FAA Federal Aviation Regulations (FARS, 14 CFR)
FARs > Part 35 > Section 45 - Teardown inspection
section 35.43 |
section 35.47

(a) After completion of the tests prescribed in this subpart, the propeller must be completely disassembled and a detailed inspection must be made of the propeller parts for cracks, wear, distortion, and any other unusual conditions.
(b) After the inspection the applicant must make any changes to the design or any additional tests that the Administrator finds necessary to establish the airworthiness of the propeller.
[Doc. No. 3095, 29 FR 7458, June 10, 1964, as amended by Amdt. 35-3, 41 FR 55475, Dec. 20, 1976]
  
Current page: FARs > Part 35 > Section 45 - Teardown inspection
section 35.43 |
section 35.47

page stats: viewed 792 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 | |