FAA AC 25.571-1 : 2011
Current
The latest, up-to-date edition.
DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE
Hardcopy , PDF
English
01-01-2011
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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
|
| SAE ARP 1311 : 2015 | LANDING GEAR STRUCTURES AND MECHANISMS |
| FAA AC 91-81 : 2008 | FATIGUE MANAGEMENT PROGRAMS FOR AIRPLANES WITH DEMONSTRATED RISK OF CATASTROPHIC FAILURE DUE TO FATIGUE |
| FAA AC 25.613-1 : 2003 | MATERIAL STRENGTH PROPERTIES AND MATERIAL DESIGN VALUES |
| FAA AC 20-66 : 2011 | PROPELLER VIBRATION AND FATIGUE |
| FAA AC 120-77 : 0 | MAINTENANCE AND ALTERATION DATA |
| FAA AC 23-19 : 2007 | AIRFRAME GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES |
| FAA AC 20-167 : 2016 | AIRWORTHINESS APPROVAL OF ENHANCED VISION SYSTEM, SYNTHETIC VISION SYSTEM, COMBINED VISION SYSTEM, AND ENHANCED FLIGHT VISION SYSTEM EQUIPMENT |
| SAE ARP 5429 : 2017 | LANDING GEAR FATIGUE TESTS WITH EQUIVALENT DAMAGE SPECTRA |
| SAE AIR 5552 : 2015 | DEVELOPMENT AND QUALIFICATION OF COMPOSITE LANDING GEARS |
| FAA 8110.4 : 2011 | TYPE CERTIFICATION |
| FAA AC 25.1529-1 : 2007 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS OF STRUCTURAL REPAIRS ON TRANSPORT AIRPLANES |
| FAA AC 120-104 : 2011 | ESTABLISHING AND IMPLEMENTING LIMIT OF VALIDITY TO PREVENT WIDESPREAD FATIGUE DAMAGE |
| FAA AC 20-128 : 0 | DESIGN CONSIDERATIONS FOR MINIMIZING HAZARDS CAUSED BY UNCONTAINED TURBINE ENGINE AND AUXILIARY POWER UNIT ROTOR FAILURE |
| FAA 8110.54 : 2010 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS RESPONSIBILITIES, REQUIREMENTS, AND CONTENTS |
| FAA AC 91-82 : 2012 | FATIGUE MANAGEMENT PROGRAMS FOR IN-SERVICE ISSUES |
| SAE ARP 6461 : 2013 | GUIDELINES FOR IMPLEMENTATION OF STRUCTURAL HEALTH MONITORING ON FIXED WING AIRCRAFT |
| FAA AC 91-56 : 2008 | CONTINUING STRUCTURAL INTEGRITY PROGRAM FOR AIRPLANES |
| FAA AC 120-73 : 0 | DAMAGE TOLERANCE ASSESSMENT OF REPAIRS TO PRESSURIZED FUSELAGES |
| FAA AC 25-24 : 0 | SUSTAINED ENGINE IMBALANCE |
| FAA AC 120-104 : 2011 | ESTABLISHING AND IMPLEMENTING LIMIT OF VALIDITY TO PREVENT WIDESPREAD FATIGUE DAMAGE |
| FAA AC 20-107 : 2009 | COMPOSITE AIRCRAFT STRUCTURE |
| FAA AC 25.1529-1 : 2007 | INSTRUCTIONS FOR CONTINUED AIRWORTHINESS OF STRUCTURAL REPAIRS ON TRANSPORT AIRPLANES |
| FAA AC 91-56 : 2008 | CONTINUING STRUCTURAL INTEGRITY PROGRAM FOR AIRPLANES |
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