Experimental, N-numbered (N2250Y)
Quicksilver MXL II Sport
AIRCRAFT:
Engine................................Rotax 582
No. Cylinders.................................2
Horsepower...............................64 hp
Length...................................210 in
Height...................................112 in
Wingspan.............................32.75 ft
Seats.........................................2
Minimum flight crew.........................1
Empty Weight.........................330 lbs
w/ added features & fuel......~500 lbs
Fuel capacity..........................12 gals
PERFORMANCE:
Takeoff distance, ground roll..............121 ft
Takeoff distance, 50 ft obstacle..........260 ft
Rate of climb............................1145 fpm
Landing distance, 50 ft obstacle...........300 ft
Glide Ratio......................................5:1
Airspeed....................................75 mph