FAA AC 120-104:2011
FAA AC 120-104:2011 Establishing And Implementing Limit Of Validity To Prevent Widespread Fatigue Damage Describes guidance on compliance with Title 14 Code of Federal Regulations (14 CFR) 26.21, 26.23, 121.1115, and 129.115.
Table of Contents
1.PURPOSE2.APPLICABILITY
3.WHYDOYOUNEEDANLOV?
4.DOCUMENTORGANIZATION
CHAPTER1-OVERVIEWOFTHEPROCESSFORESTABLISHINGA
LIMITOFVALIDITY
CHAPTER2-SECTION26.21COMPLIANCEINFORMATIONFORDESIGN
APPROVALHOLDERS
CHAPTER3-SECTION26.23EXTENDEDLOVS
CHAPTER4-COMPLIANCEINFORMATIONFOROPERATORS
APPENDIX1-RELATEDREGULATIONSANDDOCUMENTS
APPENDIX2-DEFINITIONS
APPENDIX3-ACRONYMSUSEDINTHISAC
APPENDIX4-BACKGROUND
APPENDIX5-EXAMPLESOFSTRUCTURESUSCEPTIBLETOWFD
APPENDIX6-WIDESPREADFATIGUEDAMAGEEVALUATION
APPENDIX7-EXAMPLEOFHOWTOESTABLISHANLOV
APPENDIX8-SAMPLECOMPLIANCEPLAN