MAGNUS AIRCRAFT INC.
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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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For A​vailable aircrafts in inventory click HERE, for video click HERE.

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Hours

M-F: 9am - 5pm EST

Cell

+ 1 (757) 8285486

Email

office.usa@magnus-aircraft.com
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