FAA AC 35.37-1 : 0
NA
Status of Standard is Unknown
PROPELLER FATIGUE LIMITS AND EVALUATION
Hardcopy , PDF
English
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 |
8
|
| PublisherName |
Federal Aviation Administration
|
| Status |
NA
|
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