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FAA AC 35.37-1 : 1993

NA
NA

Status of Standard is Unknown

PROPELLER FATIGUE LIMITS AND EVALUATION
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-1993

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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