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FAA AC 35.37-1 : 2011

Current
Current

The latest, up-to-date edition.

PROPELLER FATIGUE LIMITS AND EVALUATION
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2011

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

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