SAE ARP 5783 : 2012

Table of Contents

1. SCOPE
2. REFERENCES
3. METRICS
4. ACCEPTANCE CRITERIA
5. RECOMMENDED METRICS
6. NOTES
APPENDIX A - HYPOTHESIS TESTING
APPENDIX B - EXPLANATION OF DECISION MATRIX
APPENDIX C - DETAILS OF SELECTED MATRICS
APPENDIX D - IMPACT OF REDUNDANCY
APPENDIX E - X[2] GOODNESS OF BINOMIAL FIT TEST
APPENDIX F - METRICS FMEA
APPENDIX G - READING ROC CURVES
APPENDIX H - FAILURE RATES
APPENDIX I - RELATION BETWEEN EXPONENTIAL
             AND BINOMIAL FAILURE MODELS
APPENDIX J - MULTIVARIATE METRICS
APPENDIX K - QUALIFYING AN ALGORITHM FOR
             FAILURE DETECTION
APPENDIX L - QUALIFYING AN ALGORITHM FOR
             TRENDING
APPENDIX M - QUALIFYING AN ALGORITHM
             FOR FAULT CLASSIFICATION

Abstract

Pertains to vibration monitoring systems for rotorcraft and fixed-wing drive trains, airframes, propulsion systems, electric power generators, and flight control systems.

General Product Information

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