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Guidelines for Integrating Typical Engine Health Management Functions Within Aircraft Systems
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STANDARD published on 1.11.2016
Designation standards: SAE AIR4061C
Publication date standards: 1.11.2016
SKU: NS-668215
Country: American technical standard
Category: Technical standards SAE
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.
SUBJECT TAXONOMY: Aircraft operations, Vehicle health management, Jet engines, Auxiliary power units
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Standard
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Latest update: 2024-09-08 (Number of items: 2 346 217)
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