FAA AC 33.70-1:2009

FAA AC 33.70-1:2009 Guidance Material For Aircraft Engine Life-limited Parts Requirements Gives definitions, guidance, and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the engine life-limited parts integrity requirements of section 33.70 of

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Table of Contents

1.PURPOSE
2.APPLICABILITY
3.RELATEDREGULATIONS
4.RELATEDGUIDANCE
5.DEFINITIONS
6.INTRODUCTION
7.GENERAL
8.GUIDANCEFORDEFININGANENGINEERINGPLAN
9.GUIDANCEFORDEFININGAMANUFACTURINGPLAN
10.GUIDANCEFORDEFININGASERVICEMANAGEMENTPLAN
11.AIRWORTHINESSLIMITATIONSECTION

Abstract

Gives definitions, guidance, and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the engine life-limited parts integrity requirements of section 33.70 of Title 14 of the Code of Federal Regulations (14 CFR part 33).

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