FAA AC 33-11 : 2014
Current
The latest, up-to-date edition.
OXIDATION, HOT CORROSION, THERMAL FATIGUE, AND EROSION CHARACTERISTICS TESTING TO SUPPORT 14 CFR, PART 33, SECTION 33.15, COMPLIANCE FOR TURBINE ENGINES
Hardcopy , PDF
English
01-01-2014
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1. Purpose
2. Applicability
3. Reference
4. Background
5. Comparative Tests
6. Summary
Appendix - Advisory Circular (AC) Feedback Information
Specifies an acceptable method, but not the only method, to support certain comparative assessment compliance findings to Title 14 of the Code of Federal Regulations (14 CFR) part 33, section 33.15, Materials, for turbine engine projects.
| DocumentType |
Standard
|
| Pages |
8
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 33-10 : 2014 | STATISTICAL ANALYSIS CONSIDERATIONS FOR COMPARATIVE TEST AND ANALYSIS BASED COMPLIANCE FINDINGS FOR TURBINE ENGINE AND AUXILIARY POWER UNIT REPLACEMENT, REDESIGN AND REPAIRED PARTS |
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