take off weight from 472,5 kg (ULM version) to 600 kg (LSA version)
Weight unloaded ULM-LSA basic version (with optional light weight program) from 339 kg (745 lbs)
Effective load capacity up to 286 kg (629 lb)
Max wing loading ULM Version 31 kg/mq (6.38 lb/sqft)
Max wing loading LSA VERSION 40 kg/mq (8.2 lb/sqft)
Load factor +6 -3 (tested at 680kg MTOW/ 1500 lbs)
 
 
Performance
VNE (WITH SLATS) 185 km/h (115 mph)
MAX SPEED S.L. (WITH SLATS) 180 kmh ( 112 mph)
Cruising speed 75% 145 km/h (90 mph)
Climb rate 5 mt/s ( 1.000 ft/m)
MINIMUM FLIGHT SPEED WITH FULL FLAPS (MTOW) 37 km/h (23 mph)
MINIMUM FLIGHT SPEED WITH FULL FLAPS (SINGLE PILOT) 29 km/h (18 mph)
Max ceiling > 4800 m (15.750 ft)
Range 65% 560 km (348 Nm)
Required take off space (single pilot) < 35 mt ( 115 ft)
Required take off space (MTOW) 57 mt (188 ft)
Required landing space (single pilot) < 18 mt (58 ft)
Required landing space (MTOW) < 35 mt (115 ft)
 
 
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