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CS 23.2230 Limit and ultimate loads

Normal-Category Aeroplanes (CS-23) · CS-23 · EAR revision 13 May 2026

IRImplementing rule

CS 23.2230Limit and ultimate loads

(a)Unless special or other factors of safety are necessary to meet the requirements of this Subpart, the applicant must determine:

(1)the limit loads, which are equal to the structural design loads; and

(2)the ultimate loads, which are equal to the limit loads multiplied by a 1.5 factor of safety, unless otherwise provided.

(b)Some strength specifications are specified in terms of ultimate loads only, when permanent detrimental deformation is acceptable.

IR · CS 23.2230 — CS-23 · ED Decision 2017/013/R · CS-23 Easy Access Rules · EAR revision 13 May 2026

AMCAcceptable means of compliance

AMC1 23.2230Limit and ultimate loads

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ASTM F44 F3264 Standard Specification for Normal Category Aeroplanes Certification

6.7 Limit and Ultimate Loads F3114-21 Standard Specification for Structures F3408/F3408M-21 Standard Specification for Aircraft Emergency Parachute Recovery Systems [AMC & GM to CS-23: Issue 4] [AMC & GM to CS-23: Issue 5]

AMC · AMC1 23.2230 — CS-23 · ED Decision 2026/003/R · CS-23 Easy Access Rules · EAR revision 13 May 2026

AMCAcceptable means of compliance

AMC2 23.2230Limit and ultimate loads

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CS-23 Amdt 4

23.301(a) Loads

23.303 Factors of safety

AMC · AMC2 23.2230 — CS-23 · ED Decision 2017/025/R · CS-23 Easy Access Rules · EAR revision 13 May 2026

AMCAcceptable means of compliance

AMC3 23.2230Limit and ultimate loads

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CS VLA Amdt 1 VLA.301 Loads VLA.303 Factors of safety

AMC · AMC3 23.2230 — CS-23 · ED Decision 2017/025/R · CS-23 Easy Access Rules · EAR revision 13 May 2026

All rules in SUBPART C — STRUCTURES

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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