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FAA AC 33-5:1990

FAA AC 33-5:1990 Turbine Engine Rotor Blade Containment/durability Gives guidance and acceptable methods, but not the only methods, that may be used by an acceptable in showing compliance with the turbine engine rotor blade containment requirements of Part 33 of the

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Table of Contents

1PURPOSE
2RELATEDFAR
3RELATEDREADINGMATERIAL
4BACKGROUND
5DEFINITIONS
6DISCUSSION

Abstract

Gives guidance and acceptable methods, but not the only methods, that may be used by an acceptable in showing compliance with the turbine engine rotor blade containment requirements of Part 33 of the Federal Aviation Regulations (FAR).

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