FAA AC 35.37-1 : 2011
Current
The latest, up-to-date edition.
PROPELLER FATIGUE LIMITS AND EVALUATION
Hardcopy , PDF
English
01-01-2011
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1. Purpose
2. Applicability
3. Cancellation
4. Related Reference Material
5. Definitions
6. Discussion
7. Composite Component Fatigue Limits
8. Change of Composite Material and/or Process
9. Metallic Component Fatigue Limits
10. Metallic Hub and Retention Fatigue Tests
11. Fatigue Evaluation
Appendix - Figures
Gives guidance and describes methods, but not the only methods, for demonstrating compliance with section 35.37, Propeller fatigue limits and evaluation, of Title 14 of the Code of Federal Regulations (14 CFR).
| DocumentType |
Standard
|
| Pages |
25
|
| 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 20-66 : 2011 | PROPELLER VIBRATION AND FATIGUE |
| FAA AC 23-16 : 0 | POWERPLANT GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES AND AIRSHIPS |
| MIL-HDBK-17-1 Revision F:2002 | COMPOSITE MATERIALS HANDBOOK - VOLUME 1: POLYMER MATRIX COMPOSITES GUIDELINES FOR CHARACTERIZATION OF STRUCTURAL MATERIALS |
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