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Aircraft manufactured to Light Sport Aircraft airworthiness standards.
Information about the aircraft manufacturer, Aeropro CZ.
Defines the meaning of warning, caution, and note symbols used.
Details the Rotax 912ULS engine, its power, and cooling.
Describes fuel tank capacity, usable fuel, and specifications.
Identifies and describes the cockpit controls and instruments.
Lists empty weight, max take-off/landing weight, and baggage limits.
Stall speeds for flaps up and flaps down configurations.
The absolute maximum speed the aircraft can safely fly.
Specifies maneuvers like aerobatics and intentional spins are forbidden.
Maximum permitted wind components for take-off and landing.
Defines the acceptable center of gravity limits for the aircraft.
Illustrates the method for calculating the aircraft's center of gravity.
Provides distances for grass and concrete runways.
Specifies cruising speeds at different power settings.
Details fuel consumption based on engine settings.
Step-by-step guide for conducting a thorough pre-flight inspection.
Detailed steps for starting the engine.
Steps for a standard take-off, including pre-takeoff checks.
Steps for landing on base leg, final, and touchdown.
Procedures for engine failure during take-off, after take-off, and in-flight.
Actions to take if fire is detected in the engine compartment or cockpit.
Procedures for encountering icing conditions.
Procedures for refueling, checking/adding oil, and servicing coolant.
Guidance on moving the aircraft and securing it for tie-down.
Explanation of markings on the airspeed indicator.
Describes normal and tailwind takeoff procedures.
Guidance on climbing after takeoff, in cruise, and emergency climbs.
Describes the aircraft's stall behavior.
Describes approach techniques in various weather and wind conditions.
Guidance for smooth touchdowns in various conditions.
Procedure for leveling the aircraft for accurate weighing.
Example calculation to determine the aircraft's center of gravity.
General| Wing span | 8.5 m (27 ft 11 in) |
|---|---|
| Length | 6.7 m (22 ft 0 in) |
| Height | 2.1 m (6 ft 11 in) |
| Empty weight | 320 kg (705 lb) |
| Engine | Rotax 912ULS |
| Power | 73.5 kW (98.6 hp) |
| Seats | 2 |
| Powerplant | 1 × Rotax 912ULS flat-four engine, 73.5 kW (98.6 hp) |
| Stall Speed | 65 km/h |
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