Sec. 27.671 — General.
(a) Each control and control system must operate with the ease, smoothness, and positiveness appropriate to its function.
(b) Each element of each flight control system must be designed, or distinctively and permanently marked, to minimize the probability of any incorrect assembly that could result in the malfunction of the system.
NEXT: Sec. 27.672 - Stability augmentation, automatic, and power-operated systems.
PREVIOUS: Sec. 27.663 - Ground resonance prevention means.