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Aircraft Gas Turbine Engine Health Management System Development and Integration Guide
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STANDARD published on 1.3.2016
Designation standards: SAE ARP5120
Publication date standards: 1.3.2016
SKU: NS-657251
Country: American technical standard
Category: Technical standards SAE
ARP5120 provides recommended best practices, procedures, and technology to guide the physical and functional design, development, integration, verification, and validation of highly reliable Engine Health Management (EHM) systems for aircraft engines and Auxiliary Power Units (APUs). This SAE Aerospace Recommended Practice (ARP) also serves as a concise reference of considerations, approaches, activities, and requirements for producing the end-to-end engine health management system comprised of both on and off-board subsystems for the sensing, acquisition, analysis, detection, and data handling functions for EHM. These functions may also be used to effect continued operation or return to service decisions when demonstrated as compliant with the applicable airworthiness requirements defined by the responsible Aviation Authority. Where practical, this document delineates between military and commercial practices.
SUBJECT TAXONOMY: Aircraft operations, Maintenance, repair, and service operations, Gas turbines, Airworthiness
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Standard
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Latest update: 2026-04-08 (Number of items: 2 271 105)
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