Model                         Rotax 582
No. Cylinders                         2
Displacement                     580 CC
Horsepower                    64.5 H.P.
Recommended T.B.O.              300 Hrs
Propeller                  CARBON FIBER
Length                           228 in
Height                       7 ft 10 in
Wingspan                     32 ft 9 in
Wing Area                    180 sq. ft
Wing Loading                 21.5 lb/hp
Seats                                 2
Minimum Flight Crew                   1
Empty Weight                    465 lbs
Useful Load                     935 lbs
Payload W/Full Fuel             839 lbs
Max Take-off Weight            1400 lbs
Fuel Capacity (Standard)         16 gal
Structural rating               +6 -4 G

Takeoff Distance, Ground Roll    135 ft
Takeoff Distance, 50 Ft Obstacle 400 ft
Rate of Climb                   650 fpm
Max Level Speed, Sea Level       68 mph
Landing Distance, 50 Ft Obstacle 225 ft
Landing Distance, Ground Roll     60 ft
Glide Ratio                    5.00 : 1
Minimum Sink Rate               575 fpm

At 55% Power (rpm/mph)          5000/45
At 65% Power (rpm/mph)          5300/50
At 75% Power (rpm/mph)          5600/58
At 100% Power (rpm/mph)         6500/68

At 55% Power (gph/mi)            4.1/95
At 65% Power (gph/mi)            4.8/90
At 75% Power (gph/mi)            5.6/85
At 100% Power (gph/mi)           7.4/77

Vx (Best angle of climb)         38 mph
Vy (Best rate of climb)          40 mph
Va (Design maneuvering)          68 mph
Vne (Never Exceed)               94 mph
Vs1 (Stall, Power off)           27 mph
VsO (Stall, Flaps down, power off)  n/a
Landing Approach Speed           40 mph
 

All specifications are based on manufacturers calculations and are subject to change. All performance figures are based at gross weight unless stated otherwise on a standard day, standard atmosphere, at sea level unless otherwise noted. The performance shown reflect this aircrafts maximum potential

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