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CS 26.308 Damage tolerance data for existing published repairs to fatigue-critical structure

ED Decision 2020/023/R

Compliance with point 26.308(a) of Part-26 is demonstrated when damage tolerance data is developed in accordance with AMC 20-20A Paragraph 7 and Appendix 3 for each existing published repair to the fatigue-critical structure (FCS) identified in accordance with points 26.306 and 26.307 of Part‑26.

[Issue: 26/3]
Details
Source-Title: CS 26.308 Damage tolerance data for existing published repairs to fatigue-critical structure
Erulesid: ERULES-1963177438-17998 Compare versions
Domain: Additional airworthiness specifications
Amendedby: CS Issue 3
Applicabilitydate: 18 December, 2020
Entryintoforcedate: 18 December, 2020
Regulatorysource: ED Decision 2020/023/R Navigate
Regulatorysubject: Part-26, CS-26
Typeofcontent: CS (Certification specification)
Parentir: 26.308 Damage tolerance data for existing repairs to fatigue-critical structure
Origin: EASA
Category: EAR