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SAE AS 5391 : 2016

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

HELICOPTER HEALTH AND USAGE MONITORING SYSTEM ACCELEROMETER INTERFACE SPECIFICATION

Available format(s)

Hardcopy , PDF

Superseded date

14-03-2022

Superseded by

SAE AS5391A

Language(s)

English

Published date

16-06-2016

1. SCOPE
2. REFERENCES
3. REQUIREMENTS AND RECOMMENDATIONS
4. NOTES

Describes interface requirements for accelerometers and associated interfacing electronics for use in a helicopter Health and Usage Monitoring System (HUMS).

Committee
HM-1
DocumentType
Standard
Pages
22
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

SAE AIR4174A A Guide to Aircraft Power Train Monitoring
SAE AIR1871C Lessons Learned from Developing, Implementing, and Operating a Health Management System for Propulsion and Drive Train Systems
SAE ARP 1839 : 2015 A GUIDE TO AIRCRAFT TURBINE ENGINE VIBRATION MONITORING SYSTEMS
SAE AS5393 Health and Usage Monitoring System, Blade Tracker Interface Specification
SAE AIR4061C Guidelines for Integrating Typical Engine Health Management Functions Within Aircraft Systems

SAE ARP 1839 : 2015 A GUIDE TO AIRCRAFT TURBINE ENGINE VIBRATION MONITORING SYSTEMS

€132.78
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