FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 29 > Section 629 - Flutter and divergence
section 29.625 |
section 29.631

Each aerodynamic surface of the rotorcraft must be free from flutter and divergence under each appropriate speed and power condition.
[Doc. No. 28008, 61 FR 21907, May 10, 1996]
  
Current page: FARs > Part 29 > Section 629 - Flutter and divergence
section 29.625 |
section 29.631

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