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| SPECIFICATIONS | |||
| AIRFRAME | POWER PLANT | ||
| Empty
Weight Payload * Wing Area Fabric Kit Assembly |
340 lbs. 500 lbs. 500 sq. ft. 1.1 oz. soar coat 20 - 30 hours |
Rotax
Engine Horsepower Fuel Capacity |
582 -Twin Cylinder,
two cycle, water cooled, oil injection 65 hp 10 gallons |
| PERFORMANCE | |||
| Max. Speed Stall Speed Cruise Speed Glide Ratio Descent Rate/Max. |
3 mph Virtually stall resistant 30 mph 3.47:1 10 ft./sec |
Fuel
Consumption Rate of Climb ** Takeoff Roll Landing Roll Ceiling |
3 gal./hour 600 - 800 ft./min. 150 - 500 ft. 100 ft. 10,500 ft. |
* Payload is defined as combined total weight of pilot, passenger (if two-place model) and accessories. |
| ** Rate of Climb will vary depending on payload and atmospheric conditions. |
| Specifications and options are
subject to change without notice. |
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