14 CFR 35.24: Strength.
Where this section sits in the code
- Title 14—Aeronautics and Space
- CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
- SUBCHAPTER C—AIRCRAFT
- PART 35—AIRWORTHINESS STANDARDS: PROPELLERS
- Subpart B—Design and Construction
The maximum stresses developed in the propeller may not exceed values acceptable to the Administrator considering the particular form of construction and the most severe operating conditions.
Collected 2026-08-27T02:24:20Z. Source file · JSON