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]
source: Docket No. 2095, 29 FR 7458, June 10, 1964, unless otherwise noted.
cite as: 14 CFR 35.24