Navigate / EASA
Ask question Discover more Add to collection

AMC E 520(a)  Strength - High Cycle Fatigue

ED Decision 2007/015/R

In order to minimise the adverse consequences of Failures due to unpredicted high cycle fatigue it is recommended that, normally, the relative fatigue strengths of the blade/disc are graded such that they lie in the ascending order: blade form, blade root, disc blade attachment, disc rim.

[Amdt. No.: E/1]
Details
Source-Title: AMC E 520(a) Strength - High Cycle Fatigue
Erulesid: ERULES-1963177438-8940 Compare versions
Domain: Initial airworthiness
Amendedby: Amendment 1
Applicabilitydate: 10 December, 2007
Entryintoforcedate: 10 December, 2007
Regulatorysource: ED Decision 2007/015/R Navigate
Regulatorysubject: CS-E
Typeofcontent: AMC to CS (Acceptable means of compliance to certification specification)
Parentir: CS-E 520 Strength
Origin: EASA
Category: EAR