[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: 14CFR33.62]



[Page 778]

 

                     TITLE 14--AERONAUTICS AND SPACE

 

CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION

 

PART 33_AIRWORTHINESS STANDARDS: AIRCRAFT ENGINES--Table of Contents

 

       Subpart E_Design and Construction; Turbine Aircraft Engines

 

Sec. 33.62  Stress analysis.



    A stress analysis must be performed on each turbine engine showing 

the design safety margin of each turbine engine rotor, spacer, and rotor 

shaft.



[Amdt. 33-6, 39 FR 35466, Oct. 1, 1974]