FAA AC 33.15-2 : 2011
Current
Current
The latest, up-to-date edition.
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
€31.50
Excluding VAT
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 |
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