FAA AC 33-10 : 2014
Current
The latest, up-to-date edition.
STATISTICAL ANALYSIS CONSIDERATIONS FOR COMPARATIVE TEST AND ANALYSIS BASED COMPLIANCE FINDINGS FOR TURBINE ENGINE AND AUXILIARY POWER UNIT REPLACEMENT, REDESIGN AND REPAIRED PARTS
Hardcopy , PDF
English
01-01-2014
1. Purpose
2. Applicability
3. Related Advisory and Reading Material
4. Background
5. Guidance
Appendix A - Advisory Circular Feedback
Information
Defines acceptable statistical methods, but not the only methods, to help develop substantiating data for comparative test and analysis compliance findings.
| DocumentType |
Standard
|
| Pages |
13
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| 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 |
| FAA AC 33.83-1 : 2009 | COMPARATIVE METHOD TO SHOW EQUIVALENT VIBRATORY STRESSES AND HIGH CYCLE FATIGUE CAPABILITY FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS |
| FAA AC 33-8 : 2009 | GUIDANCE FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS UNDER TEST AND COMPUTATION |
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