View all text of Subpart E [§ 33.61 - § 33.79]
§ 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.
View all text of Subpart E [§ 33.61 - § 33.79]
A stress analysis must be performed on each turbine engine showing the design safety margin of each turbine engine rotor, spacer, and rotor shaft.