MANUFACTURING PROCESSES FOR PREMIUM QUALITY NICKEL ALLOY FOR ENGINE ROTATING PARTS

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2011

Publisher

Federal Aviation Administration

1. Purpose
2. Applicability
3. Related Guidance
4. Definitions
5. Background
6. General
7. Raw Materials and Storage
8. Melting and Remelting
9. Billet/Bar Conversion, Disk Forging, and
Nondestructive Testing (NDT)

Gives information and guidance on compliance with the nickel materials suitability and durability requirements in part 33 of Title 14 of the Code of Federal Regulations (14 CFR part 33).

DocumentType	Standard
Pages	17
PublisherName	Federal Aviation Administration
Status	Current

FAA AC 33.15-1 : 0	MANUFACTURING PROCESS OF PREMIUM QUALITY TITANIUM ALLOY ROTATING ENGINE COMPONENTS
FAA AC 33-3 : 0	TURBINE AND COMPRESSOR ROTORS TYPE CERTIFICATION SUBSTANTIATION PROCEDURES