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SAE ARP 1839 : 2015

SAE ARP 1839 : 2015

A GUIDE TO AIRCRAFT TURBINE ENGINE VIBRATION MONITORING SYSTEMS

SAE International

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Table of Contents

1. SCOPE
2. REFERENCES
3. INTRODUCTION
4. HISTORY
5. EVM SYSTEM FUNCTIONALITY
6. SYSTEM DESIGN
7. VIBRATION ANALYSIS TECHNIQUES (FOR
    MAINTENANCE PURPOSES)
8. ROTOR TRIM BALANCING
9. RESPONSIBILITIES
10. REGULATORY REQUIREMENTS
11. HUMAN FACTORS
12. THE ECONOMICS OF A VIBRATION MONITORING
    SYSTEM
13. USAGE
14. MAINTENANCE BENEFITS
15. SUMMARY
16. NOTES

Abstract

Gives a general overview of typical airborne engine vibration monitoring (EVM) systems applicable to fixed or rotary wing aircraft applications, with an emphasis on system design considerations.

General Product Information

Document Type Standard
Status Current
Publisher SAE International
Committee E-32
Supersedes
  • SAE AIR 1839 : 2017

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