§27.673 Primary flight control.

14 CFR 27 · Design and Construction · Control Systems · at 27-51 (current)

Text in force at 27-51: from 27-21, effective 6 Dec 1984.

[Primary flight controls are those used by the pilot for immediate control of pitch, roll, yaw, and vertical motion of the rotorcraft.]

49 FR 44434 · Source

Version history

Version	Effective	Published
27-21	6 Dec 1984	49 FR 44434

No aircraft in the dataset reference this section.

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