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Crew |
2 Pilots, Side by Side |
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Propulsion system |
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Engine Type |
Rotax
914 FS1 Turbo-charged
4 cylinder/4 stroke |
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Take-off Power |
115 hp (87.7 kW) |
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Maximum Continuous Power |
100 hp (74.5 kW) |
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Cooling System |
Liquid/Air Cooled |
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Grearbox design |
Gear Box |
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Reduction Ratio |
0.9:1 |
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|
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Wings |
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Span |
75.5 ft (23 m) |
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Area |
201 ft2 (18.7 m2) |
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Aspect Ratio |
28.2 |
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Profile |
HQ41/14.35 |
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Fuselage |
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Length |
27.6 ft (8.42 m) |
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Cockpit Width (outside) |
3.9 ft (1.18 m) |
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Cockpit Width (inside) |
3.8 ft (1.16 m) |
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Cockpit Height |
3.1 ft (0.93 m) |
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Tail Height |
5.9 ft (1.8 m) |
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Empty Weight |
1420 lbs (645 kg) |
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Performance |
|
Takeoff (Sea Level) |
590 ft (180 m) |
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Climb Rate |
800 ft/min (4.0 m/s) |
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Cruise Speed |
140 knots (259 km/h) |
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Vne |
146 knots (270 km/h) |
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Stall Speed |
42 knots (78 km/h) |
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Range (standard fuel tanks) |
590 nm (1090 km) |
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Range (optional fuel tanks) |
780 nm (1450 km) |
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Glide Ratio |
50:1 |
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Minimum Sink Rate |
112 ft/min (0.56 m/s) |
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