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Federal regulations · Through 2026-08-25 · Newer source version available

14 CFR 27.691: Autorotation control mechanism.

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Where this section sits in the code
  1. Title 14—Aeronautics and Space
  2. CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
  3. SUBCHAPTER C—AIRCRAFT
  4. PART 27—AIRWORTHINESS STANDARDS: NORMAL CATEGORY ROTORCRAFT
  5. Subpart D—Design and Construction

Each main rotor blade pitch control mechanism must allow rapid entry into autorotation after power failure.

Collected 2026-08-27T02:24:20Z. Source file · JSON

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