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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Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by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Superseded date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Superseded by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:2002(R2022)

Language(s)

English

Published date

16-06-2016

€128.14
Excluding VAT

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Superseded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 AIR 4174A : 2017 A GUIDE TO AIRCRAFT POWER TRAIN MONITORING
SAE AIR 1871 : 2017 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 AS 5393 : 2009 HEALTH AND USAGE MONITORING SYSTEM, BLADE TRACKER INTERFACE SPECIFICATION
SAE AIR 4061 : 2016 GUIDELINES FOR INTEGRATING TYPICAL ENGINE HEALTH MANAGEMENT FUNCTIONS WITHIN AIRCRAFT SYSTEMS

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

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