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United States Department of Transportation United States Department of Transportation

AC 33.14-1 - Damage Tolerance for High Energy Turbine Engine Rotors - Including Change 1

Document Information

Number
33.14-1
Title
Damage Tolerance for High Energy Turbine Engine Rotors - Including Change 1
Status
Active
Date issued
2001-01-08
Office of Primary Responsibility
ANE-110
Description

This advisory circular describes an acceptable means for showing compliance with the requirements of section 33.14 of the Federal Aviation Regulations (Title 14, Code of Federal Regulations). Section 33.14 contains requirements applicable to the design and life management of high energy rotating parts of aircraft gas turbine engines.

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