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PERFORMANCE  
Cruise speed 130 mph / 5200 rpm
Maximum speed 137 mph
Stall speed - Full Flaps 44 mph
Stall speed - No Flaps 51 mph
Rate of climb 1.050 fpm
Glide ratio 10:1
Take off Roll Distance 510 ft*
Take off Distance
730 ft*
Landing Roll Distance 270 ft*
Landing Distance 760 ft**
Loading +4 G's, -2 G's
Maximum Range 857 sm / 745 nm
Maximum Endurance 9.5 hrs at 4000 rpm
Fuel Consumption 2.3 gph at 4000 rpm
Powerplant Rotax 912 UL-S, 100 hp


DIMENSIONS
 
Wingspan 30'6"
Overall length 21'3"
Height 7'5"
Wing area 118 sq ft
Cockpit width 46.8"
Main gear width 6'9"
Useable fuel capacity 21 gallons / 80l
Total fuel capacity 22 gallons / 84l


VSPEED MPH/KTS
 
VA Maneuvering speed 108 / 94
VAPPROACH Approach airspeed 75 / 65
VNO Maximum airspeed in turbulence 123 / 107
VFE Speed range, flaps extended 44-81 / 38-70
VH Maximum speed in level flight 137 / 119
VNE Never exceed speed

155 / 134
VREF 1.3 x Vso
57 / 49
VSO Minimum airspeed

44 / 38 flaps extended (40�)

VS Minimum airspeed

51 / 44 flaps retracted (0�)

VX Best angle of climb

68-75 / 59-65

VY Best rate of climb

85-88 / 73-76



WEIGHT
 
Empty weight 670 lbs
Max. gross weight 1320 lbs
Useful load 650 lbs

 






















* USA LSA Category certified, all weights with basic instruments and lubricant but without fuel
** German LTF-UL 2003, check allowance with national regulation

Values may vary depending on the needs of the regulations in different markets. Measures may vary depending on the specific equipment of each plane. Values are subject to change without notice.
 

 

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