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Code · CFR · Title 14 — Aeronautics and Space · Part 33 — Airworthiness Standards: Aircraft Engines · § 33.62

§ 33.62. Stress analysis.

32 words·~1 min read·/us/cfr/t14/s§ 33.62·

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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]
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§ 33.62
Stress analysis.
Fed. Reg.×1
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