14 C.F.R. § 33.62 Stress analysis.
Title 14 - Aeronautics and Space
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]
Title 14: Aeronautics and Space
PART 33—AIRWORTHINESS STANDARDS: AIRCRAFT ENGINES
Subpart E—Design and Construction; Turbine Aircraft Engines
§ 33.62 Stress analysis.
