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