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FAA AC 33-8:2009

FAA AC 33-8:2009 Guidance For Parts Manufacturer Approval Of Turbine Engine And Auxiliary Power Unit Parts Under Test And Computation Gives guidance for developing substantiation data to support the design approval of critical and complex turbine engine and auxiliary power unit (APU) parts produced under parts manufacturer approval

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Table of Contents

1.Purpose
2.Applicability
3.RelatedReferences
4.Background
5.PartCriticality
6.ComparativeTestandAnalysisMethod
7.ReverseEngineeringConsiderations
8.ContinuedOperationalSafety
9.PartNumbering
APPENDIX1-FAILUREMODESANDEFFECTSASSESSMENT
APPENDIX2-TEMPLATES
APPENDIX3-REVERSEENGINEERINGDESIGNPROCESS
APPENDIX4-CONTINUEDOPERATIONALSAFETY

Abstract

Gives guidance for developing substantiation data to support the design approval of critical and complex turbine engine and auxiliary power unit (APU) parts produced under parts manufacturer approval (PMA).

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