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

Document Information

Number
33.15-1A
Title
Manufacturing Process of Premium Quality Titanium Alloy Rotating Engine Components
Status
Active
Date issued
2025-09-08
Office of Primary Responsibility
AIR-625, Interactive Org Chart: Engine & Propulsion Section
Content
Cancels
Cancels
Number Title Date
33.15-1 Manufacturing Process of Premium Quality Titanium Alloy Rotating Engine Components

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.

 2025-09-08