§27.629 Flutter.

14 CFR 27 · Design and Construction · General · at 27-51 (current)

Text in force at 27-51: from 27-26, effective 5 Apr 1990.

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

55 FR 8000 · Source

Version history

Version	Effective	Published
27-26	5 Apr 1990	55 FR 8000
27-0	1 Feb 1965	29 FR 15695

No aircraft in the dataset reference this section.

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