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VS (stall speed): 36 kts | 42 mph | 68 kph
VC (cruise speed): 72 kts | 83 mph | 134 kph
VNE (never exceed speed) : 79 kts | 91 mph | 146 kph
Climb ratio: 655 ft/min | 3 m/s
Glide ratio: 7:1

Takeoff distance over 50ft (15m) obstacle: 621 ft | 189 m
Landing distance over 50ft (15m) obstacle: 905 ft | 276 m

MEW (manufacturers empty weight): 289 kg | 638 lbs
MTOW (maximum takeoff weight): 499 kg | 1100 lbs

Engine: Rotax R912UL
Fuel consumption: 12 - 15

The Quicksilver GT-500 development program was started with the goal of producing the best performing Quicksilver ever. Quicksilver?s aim was to design an aircraft that would change the category of ultralight & provide general aviation with the entry level aircraft it desperately needed. The focus was on more speed, better aerodynamics, and a greater range.

Photo and text from: http://www.quicksilveraircraft.com/gt500.htm


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