CS 29.629 Flutter and divergence

Navigate / EASA

Ask question Discover more Add to collection

ED Decision 2003/16/RM

Each aerodynamic surface of the rotorcraft must be free from flutter and divergence under each appropriate speed and power condition.

Source-Title: CS 29.629 Flutter and divergence

Erulesid: ERULES-1963177438-5549 Compare versions

Domain: Initial airworthiness

Amendedby: Initial issue

Applicabilitydate: 14 November, 2003

Entryintoforcedate: 14 November, 2003

Regulatorysource: ED Decision 2003/16/RM Navigate

Regulatorysubject: CS-29

Typeofcontent: CS (Certification specification)

Origin: EASA

Category: EAR