[Code of Federal Regulations]
[Title 14, Volume 1]
[Revised as of January 1, 2003]
From the U.S. Government Printing Office via GPO Access
[CITE: 14CFR35.45]

[Page 778]
 
                     TITLE 14--AERONAUTICS AND SPACE
 
CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
 
PART 35--AIRWORTHINESS STANDARDS: PROPELLERS--Table of Contents
 
                    Subpart C--Tests and Inspections
 
Sec. 35.45  Teardown inspection.

    (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]