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FAA AC 25.571-1 : 2011

Current
Current

The latest, up-to-date edition.

DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2011

Publisher

Federal Aviation Administration

1. Purpose
2. Applicability
3. Cancellation
4. Background
5. Introduction
6. Damage-Tolerance Evaluation
7. Establishing an LOV
8. Fatigue Evaluation
9. Discrete Source Damage
Appendix 1 - References and Definitions
Appendix 2 - Full-Scale Fatigue Testing
Appendix 3 - Process for Compliance with 14 CFR 25.571(a),
             (b) and (c) for Fatigue Damage
Appendix 4 - Examples of Alterations that May Require
             Full-Scale Fatigue Testing
Appendix 5 - PSE, FCS and WFD-Susceptible Structure
Appendix 6 - Acronyms and Abbreviations used in this AC

Gives guidance for compliance with the provisions of Tide 14, Code of Federal Regulations (14 CFR) part 25, pertaining to the requirements for damage-tolerance and fatigue evaluation of transport category aircraft structure, including evaluation of widespread fatigue damage (WFD) and establishing a limit of validity of the engineering data that supports the structural-maintenance Program (hereafter referred to as the LOY).

DocumentType
Standard
Pages
41
PublisherName
Federal Aviation Administration
Status
Current

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