CS-23 — Certification Specifications for Normal-Category Aeroplanes

Section 01: Organizations & Authorities

Definition

The EASA Certification Specifications for normal-category aeroplanes, harmonized with FAA 14 CFR Part 23. CS-23 Amendment 5 adopted the restructured performance-based approach matching the FAA's Part 23 Amendment 64, using high-level safety objectives with detailed compliance methods provided through referenced consensus standards. CS-23 covers aeroplanes with a maximum seating configuration of 19 passengers and a maximum certificated takeoff mass of 8,618 kg (19,000 lb).

Primary Sources

EASA CS-23 — Certification Specifications and Acceptable Means of Compliance for Normal-Category AeroplanesEASA

EASA airworthiness standards for normal-category aeroplanes.

Related Terms

European Union Aviation Safety Agency (EASA)14 CFR Part 23 — Airworthiness Standards: Normal Category Airplanes

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