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Aircraft dimensions, weight, powerplant, and fuel/oil details.
Description of the aircraft's monoplane, high-wing structure and tail features.
Details on the tricycle type landing gear, including nose and main gear.
Information on installed engines (ROTAX 912 ULS/UL) and associated warnings.
Description of throttle, mixture, master switch, and magneto controls.
Details on the propeller type: 'DUC Helice', 3 or 2 blades.
Explanation of the fuel system, including tanks, filler caps, and fuel pump.
Overview of the 12V electrical system, battery, generator, and components.
Description of cabin access via lateral doors and window usage restrictions.
Details on cabin seating arrangement and upholstery.
Explanation of cabin ventilation system and air scoops.
Description of the cabin heating system using the silencer.
Listing and identification of standard instruments on the panel.
Description of the Y-shaped stick, rudder pedals, and longitudinal trim.
Details on the flaperon system and its control lever operation.
Information on the Pitot tube for pressure supply and static pressure assumption.
Guidelines for baggage storage and securing in the compartment.
Table of stall, normal operating, maneuvering, and never exceeding speeds.
Defines load factors for flaps retracted and extended positions.
Specifies RPM, temperature, and pressure limits for engine operation.
Maximum and minimum take-off and landing weights.
Defines forward and rearward Center of Gravity limits.
Specifies that the airplane is for day-VFR conditions only.
States the aircraft is intended for non-aerobatic operations only.
Maximum permissible cross-wind component for take-off and landing.
Procedures for emergency landing, including speed, flaps, and landing technique.
Steps to take in case of fire on the ground with the engine off.
Procedures for fire on the ground with the engine running.
Actions to take if a fire occurs in flight.
Procedure for dealing with a fire in the cabin.
Instructions for recovering from unintentional spins.
Procedures for engine failure during take-off or immediately after.
Steps for attempting to restart the engine during flight.
Checklist for master switch, magnetos, fuel selector, and controls before flight.
Visual checks of propeller, engine, landing gear, slats, and control surfaces.
Procedures for starting the engine when cold, including notes.
Guidelines for taxying, including power, steering, and crosswind considerations.
Pre-take-off checks including altimeter, trim, flaps, and engine instruments.
Procedures for normal and short take-off, including flap settings and climb speeds.
Details on achieving cruising speed using engine power and RPM.
Recommendations for descent, avoiding idle and using air-box control.
Procedures for approach, landing, flap settings, and airspeed.
Techniques for handling crosswinds during approach and landing.
Procedure for aborting a landing and performing a go-around.
Steps for shutting down the engine, including recommended low RPM running.
Instructions for parking, mooring, and securing the aircraft.
Stall speeds with flaps retracted and extended at maximum weight.
Take-off run distances at various altitudes and conditions.
Landing distances from 15m obstacle and landing run length.
Rate of climb data at different altitudes and full power settings.
Overview of aircraft CG limits and importance of weight and balance.
Procedure to determine CG position and calculate empty weight.
Diagrams illustrating weight and balance calculation parameters.
Table and graph for pilot to compute and verify aircraft weight and balance.
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General