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FAA AC 33.15-1 : 0

Current
Current

The latest, up-to-date edition.

MANUFACTURING PROCESS OF PREMIUM QUALITY TITANIUM ALLOY ROTATING ENGINE COMPONENTS
Available format(s)

Hardcopy , PDF

Language(s)

English

Publisher

Federal Aviation Administration

1 PURPOSE
2 RELATED READING MATERIAL
3 DEFINITIONS
4 BACKGROUND
5 GENERAL
6 RAW MATERIALS & STORAGE
7 CONSOLIDATION AND MELTING
8 BILLET CONVERSION, DISK FORGING, AND NDT
APPENDIX 1 MINIMUM RECOMMENDED PROCEDURE FOR 3D INCLUSION
           CHARACTERIZATION

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.

DocumentType
Standard
Pages
20
PublisherName
Federal Aviation Administration
Status
Current

FAA AC 33.15-2 : 2011 MANUFACTURING PROCESSES FOR PREMIUM QUALITY NICKEL ALLOY FOR ENGINE ROTATING PARTS

FAA AC 33-2 : 2013 GENERAL TYPE CERTIFICATION GUIDELINES FOR TURBINE ENGINES
FAA AC 33-4 : 0 DESIGN CONSIDERATIONS CONCERNING THE USE OF TITANIUM IN AIRCRAFT TURBINE ENGINES
FAA AC 33-3 : 0 TURBINE AND COMPRESSOR ROTORS TYPE CERTIFICATION SUBSTANTIATION PROCEDURES

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Hardcopy - English
PDF - English
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