Estimated Technical Specification

 

	Category
	UL	LSA/ELSA
Wing span	9,0 m  /  29,5 ft
Height	2,1 m  /  6,9 ft
Length	6,3 m  /  20,6 ft
Wing area	10,0 m2  /  107,6 sqft
Engine 4-stroke Rotax 912	ULS 100 HP
Max. take-off weight incl. BRS	472,5 kg  /  1 040,5 lbs	600 kg  /  1 320 lbs
Max. permissible speed (VNE)	250 km/h  /  135 kn
Economical crusing speed	220 km/h  /  119 kn
Stall speed without flaps	75 km/h  /  40 kn	86 km/h  /  46 kn
Stall speed with flaps	61 km/h  /  33 kn	72 km/h  /  39 kn
Max. climb rate	6 m/s  /  1 181 ft/min	4 m/s  /  787 ft/min
Ceiling	5 000 m  /  16 404 ft
Length Take-off and Landings (23º/30º flaps)	80 – 120 m  /  262 - 394 ft
Fuel capacity	92 l  /  24 US gal
Fuel consumption	15 l  /  4 US gal
Fuel tank volume	70 l  /  18,5 US gal	100 l  /  26,4 US gal