§29.629 Flutter and divergence

CS-29 · Subpart D — Design And Construction · at CS29-12 (current)

Text in force at CS29-12: from CS29-0, effective 14 Nov 2003.

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

ED Decision 2003/016/RM · Source

Version history

Version	Effective	Published
CS29-0	14 Nov 2003	ED Decision 2003/016/RM

No aircraft in the dataset reference this section.

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