1. LawStack
  2. Title 14 - Aeronautics and Space
  3. Chapter I - FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
  4. Subchapter C - AIRCRAFT
  5. Part 33 - AIRWORTHINESS STANDARDS: AIRCRAFT ENGINES
  6. Subpart E - Design and Construction; Turbine Aircraft Engines
  7. 14 CFR § 33.62
14 CFR § 33.62
Stress analysis
July 13, 2020
CFR

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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§ 33.61 Applicability
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§ 33.63 Vibration

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