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  • SAE AS 8054 : 1996

    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

    AIRBORNE ENGINE VIBRATION MONITORING (EVM) SYSTEM, GUIDELINES FOR PERFORMANCE STANDARD FOR

    Available format(s): 

    Withdrawn date:  31-05-2012

    Language(s): 

    Published date:  01-01-1996

    Publisher:  SAE International

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

    1 SCOPE
    2 APPLICABLE DOCUMENTS
    3 REQUIREMENTS
    4 UNIT QUALIFICATION AND ACCEPTANCE
    5 NOTES

    Abstract - (Show below) - (Hide below)

    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) or transport category airplanes.

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

    Committee E-32
    Document Type Standard
    Publisher SAE International
    Status Withdrawn

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

    SAE ARP 1839 : 2015 A GUIDE TO AIRCRAFT TURBINE ENGINE VIBRATION MONITORING SYSTEMS
    SAE ARP 1587 : 2013 AIRCRAFT GAS TURBINE ENGINE HEALTH MANAGEMENT SYSTEM GUIDE
    SAE AIR 4175 : 2016 A GUIDE TO THE DEVELOPMENT OF A GROUND STATION FOR ENGINE CONDITION MONITORING
    SAE AIR 1839 : 2017 A GUIDE TO AIRCRAFT TURBINE ENGINE VIBRATION MONITORING SYSTEMS

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

    FAA AC 21-16 : 2011 RTCA DOCUMENT DO-160 VERSIONS D, E, F, AND G, "ENVIRONMENTAL CONDITIONS AND TEST PROCEDURES FOR AIRBORNE EQUIPMENT"
    RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
    FAA AC 20-136 : 2011 AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION
    SAE AIR 1839 : 2017 A GUIDE TO AIRCRAFT TURBINE ENGINE VIBRATION MONITORING SYSTEMS
    ISA RP37.2 : 1982 GUIDE FOR SPECIFICATIONS AND TESTS FOR PIEZOELECTRIC ACCELERATION TRANSDUCERS FOR AEROSPACE TESTING
    MIL-HDBK-217 Revision F:1991 RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT
    ANSI S2.11 : 69(R2001) AMERICAN NATIONAL STANDARD FOR THE SELECTION OF CALIBRATIONS AND TESTS FOR ELECTRICAL TRANSDUCERS USED FOR MEASURING SHOCK AND VIBRATION
    FAA AC 20-115 : 2017 AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
    ARINC 404A : 1974 AIR TRANSPORT EQUIPMENT CASES AND RACKING
    FAA AC 25-13 : 0 REDUCED AND DERATED TAKEOFF THRUST (POWER) PROCEDURES
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