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AMC2 23.2215 Flight load conditions

ED Decision 2026/003/R

CS-23 Amdt 4

23.331 Symmetrical flight conditions

23.333(c) Flight envelope

23.347 Unsymmetrical flight loads

23.349 Rolling conditions

23.351 Yawing conditions

23.367 Unsymmetrical loads due to engine failure


[AMC & GM to CS-23: Issue 5]
Details
Source-Title: AMC2 23.2215 Flight load conditions View latest amendments
Erulesid: ERULES-1963177438-7005 Compare versions
Domain: Initial airworthiness
Amendedby: CS-23 Amendment 6 and AMC ＆ GM to CS-23 Issue 5
Applicabilitydate: 16 April, 2026
Entryintoforcedate: 16 April, 2026
Regulatorysource: ED Decision 2026/003/R Navigate
Regulatorysubject: CS-23
Typeofcontent: AMC to CS (Acceptable means of compliance to certification specification)
Parentir: CS 23.2215 Flight load conditions
Origin: EASA
Category: EAR