PROPELLER VIBRATION AND FATIGUE

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2011

Publisher

Federal Aviation Administration

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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FAA AC 20-66 : 2011

PROPELLER VIBRATION AND FATIGUE

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Abstract

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Standards Referenced By This Book

Standards Referencing This Book

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