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FAA AC 33.83:2006

FAA AC 33.83:2006 Turbine Engine Vibration Test Provides guidance and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the vibration test requirements of section 33.83 of Title 14 of the Code of Federal

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Table of Contents

1.PURPOSE
2.CANCELLATION
3.APPLICABILITY
4.DEFINITIONS
5.TESTPREPARATION
6.ENGINETESTCONDITIONS
7.FLUTTER
8.VIBRATORYSTRESSESANDMATERIALALLOWABLES
9.RESONANTDWELL
10.FAULTCONDITIONS
11.INSTALLATIONCOMPATIBILITY
12.INSTRUMENTATION

Abstract

Provides guidance and acceptable methods, but not the only methods, that may be used to demonstrate compliance with the vibration test requirements of section 33.83 of Title 14 of the Code of Federal Regulations (14 CFR part 33).

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