GroundRules
14 CFR 33.62: Stress analysis.
Where this section sits in the code
- Title 14—Aeronautics and Space
- CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
- SUBCHAPTER C—AIRCRAFT
- PART 33—AIRWORTHINESS STANDARDS: AIRCRAFT ENGINES
- Subpart E—Design and Construction; Turbine Aircraft Engines
A stress analysis must be performed on each turbine engine showing the design safety margin of each turbine engine rotor, spacer, and rotor shaft.
Collected 2026-08-27T02:24:20Z. Source file · JSON