§29.629. Flutter and divergence.
14 C.F.R. § 29.629
Each aerodynamic surface of the rotorcraft must be free from flutter and divergence under each appropriate speed and power condition.
Notes, amendments, and revision history
Amendments
[Doc. No. 28008, 61 FR 21907, May 10, 1996]
Authority
Authority: 49 U.S.C. 106(f), 106(g), 40113, 44701-44702, 44704.
Source
Source: Docket No. 5084, 29 FR 16150, Dec. 3, 1964, unless otherwise noted.
Amendments
[Doc. No. 28008, 61 FR 21907, May 10, 1996]