FAA AC 33-1:1970

FAA AC 33-1:1970 Turbine Engine Foreign Object Ingestion And Rotor Blade Containment Type Certification Procedures Gives guidance and acceptable means, not the sole means, by which compliance may be shown with the design and construction requirements of Part 33 of the Federal Aviation Regulations.

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Table of Contents

1PURPOSE
2CANCELLATION
3CHANGES
4REFERENCES
5BACKGROUND
6SCOPE
7DESIRABLEENGINEDESIGNFEATURES
8CLASSIFICATIONOFTYPICALFOREIGNOBJECTS
9ACCEPTANCEMEANSOFCOMPLIANCE
10SUBSTANTIATIONTESTS
11SUBSTANTIATIONCRITERIA

Abstract

Gives guidance and acceptable means, not the sole means, by which compliance may be shown with the design and construction requirements of Part 33 of the Federal Aviation Regulations.

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