SAE AIR 5301 : 2017

Table of Contents

1. SCOPE
2. REFERENCES
3. TECHNICAL BACKGROUND
4. DISADVANTAGES
5. ENGINE TEST CRITERIA
6. AIRCRAFT OUTDOOR TEST FACILITY CONSIDERATIONS
7. AIRCRAFT INSTALLED INSTRUMENTATION SYSTEMS
8. EXISTING GROUND-BASED DATA ACQUISITION/INSTRUMENTATION
    SYSTEMS FOR ON-THE-WING INSTALLED ENGINE TESTING
9. CAPABILITIES OF ENGINE ON-BOARD-CONDITION-MONITORING
    SYSTEMS (EOBCMS)
10. INSTALLATION EFFECTS ON ENGINE PERFORMANCE
11. PROCEDURES, DATA, EQUIPMENT AND PERSONNEL REQUIRED
    FOR ON-THE-WING INSTALLED ENGINE TESTING
12. IMPACT OF ENGINE MODULARITY ON INSTALLED ENGINE TESTING
13. CONCLUSIONS
14. NOTES
APPENDIX A - CLASSICAL SEA LEVEL STANDARD DAY CORRECTION
             EQUATIONS

Abstract

Gives aircraft operators with an overview of current industry on-the-wing engine test practices including advantages/disadvantages derived, test criteria, capabilities of remote ground based test data acquisition/instrumentation and on-board condition monitoring systems, aircraft installation effects, and a general discussion of procedures, data, equipment and personnel required to perform safe, accurate, on-the-wing engine tests.

General Product Information

Published
Document Type	Standard
Status	Current
Publisher	SAE International
Pages
ISBN
Committee	EG-1E