1. Regulations
  2. title 14
  3. chapter I
  4. part 29
  5. subpart B
  6. subjgrp 244
  7. § 29.181

View all text of Subjgrp 244 [§ 29.141 - § 29.181]

§ 29.181 - Dynamic stability: Category A rotorcraft.

Any short-period oscillation occurring at any speed from VY to VNE must be positively damped with the primary flight controls free and in a fixed position.

[Amdt. 29-24, 49 FR 44437, Nov. 6, 1984]

AUTHORITY: 49 U.S.C. 106(f), 106(g), 40113, 44701-44702, 44704.

SOURCE: Docket No. 5084, 29 FR 16150, Dec. 3, 1964, unless otherwise noted.

CITE AS: 14 CFR 29.181