Do you have a question about the ELA Aviacion ELA 10-Eclipse and is the answer not in the manual?
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.
| 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 |
Loading...