L2 Specifications

A22L2 Ultra Light (450kg)

Flight performance at maximum take-off weight
Max speed Vne 113 kts
Stalling speed (flaps down) 33 kts
Max. range (90 fuel, still air) 590 nm
Max. endurance (90 l fuel) 10 h
Rate of climb (ISA, sea level) >1000 ft/min
Engine: Rotax-912 100 h.p.
Takeoff/landing run (no wind) 105/135 m
Wing span 9.55 m
Length 6.23 m
Height 2.4 m
Wing area 12.62 m2
Maximum take-off weight 450 kg
Empty weight 264 kg
Loads +4 / −2

 

Dimensions – subject to specification (wheel/tyre and propellor type)

 

A-22LS