1. Regulations
  2. title 14
  3. chapter I
  4. part 29
  5. subpart D
  6. subjgrp 257
  7. § 29.691

View all text of Subjgrp 257 [§ 29.671 - § 29.695]

§ 29.691 - Autorotation control mechanism.

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

AUTHORITY: 49 U.S.C. 106(f), 106(g), 40113, 44701-44702, 44704.

SOURCE: Docket No. 5084, 29 FR 16150, Dec. 3, 1964, unless otherwise noted.

CITE AS: 14 CFR 29.691