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Aircraft Specifications |
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| Estimated, Subject to change | |||||||
| Weight Summary (lbs)
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| Estimated Weight | 710
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| Useful Load | 610 |
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| Maximum Gross Weight | 1,320 |
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| Fuel Capacity (U.S. Gallons) | 24 |
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| (long range tanks optional) | |||||||
| Wing | |||||||
| Wing Span | 30 feet |
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| Wing Area | 125 sq. feet |
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| Wing Chord, constant | 50 inches |
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| Aspect Ratio | 7.2 |
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| Horizontal Tail | |||||||
| Horizontal Tail Span | 10 Feet |
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| Horizontal Tail Area | 25.83 sq. feet |
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| Horizontal Tail Chord, constant | 3 feet (root), 2.16 feet (tip) |
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| Engine | |||||||
| Jabiru 3300 Aircraft Engine | |||||||
| • Displacement 3314 cc | |||||||
| • Engine Weight 178 complete with engine oil, exhaust and starter motor. | |||||||
| • Jabiru, permanently excited single phase generator 20 amps continuous DC output (optional 40 amps) | |||||||
| • Maximum 120 hp @ 3300 RPM | |||||||
| • Maximum continuous 2750 RPM | |||||||
| • Bing constant depression type carburetor or | |||||||
| • MySky carburetor with manual mixture control (optional) | |||||||
| • Fuel: AVGAS 100 LL or unleaded automotive gasoline 91 Octane | |||||||
| • Fuel Burn at 120 KTS: less than 4.5 gal/hr. (with manual carburetor) | |||||||
| Propeller | |||||||
| Sensenich Composite, ground adjustable | |||||||