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FAA AC 33-4:1983

FAA AC 33-4:1983 Design Considerations Concerning The Use Of Titanium In Aircraft Turbine Engines Gives guidance and acceptable means, not the sole means, by which compliance may be shown with the design requirements of Part 33 to minimize the probability of the occurrence of an internal fire when

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Table of Contents

1PURPOSE
2APPLICABLEREGULATIONS
3REFERENCES
4BACKGROUND
5DESIGNCONSIDERATIONS

Abstract

Gives guidance and acceptable means, not the sole means, by which compliance may be shown with the design requirements of Part 33 to minimize the probability of the occurrence of an internal fire when titanium is used in aircraft turbine engines.

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