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United States Department of TransportationUnited States Department of Transportation

AC 33-5 - Turbine Engine Rotor Blade Containment/Durability

Document Information

Number
33-5
Title
Turbine Engine Rotor Blade Containment/Durability
Status
Active
Date issued
1990-06-18
Office of Primary Responsibility
ANE-110
Description
Provides guidance and acceptable methods, but not the only methods, that may be used by an applicant in showing compliance with the turbine engine rotor blade containment requirements of Part 33 of the Federal Aviation Regulations (FAR).
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