14 CFR 33.62
§ 33.62 Stress analysis.
United States · 14 CFR — Aeronautics and Space · Status: effective
Cite this
- Citation
- 14 CFR 33.62, § 33.62 Stress analysis, United States, version 1 as recorded 2026-07-09, yourstate.us, https://yourstate.us/provision/55079
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Full text
A stress analysis must be performed on each turbine engine showing the design safety margin of each turbine engine rotor, spacer, and rotor shaft.
Legislative history
This is a federal regulation, adopted through agency rulemaking under the Administrative Procedure Act — not enacted by a recorded vote of Congress.