14 C.F.R. § 33.62

Current through September 30, 2024
Section 33.62 - Stress analysis

A stress analysis must be performed on each turbine engine showing the design safety margin of each turbine engine rotor, spacer, and rotor shaft.

14 C.F.R. §33.62

Amdt. 33-6, 39 FR 35466, Oct. 1, 1974