14 C.F.R. § 33.62
Current through November 30, 2024
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
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