C.F.R. » Title 14 » CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION › SUBCHAPTER C—AIRCRAFT › PART 33—AIRWORTHINESS STANDARDS: AIRCRAFT ENGINES › Subpart E—Design and Construction; Turbine Aircraft Engines

14 C.F.R. § 33.62

Stress analysis

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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]