FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 27 > Section 341 - Gust loads
section 27.339 |
section 27.351

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.
  
Current page: FARs > Part 27 > Section 341 - Gust loads
section 27.339 |
section 27.351

page stats: viewed 1072 unique times - last change 25-Jan-2005
» DOWNLOADING (PARTS OF) THIS WEBSITE AUTOMATICALLY IS NOT ALLOWED! «
THIS IS NO OFFICIAL SOURCE --
[DISCLAIMER]
[FAA WEBSITE]
See also:
AIM | ATC | FSS | NOTAMS | PCG | |