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Sec. 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]


Previous: Sec. 29.177 - Static directional stability.
Next: Sec. 29.231 - General.

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