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United States Department of Transportation United States Department of Transportation

AC 33.70-5 - Damage Tolerance of Axial Blade Slot Features in High Energy Turbine Engine Rotors

Document Information

Number
33.70-5
Title
Damage Tolerance of Axial Blade Slot Features in High Energy Turbine Engine Rotors
Status
Inactive
Date issued
2024-07-02
Office of Primary Responsibility
AIR-625, Interactive Org Chart: Engine & Propulsion Section
Description

This advisory circular (AC) provides definitions, guidance, and acceptable methods, but not the only methods, that may be used to demonstrate compliance with requirements in § 33.70 of Title 14 of the Code of Federal Regulations related to the integrity of engine life-limited parts. Section 33.70 contains requirements applicable to the design and life management of propulsion system life-limited parts, including high-energy rotating parts.

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