FAA AC 33.70-2:2009

FAA AC 33.70-2:2009 Damage Tolerance Of Hole Features In High-energy Turbine Engine Rotors Gives definitions, guidance, and acceptable methods, but not the only methods, that may be used to demonstrate compliance with requirements in section 33.70 of Title 14 of the Code of Federal Regulati

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Table of Contents

CHAPTER1-ENHANCEDLIFEMANAGEMENTPROCESS
CHAPTER2-DAMAGETOLERANCEASSESSMENTS
CHAPTER3-"SOFTTIMEINSPECTION"ROTORLIFEMANAGEMENT
APPENDIX1-MANUFACTURING-INDUCEDANOMALYCALIBRATIONTESTCASE
APPENDIX2-DEFAULTANOMALYDISTRIBUTIONCURVES
APPENDIX3-DEFAULTPODAPPLICABILITY
APPENDIX4-DEFAULTPODCURVES
APPENDIX5-DEFINITIONOFAHOLEFORMANUFACTURINGANOMALY
ASSESSMENTS
APPENDIX6-MANUFACTURINGCREDITS
APPENDIX7-SURFACE(MANUFACTURINGINDUCTEDANOMALY)DAMAGE
TOLERANCEASSESSMENT

Abstract

Gives definitions, guidance, and acceptable methods, but not the only methods, that may be used to demonstrate compliance with requirements in section 33.70 of Title 14 of the Code of Federal Regulations related to the integrity of engine life-limited parts.

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