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33.15-1 - Manufacturing Process of Premium Quality Titanium Alloy Rotating Engine Components

Date Issued
September 22, 1998
Responsible Office
Provides guidance for compliance with the provisions under Title 14 under the Code of Federal Regulations, Part 33 (14 CFR 33) pertaining to the materials suitability and durability requirements, 33.15, as applicable to the manufacture of titanium alloy high energy rotating parts of aircraft engines.