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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

€35.89
Excluding VAT

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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