SAE ARP 5120 : 2016

SAE ARP 5120 : 2016

AIRCRAFT GAS TURBINE ENGINE HEALTH MANAGEMENT SYSTEM DEVELOPMENT AND INTEGRATION GUIDE

SAE International

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Table of Contents

1. SCOPE
2. REFERENCES
3. CONCEPTS AND CONSIDERATIONS
4. RECOMMENDED PRACTICES FOR DESIGN, DEVELOPMENT,
   AND TEST
5. RECOMMENDED PRACTICES FOR IMPLEMENTATION
6. CONCLUSION
7. NOTES
APPENDIX A - HEALTH MANAGEMENT STANDARDS
APPENDIX B - SENSOR PARAMETER AND SIGNAL PERFORMANCE
             REQUIREMENTS (SENSE/ACQUIRE)
APPENDIX C - EXAMPLE EGT MARGIN CALCULATION
APPENDIX D - DATA MANIPULATION DESIGN AND PERFORMANCE
             REQUIREMENTS (ANALYSIS/ACT)

Abstract

Gives recommended best practices, procedures, and technology to guide the physical and functional design, development, integration, verification, and validation of highly reliable Engine Health Management (EHM) systems for aircraft engines and Auxiliary Power Units (APUs).

General Product Information

Document Type Standard
Status Current
Publisher SAE International
Committee E-32

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