• SAE AS 5391 : 2016

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

    HELICOPTER HEALTH AND USAGE MONITORING SYSTEM ACCELEROMETER INTERFACE SPECIFICATION

    Available format(s):  Hardcopy, PDF

    Superseded date:  14-03-2022

    Language(s):  English

    Published date:  16-06-2016

    Publisher:  SAE International

    Add To Cart

    Table of Contents - (Show below) - (Hide below)

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

    Abstract - (Show below) - (Hide below)

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

    General Product Information - (Show below) - (Hide below)

    Committee HM-1
    Document Type Standard
    Publisher SAE International
    Status Superseded
    Superseded By
    Supersedes

    Standards Referenced By This Book - (Show below) - (Hide below)

    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

    Standards Referencing This Book - (Show below) - (Hide below)

    SAE ARP 1839 : 2015 A GUIDE TO AIRCRAFT TURBINE ENGINE VIBRATION MONITORING SYSTEMS
    • Access your standards online with a subscription

      Features

      • Simple online access to standards, technical information and regulations
      • Critical updates of standards and customisable alerts and notifications
      • Multi - user online standards collection: secure, flexibile and cost effective