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

Document Information

Number
33.15-1
Title
Manufacturing Process of Premium Quality Titanium Alloy Rotating Engine Components
Status
Active
Date issued
1998-09-22
Office of Primary Responsibility
ANE-110
Description
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.
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