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Manufacturer | ELA Aviacion |
---|---|
Model | ELA 10-Eclipse |
Type | Gyroplane |
Category | Light Sport Aircraft |
Seats | 2 |
Engine | Rotax 912 ULS |
Engine Power | 100 hp (75 kW) |
Empty Weight | 250 kg (551 lb) |
Height | 2.7 m (8 ft 10 in) |
Cruise Speed | 160 km/h (99 mph, 86 kn) |
Fuel Capacity | 100 L (26 US gal; 22 imp gal) |
Rate of Climb | 3 m/s (590 ft/min) |
Takeoff Distance | 50 m (164 ft) |
Landing Distance | 10 m (33 ft) |
Powerplant | Rotax 912 ULS |
Max Takeoff Weight | 600 kg |
Gross weight | 600 kg |
Specifies engine manufacturer, power, speed, cooling, and electrical system details.
Defines the Never Exceed (Vne) and Turbulence (Vb) speeds for the aircraft.
Prohibits all aerobatic and low-G manoeuvres due to safety risks.
Specifies maximum take-off weight (MTOW) and load factors for different engine variants.
Details the comprehensive pre-flight checks required for safe aircraft operation.
Provides step-by-step instructions for safely starting the aircraft's engine.
Outlines procedures for safe taxiing, including speed, steering, and caution points.
Covers essential checks before initiating the take-off run, including ignition and engine parameters.
Explains the procedure for pre-rotating the rotor system before take-off.
Guides on the take-off process, including stick position, rotor speed, and acceleration.
Details the steps for a safe landing, including approach, circuit entry, and flares.
Instructs on actions to take in case of engine failure during the take-off run.
Outlines procedures for engine failure occurring below 150 ft during take-off.
Details procedures for engine failure occurring above 150 ft during take-off.
Provides guidance for engine failure encountered during flight.