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Sec. 27.399 - Dual control system.

Each dual primary flight control system must be designed to withstand the loads that result when pilot forces of 0.75 times those obtained under §27.395 are applied --

(a) In opposition; and

(b) In the same direction.

Previous: Sec. 27.397 - Limit pilot forces and torques.
Next: Sec. 27.411 - Ground clearance: tail rotor guard.

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