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General| Crew | 1 |
|---|---|
| Capacity | 1 passenger |
| Seats | 2 |
| Manufacturer | Evektor |
| Engine | Rotax 912ULS, 100 hp (75 kW) |
| Maximum speed | 120 kn |
Details airspeed limitations and operational significances.
Details engine model, manufacturer, power ratings, and operating parameters.
Lists empty weight, max take-off, landing, fuel, and baggage weights.
Specifies the empty aircraft CG position and operating CG range.
Specifies operations are limited to Daytime VFR; IFR and icing are prohibited.
Details procedures for engine failure during take-off run, take-off, and in flight.
Outlines the procedure for attempting an engine restart during flight.
Provides procedures for fire on the ground, during take-off roll, and in flight.
Lists steps for emergency landings, including trimming and fuel shut-off.
Details procedures for precautionary landings due to disorientation or hazards.
Details the vital pre-flight inspection procedure recommended by the manufacturer.
Covers cockpit checks, engine starting, taxiing, take-off, climb, cruise, descent, landing, and engine shutdown.
Details stall speeds for various flap settings, power settings, and flight conditions.
Provides take-off distances for concrete and short grass runways.
Lists landing distances for concrete and short grass runways.
Graph showing rate of climb versus airspeed for different altitudes.
Graph showing horizontal speeds versus engine speed at different altitudes.
Provides a table for maximum permitted crew weight with baggage and fuel loads.
Details the standard ROTAX 912 UL engine and propeller specifications.
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