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FAA AC 33.87-2:2009

FAA AC 33.87-2:2009 Comparative Endurance Test Method To Show Durability For Parts Manufacturer Approval Of Turbine Engine And Auxiliary Power Unit Parts Specifies a comparative endurance test method to be used for certain turbine engine or auxiliary power unit (APU) parts when manufactured under Parts Manufacturer Approval (PMA).

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Table of Contents

1.PURPOSE
2.APPLICABILITY
3.RELATEDREFERENCES
4.BACKGROUND
5.BLADEDURABILITY
6.COMPARATIVEENDURANCETESTMETHOD
7.COMPARATIVEENDURANCETESTMETHODFOROTHERGAS
PATHPARTS
Appendix-EnduranceTestCycle

Abstract

Specifies a comparative endurance test method to be used for certain turbine engine or auxiliary power unit (APU) parts when manufactured under Parts Manufacturer Approval (PMA).

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