FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 25 > Section 581 - Lightning protection
section 25.571 |
section 25.601

(a) The airplane must be protected against catastrophic effects from lightning.
(b) For metallic components, compliance with paragraph (a) of this section may be shown by --
(1) Bonding the components properly to the airframe; or
(2) Designing the components so that a strike will not endanger the airplane.
(c) For nonmetallic components, compliance with paragraph (a) of this section may be shown by --
(1) Designing the components to minimize the effect of a strike; or
(2) Incorporating acceptable means of diverting the resulting electrical current so as not to endanger the airplane.
[Amdt. 25-23, 35 FR 5674, Apr. 8, 1970]
  
Current page: FARs > Part 25 > Section 581 - Lightning protection
section 25.571 |
section 25.601

page stats: viewed 8411 unique times - last change 08-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 | |