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CS 22.1937  Vibration load limit test

ED Decision 2003/13/RM

The vibration load limits of each metal hub and blade, and of each primary load-carrying metal component of non-metallic blades, must be determined for all reasonably foreseeable vibration load patterns.
Details
Source-Title: CS 22.1937 Vibration load limit test View latest amendments
Erulesid: ERULES-1963177438-5235 Compare versions
Domain: Initial airworthiness
Amendedby: Initial issue
Applicabilitydate: 14 November, 2003
Entryintoforcedate: 14 November, 2003
Regulatorysource: ED Decision 2003/13/RM Navigate
Regulatorysubject: CS-22
Typeofcontent: CS (Certification specification)
Origin: EASA
Category: EAR