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Airborne Engine Vibration Monitoring (EVM) System, Guidelines for Performance Standard For
- Aerospace Standard
Published May 31, 2012 by SAE International in United States
This SAE Aerospace Standard (AS) provides guidelines for the functional, performance, qualification and acceptance testing, and documentation requirements for the components of an airborne engine vibration monitoring (EVM) system which is intended for use as a turbojet engine rotor unbalance indicating system, per FAR 25.1305 (D)(3) on transport category airplanes.
This AS was raised at the request of the Regulatory authorities to provide a minimum performance standard for airborne vibration monitoring systems. Since its creation, these systems have greatly advanced in technology and application and AIR1839, shortly to be re-issued as ARP1839 now contains much more extensive and up-to-date information concerning such installations. Recent survey of the regulatory authorities by E-32 showed no further interest or usage of AS8054. E-32 therefore voted for its cancellation.
|Aerospace Standard||Lessons Learned from Developing, Implementing, and Operating a Health Management System for Propulsion and Drive Train Systems|
|Aerospace Standard||Guide to Life Usage Monitoring and Parts Management for Aircraft Gas Turbine Engines|
Data Sets - Support Documents
No Datasets Available
BackgroundEngine condition monitoring and rotorcraft HUMS(Health and Usage Monitoring Systems)can be used as a tool to track and restore engine performance, improve problem diagnosis, suggest solutions, promote better commercial and military aircraft operation, minimize in-flight failures, and reduce costs of engine maintenance. Because of these and other continuing objectives, the need for consolidated action by a group of experts to promote engine monitoring and rotorcraft condition monitoring know-how and standards was identified. It was deemed appropriate by the SAE Propulsion Division to assign this task to a special committee designated as Committee E-32. The committee has existed for over 40 years and has 26 active members. Purpose / Charter E-32 Committee serves as a forum to gather, record, and publish expert information in the discipline of aerospace propulsion system health management. The Committee gathers and analyzes requirements for propulsion system health management for the various types of air vehicle propulsion systems and develops standards and recommendations for the adoption of aerospace propulsion system health management devices that affect the operation of propulsion systems. Objectives Identifies potential propulsion system parameters suitable for sensing (pressure, temperature, vibration, etc.) and considerations involved in selecting parameters (potential problems, accuracy, cost, etc.), Analyzes the various approaches to aerospace propulsion system health management (e.g., airborne vibration health management systems, fault prediction capabilities, ground software interfaces, etc.) and establishes criteria for cost effective systems, and guidance regarding best practices for designing propulsion health management systems, Develops appropriate standards for aerospace propulsion system health management equipment and techniques; e.g., types of sensors, identification of signals which should be led to common diagnostic connectors, etc., Develops new requirements and uses for aerospace propulsion system health management to promote sustainable and cost effective operation of air vehicles, and Hosts technical conferences related to health management of propulsion systems. Provide a means to gain regulatory approval for utilizing EHM data in a range of maintenance activities.
|AIR1839||A Guide to Aircraft Turbine Engine Vibration Monitoring Systems|
|ANSI/S2.11||This document is not part of the subscrption.|
|ARINC404A||Air Transport Equipment Cases and Racking|
|ARINC600||This document is not part of the subscrption.|
|FAA/AC 25-1309.1A||This document is not part of the subscrption.|
|FAA/AC20-115B||This document is not part of the subscrption.|
|FAA/AC20-136||This document is not part of the subscrption.|
|FAA/AC21-16C||This document is not part of the subscrption.|
|FAA/AC25-1309.1||This document is not part of the subscrption.|
|FAR21.611||This document is not part of the subscrption.|
|FAR25.1309||This document is not part of the subscrption.|
|ISA-RP37.2||This document is not part of the subscrption.|
|MIL-HDBK-217||This document is not part of the subscrption.|
|RTCA/DO-160C||This document is not part of the subscrption.|
|RTCA/DO-178B||This document is not part of the subscrption.|
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