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33.14-1 - Damage Tolerance for High Energy Turbine Engine Rotors

Date Issued
January 08, 2001
Responsible Office
This advisory circular describes an acceptable means for showing compliance with the requirements of section 33.14 of the Federal Aviation Regulations (Title 14, Code of Federal Regulations). Section 33.14 contains requirements applicable to the design and life management of high energy rotating parts of aircraft gas turbine engines.