[Code of Federal Regulations]

[Title 14, Volume 1]

[Revised as of January 1, 2006]

From the U.S. Government Printing Office via GPO Access

[CITE: 14CFR35.45]



[Page 810]

 

                     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]