[Code of Federal Regulations]
[Title 14, Volume 1]
[Revised as of January 1, 2004]
From the U.S. Government Printing Office via GPO Access
[CITE: 14CFR33.62]

[Page 769]
 
                     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]