TECHNICAL DATA
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Max take off weight |
600 kg (1,323 lbs.) |
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Empty weight |
290 kg (640 lbs.) |
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Fuel quantity |
2 x 50 L (27 US Gallons) |
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Max fuel load |
76 kg (168 lbs.) |
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Max payload (including fuel) |
310 kg (684 lbs.) |
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Load factors (at weight 540 kg) |
+6 –3 G |
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Load factors (at weight 600 kg) |
+5.4 –2.7 G |
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Wing span |
10,830 mm (35 ft 7 in.) |
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Fuselage length |
6,720 mm (22 ft 1 in.) |
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Fuselage max width |
760 mm (30 in.) |
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Fuselage height (fuselage horizontal) |
2,150 mm (85 in.) |
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POWER PLANT |
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Make and model |
Jabiru 2200(Rotax 912 ULS) |
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PERFORMANCE |
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Max horizontal speed (540 kg) gnd. level |
190 km/hr (102 kt.) |
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Cruise speed 75% power |
170 km/hr (92 kt.) |
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Most economical speed 40% power |
148 km/hr (80 kt.) |
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Stall speed (540 kg) clean |
80 km/hr (43 kt.) |
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Stall speed (540 kg) flaps and gear |
70 km/hr (38 kt.) |
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Max climb rate (540 kg) |
5 m/s (990 ft/min.) |
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Max maneuver speed (540 kg) |
213 km/hr (115 kt.) |
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Speed never exceed (approx.) |
282 km/hr (152 kt.) |
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Endurance cruise speed 65% |
7.6 hours without reserve |
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Range at cruise speed 65% |
1,200 km (650 nautical miles) |
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Mileage |
8 liter/100 km (29 mpg) |
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Endurance most economical speed |
12 hours without reserve. |
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Range at most economical speed |
1,700 km (918 nautical miles) |
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Mileage |
6 liter/100 km (39 mpg) |
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