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 600 kg
Weight unloaded basic version (with optional light weight program) below 295 kg (649 lbs)
Effective load capacity up to 305 kg (671 lb)
Max wing loading 40 kg/mq (8,2 lb/sqft)
Load factor +6 -3 (tested at 600kg MTOW/ 1320 lbs)
 
 
Performance
VNE (WITH SLATS) 185 km/h (115 mph)
MAX SPEED S.L. (WITH SLATS) 180 kmh ( 112 mph)
Cruising speed 75% 140 km/h (87 mph)
Climb rate 5 mt/s ( 1.000 ft/m)
MINIMUM FLIGHT SPEED WITH FULL FLAPS (MTOW) 34 km/h (21 mph)
MINIMUM FLIGHT SPEED WITH FULL FLAPS (SINGLE PILOT) 27 km/h (17 mph)
Max ceiling > 4800 m (15.750 ft)
Range 65% 520 km (323 Nm)
Required take off space (single pilot) < 28 mt ( 90 ft)
Required take off space (MTOW) 50 mt (160 ft)
Required landing space (single pilot) < 16 mt (51 ft)
Required landing space (MTOW) < 33 mt (105 ft)
 
 
Photo Gallery
Photos
 


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