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SUBPART D — DESIGN AND CONSTRUCTION

Normal-Category Aeroplanes (CS-23) · CS-23 · CS 23.2300 – CS 23.2340

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  1. CS 23.2300 Flight control systems

    The flight control systems are designed to: operate easily, smoothly, and positively enough to allow proper performance of their functions;

    AMC1 23.2300 Flight control systems

    AMC2 23.2300 Flight control systems

    AMC3 23.2300 Flight control systems

  2. CS 23.2305 Landing gear systems

    The landing gear is designed to: provide stable support and control to the aeroplane during surface operation;

    AMC1 23.2305 Landing gear systems

    AMC2 23.2305 Landing gear systems

    AMC3 23.2305 Landing gear systems

  3. CS 23.2310 Buoyancy for seaplanes and amphibians

    Aeroplanes intended for operations on water must: provide buoyancy of 80 % in excess of the buoyancy required to support the maximum weight of the…

    AMC1 23.2310 Buoyancy for seaplanes and amphibians

    AMC2 23.2310 Buoyancy for seaplanes and amphibians

    AMC3 23.2310 Buoyancy for seaplanes and amphibians

  4. CS 23.2315 Means of egress and emergency exits

    With the cabin configured for take-off or landing, the aeroplane is designed to:

    AMC1 23.2315 Means of egress and emergency exits

    AMC2 23.2315 Means of egress and emergency exits

    AMC3 23.2315 Means of egress and emergency exits

  5. CS 23.2320 Occupant physical environment

    The applicant must design the aeroplane to: allow clear communication between the flight crew and passengers;

    AMC1 23.2320 Occupant physical environment

    AMC2 23.2320 Occupant physical environment

    AMC3 23.2320 Occupant physical environment

  6. CS 23.2325 Fire protection

    The aeroplane is designed to minimise the risk of fire initiation due to:

    AMC1 23.2325 Fire protection

    AMC2 23.2325 Fire protection

    AMC3 23.2325 Fire protection

  7. CS 23.2330 Fire protection in designated fire zones

    Flight controls, engine mounts, and other flight structures within or adjacent to designated fire zones must be capable of withstanding the effects of a…

    AMC1 23.2330 Fire protection in designated fire zones

    AMC2 23.2330 Fire protection in designated fire zones

    AMC3 23.2330 Fire protection in designated fire zones

  8. CS 23.2335 Lightning protection

    For operations where the exposure to lightning is likely, the aeroplane must be protected against catastrophic effects of lightning.

    AMC1 23.2335 Lightning protection

    AMC2 23.2335 Lightning protection

    AMC3 23.2335 Lightning protection

  9. CS 23.2340 Design and construction information

    The following design and construction information is established:

    AMC1 23.2340 Design and construction information

    AMC2 23.2340 Design and construction information

    AMC3 23.2340 Design and construction information

Consolidated from the EASA Easy Access Rules (revision 13 May 2026, extracted 17 Aug 2026) for convenience. Not the official publication — verify against the Official Journal of the European Union and the EASA publications before operational use.

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