§ 29.181. Dynamic stability: Category A rotorcraft.
34 words·~1 min read·
/us/cfr/t14/s§ 29.181·A research copy — for the controlling text, always check the official state or federal source. Not legal advice.
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]