FAA AC 20-66 : 2011
Current
The latest, up-to-date edition.
PROPELLER VIBRATION AND FATIGUE
Hardcopy , PDF
English
01-01-2011
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1. Purpose
2. Applicability
3. Cancellation
4. Related Documents
5. Definitions
6. Discussion
7. Vibration Tests
8. Stress Peaks and Resonant Conditions
9. Propeller Flutter
10. Similarity
11. Note 9 Vibration Approvals
12. Propeller Fatigue Evaluation
13. Airplane and Propeller Operating and Airworthiness
Limitations
Appendix 1 - Tables and Figures
Appendix 2 - Propeller Vibration Background Information
Appendix 3 - Propeller Vibration Evaluation Test Conditions
Gives guidance and describes one method, but not the only method, for demonstrating compliance with Section 23.907 and 25.907 of Title 14 of the Code of Federal Regulations, for the evaluation of vibration stresses on propellers installed on airplanes.
| DocumentType |
Standard
|
| Pages |
39
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Current
|
| FAA AC 23-24 : 2005 | AIRWORTHINESS COMPLIANCE CHECKLISTS FOR COMMON PART 23 SUPPLEMENTAL TYPE CERTIFICATE (STC) PROJECTS |
| FAA AC 35-1 : 2008 | CERTIFICATION OF PROPELLERS |
| FAA AC 23-16 : 0 | POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS |
| FAA AC 35.37-1 : 2011 | PROPELLER FATIGUE LIMITS AND EVALUATION |
| FAA AC 35-1 : 2008 | CERTIFICATION OF PROPELLERS |
| FAA AC 20-107 : 2009 | COMPOSITE AIRCRAFT STRUCTURE |
| FAA AC 25.571-1 : 2011 | DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE |
| FAA AC 21-26 : 2010 | QUALITY SYSTEM FOR THE MANUFACTURE OF COMPOSITE STRUCTURES |
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