CFR > Title 14 - Aeronautics and Space > CHAPTER I—FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION > SUBCHAPTER C—AIRCRAFT (parts 21 to 50) > PART 35—AIRWORTHINESS STANDARDS: PROPELLERS > SUBPART B—Design and Construction (§35.11 to §35.24) > 35.24—Strength.

35.24—Strength.

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.

Code of Federal Regulations

[Amdt. No. 35-8, 73 FR 63348, Oct. 24, 2008]