1. Regulations
  2. title 14
  3. chapter I
  4. part 27
  5. subpart C
  6. subjgrp 167
  7. § 27.341

View all text of Subjgrp 167 [§ 27.321 - § 27.361]

§ 27.341 - Gust loads.

The rotorcraft must be designed to withstand, at each critical airspeed including hovering, the loads resulting from a vertical gust of 30 feet per second.

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

SOURCE: Docket No. 5074, 29 FR 15695, Nov. 24, 1964, unless otherwise noted.

CITE AS: 14 CFR 27.341