SAE AIR4061C
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
Guidelines for Integrating Typical Engine Health Management Functions Within Aircraft Systems
Hardcopy , PDF
English
12-11-2016
01-11-2016
1. SCOPE
2. REFERENCES
3. GENERAL INTRODUCTION
4. GENERAL CONSIDERATIONS
5. PARAMETER SELECTION AND REQUIREMENTS
6. SIGNAL SOURCES
7. SIGNAL TRANSMISSION, CONDITIONING, AND DATA PROCESSING
8. DATA STORAGE
9. DATA RETRIEVAL
10. CONCLUSION
11. NOTES
Provides best practice guidelines for the integration of Engine Health Management (EHM) system functions within aircraft systems to include both its main engine(s) and any Auxiliary Power Unit(s) (APU).
| DocumentType |
Standard
|
| Pages |
25
|
| PublisherName |
SAE International
|
| Status |
Withdrawn
|
| Supersedes |
SAE Aerospace Information Report (AIR) 4061 provides best practice guidelines for the integration of Engine Health Management (EHM) system functions within aircraft systems to include both its main engine(s) and any Auxiliary Power Unit(s) (APU). This document provides an overview of some of the functions EHM typically integrates, offers some system variations encountered with different aircraft, and suggests general considerations involved with integration. It presents a sample EHM parameter coverage matrix to show the types of parameters with which a typical EHM system might interface, offers insight into signal and data processing and retrieval, and offers a view of typical EHM parameter requirements by function. Where practical, this document delineates between military and commercial practices.
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