TURBINE ENGINE VIBRATION TEST

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-01-2006

Publisher

Federal Aviation Administration

1. PURPOSE
2. CANCELLATION
3. APPLICABILITY
4. DEFINITIONS
5. TEST PREPARATION
6. ENGINE TEST CONDITIONS
7. FLUTTER
8. VIBRATORY STRESSES AND MATERIAL ALLOWABLES
9. RESONANT DWELL
10. FAULT CONDITIONS
11. INSTALLATION COMPATIBILITY
12. INSTRUMENTATION

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).

DocumentType	Standard
Pages	8
PublisherName	Federal Aviation Administration
Status	Current

FAA AC 33.83-1 : 2009

COMPARATIVE METHOD TO SHOW EQUIVALENT VIBRATORY STRESSES AND HIGH CYCLE FATIGUE CAPABILITY FOR PARTS MANUFACTURER APPROVAL OF TURBINE ENGINE AND AUXILIARY POWER UNIT PARTS

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FAA AC 33.83 : 2006

TURBINE ENGINE VIBRATION TEST

Table of Contents

Abstract

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Standards Referenced By This Book

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