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Code of Federal Regulations (Last Updated: April 5, 2024) |
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Title 14 - Aeronautics and Space |
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Chapter I - Federal Aviation Administration, Department of Transportation |
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SubChapter C - Aircraft |
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Part 33 - Airworthiness Standards: Aircraft Engines |
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Subpart E - Design and Construction; Turbine Aircraft Engines |
§ 33.62 - Stress analysis.
Latest version.
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§ 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]