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FAA AC 33.15-1:1998

FAA AC 33.15-1:1998 Manufacturing Process Of Premium Quality Titanium Alloy Rotating Engine Components Gives guidance and information 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 requi

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Table of Contents

1PURPOSE
2RELATEDREADINGMATERIAL
3DEFINITIONS
4BACKGROUND
5GENERAL
6RAWMATERIALSSTORAGE
7CONSOLIDATIONANDMELTING
8BILLETCONVERSION,DISKFORGING,ANDNDT
APPENDIX1MINIMUMRECOMMENDEDPROCEDUREFOR3DINCLUSION
CHARACTERIZATION

Abstract

Gives guidance and information 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, section 33.15, as applicable to the manufacture of titanium alloy high energy rotating parts of aircraft engines.

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