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Details airspeed limitations and their operational significance at MTOW.
Specifies limitations for the engine, including RPM, temperatures, pressure, and fuel.
Defines the maximum take-off, landing, taxi, and baggage weights.
Provides datum references and center of gravity limits for safe operation.
Details procedures for engine fire, failure during take-off, in flight, and emergency landing.
Outlines procedures for engine fires and electrical fires.
Describes the procedure for recovering from an unintentional spin.
Outlines the steps for performing a precautionary landing.
Provides detailed checklists for pre-flight, start-up, and flight phases.
Contains tables and diagrams for airspeed calibration, engine performance, and climb/take-off data.
Details stall speeds under various conditions like bank angle, load factor, and flap settings.
Provides data for take-off run and distance, including factors for grass and runway conditions.
Details take-off and cruise climb performance based on altitude and ISA delta.
Provides landing distance data with flaps in landing position, including correction factors.
Specifies forward and rear limits for CG and shows the centrogram.
Details how to calculate mass and balance before each flight.
Describes the panel-mounted avionics, including PFD, Audio Panel, GPS, and EMS.
Describes the Rotax 914 F engine, cooling, lubrication, and controls.
Details the fuel tanks, selector, pumps, filters, and quantity indication.
| Manufacturer | Sonaca Aircraft |
|---|---|
| Model | S201 |
| Seating Capacity | 2 |
| Engine Power | 100 hp |
| Max Takeoff Weight | 750 kg |
| Wingspan | 9.15 m |
| Cruise Speed | 220 km/h |
| Maximum Speed | 135 knots |
| Stall Speed | 45 knots |
| Rate of Climb | 700 ft/min (3.6 m/s) |
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