CFR > Title 14 - Aeronautics and Space > CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION > SUBCHAPTER C—AIRCRAFT (parts 21 to 50) > PART 33—AIRWORTHINESS STANDARDS: AIRCRAFT ENGINES > SUBPART E—Design and Construction; Turbine Aircraft Engines (§33.61 to §33.79) > 33.62—Stress analysis.

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.

Code of Federal Regulations

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