FAA AC 33.15-2 : 2011
Current
The latest, up-to-date edition.
MANUFACTURING PROCESSES FOR PREMIUM QUALITY NICKEL ALLOY FOR ENGINE ROTATING PARTS
Hardcopy , PDF
English
01-01-2011
Important note : Users cannot be edited or removed once added to your Multi user PDF.
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 |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.