 |
| SPECIFICATIONS | |||
| AIRFRAME | POWER PLANT | ||
| Empty
Weight Payload * Wing Area Fabric Kit Assembly |
390 lbs. 500 lbs. 500/550 sq. ft. 1.1 oz. soar coat |
Rotax
Engine Horsepower Fuel Capacity |
582 - water
cooled, oil injection 465hp |
| PERFORMANCE | |||
| Max. Speed Stall Speed Cruise Speed Glide Ratio Descent Rate/Max. |
34 mph Virtually stall resistant 26 mph 3.81:1 10 ft./sec 34 mph 6:25/1 8 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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