14 CFR § 33.62 Airworthiness Standards: Aircraft Engines

§ 33.62 Stress analysis.

Current through Jul 24, 2026 · Read all of Part 33

⚠ 2 pending changes to Part 33

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]

← § 33.61 Applicability.§ 33.63 Vibration. →