SPECIFICATIONS 

Certification base	SLSA by FAA (USA)
Engine	Rotax 912 ULS Rotax 912 iS UL Power UL 260iSA
Horsepower	100 HP
Propeller	​MT / DUC
Fuel Capacity	Max: 23.7 US gal (90 L) Usable: 22,4 US gal (85 L)

Length	22 ft
Wingspan (with winglet)	28 ft
MTOW	LSA: 1,320 lb (600 kg)
Cockpit Seats	2
Cockpit Width/Hight	46/40 in
Fuel Consumption	4.9 - 7.1 gal/hr

Va (Maneuvering speed)	110 kts	Service Ceiling	12,000 ft
Vhmax (max horizontal speed)	130 kts	Takeoff Distance	394 - 427 ft
Vne (never exceed speed)	151 kts	Landing Distance	492 - 656 ft
Vcr (Cruising speed at 75% power)	116 - 122 kts	Cross Wind Landing	15 kts
Stall Speed (with flap)	45 kts	Range	497 - 633 miles

* Information purposes only. Please refer to the POH and other manuals of the specific aircraft. 

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