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Sec. 27.171 - Stability: general.

The rotorcraft must be able to be flown, without undue pilot fatigue or strain, in any normal maneuver for a period of time as long as that expected in normal operation. At least three landings and takeoffs must be made during this demonstration.

Previous: Sec. 27.161 - Trim control.
Next: Sec. 27.173 - Static longitudinal stability.

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