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AMC2 23.2240 Structural durability

ED Decision 2017/025/R

CS-23 Amdt 4

23.571 Metallic pressurized cabin structures

23.572 Metallic wing, empennage, and associated structures

23.573 Damage tolerance and fatigue evaluation of structure

23.574 Metallic damage tolerance and fatigue evaluation of commuter category airplanes

23.575 Inspections and other procedures

23.627 Fatigue strength

23.1461 Equipment containing high-energy rotors
Details
Source-Title: AMC2 23.2240 Structural durability View latest amendments
Erulesid: ERULES-1963177438-7016 Compare versions
Domain: Initial airworthiness
Amendedby: CS Issue 1
Applicabilitydate: 21 December, 2017
Entryintoforcedate: 21 December, 2017
Regulatorysource: ED Decision 2017/025/R Navigate
Regulatorysubject: CS-23
Typeofcontent: AMC to CS (Acceptable means of compliance to certification specification)
Parentir: CS 23.2240 Structural durability
Origin: EASA
Category: EAR