OXIDATION, HOT CORROSION, THERMAL FATIGUE, AND EROSION CHARACTERISTICS TESTING TO SUPPORT 14 CFR, PART 33, SECTION 33.15, COMPLIANCE FOR TURBINE ENGINES

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Hardcopy , PDF

Language(s)

English

Published date

01-01-2014

Publisher

Federal Aviation Administration

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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FAA AC 33-11 : 2014

OXIDATION, HOT CORROSION, THERMAL FATIGUE, AND EROSION CHARACTERISTICS TESTING TO SUPPORT 14 CFR, PART 33, SECTION 33.15, COMPLIANCE FOR TURBINE ENGINES

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Abstract

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