FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 35 > Section 17 - Materials
section 35.15 |
section 35.19

The suitability and durability of materials used in the propeller must --
(a) Be established on the basis of experience or tests; and
(b) Conform to approved specifications (such as industry or military specifications, or Technical Standard Orders) that ensure their having the strength and other properties assumed in the design data. (Secs. 313(a), 601, and 603, 72 Stat. 752, 775, 49 U.S.C. 1354(a), 1421, and 1423; sec. 6(c), 49 U.S.C. 1655(c))
[Amdt. 35-4, 42 FR 15047, Mar. 17, 1977]
  
Current page: FARs > Part 35 > Section 17 - Materials
section 35.15 |
section 35.19

page stats: viewed 399 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 | |