14 CFR § 35.24 - Strength.

---
identifier: "/us/cfr/t14/s35.24"
source: "ecfr"
legal_status: "authoritative_unofficial"
title: "14 CFR § 35.24 - Strength."
title_number: 14
title_name: "Aeronautics and Space"
section_number: "35.24"
section_name: "Strength."
chapter_name: "FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION"
subchapter_number: "C"
subchapter_name: "AIRCRAFT"
part_number: "35"
part_name: "AIRWORTHINESS STANDARDS: PROPELLERS"
positive_law: false
currency: "2026-04-05"
last_updated: "2026-04-05"
format_version: "1.1.0"
generator: "[email protected]"
authority: "49 U.S.C. 106(f), 106(g), 40113, 44701-44702, 44704."
regulatory_source: "Docket No. 2095, 29 FR 7458, June 10, 1964, unless otherwise noted."
cfr_part: "35"
---


# 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.

[Amdt. 35-8, 73 FR 63348, Oct. 24, 2008]