FAA AC 25.571-1:2011

FAA AC 25.571-1:2011 Damage Tolerance And Fatigue Evaluation Of Structure 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 cate

More details

Download

PDF AVAILABLE FORMATS IMMEDIATE DOWNLOAD
$17.60 tax incl.

$40.00 tax incl.

(price reduced by 56 %)

1000 items in stock

Table of Contents

1.Purpose
2.Applicability
3.Cancellation
4.Background
5.Introduction
6.Damage-ToleranceEvaluation
7.EstablishinganLOV
8.FatigueEvaluation
9.DiscreteSourceDamage
Appendix1-ReferencesandDefinitions
Appendix2-Full-ScaleFatigueTesting
Appendix3-ProcessforCompliancewith14CFR25.571(a),
(b)and(c)forFatigueDamage
Appendix4-ExamplesofAlterationsthatMayRequire
Full-ScaleFatigueTesting
Appendix5-PSE,FCSandWFD-SusceptibleStructure
Appendix6-AcronymsandAbbreviationsusedinthisAC

Abstract

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).

Contact us