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CS 27.629  Flutter

ED Decision 2003/15/RM

Each aerodynamic surface of the rotorcraft must be free from flutter under each appropriate speed and power condition.
Details
Source-Title: CS 27.629 Flutter View latest amendments
Erulesid: ERULES-1963177438-4939 Compare versions
Domain: Initial airworthiness
Amendedby: Initial issue
Applicabilitydate: 14 November, 2003
Entryintoforcedate: 14 November, 2003
Regulatorysource: ED Decision 2003/15/RM Navigate
Regulatorysubject: CS-27
Typeofcontent: CS (Certification specification)
Origin: EASA
Category: EAR