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  • SAE ARP 6461 : 2013

    View superseded by
    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
    View superseded by

    GUIDELINES FOR IMPLEMENTATION OF STRUCTURAL HEALTH MONITORING ON FIXED WING AIRCRAFT

    Available format(s):  Hardcopy, PDF

    Superseded date:  28-02-2024

    Language(s):  English

    Published date:  19-09-2013

    Publisher:  SAE International

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

    1. SCOPE
    2. REFERENCES
    3. INTRODUCTION TO AIRCRAFT STRUCTURES DESIGN AND
       MAINTENANCE
    4. ESSENTIAL ASPECTS OF STRUCTURAL HEALTH MONITORING
    5. SHM SYSTEM REQUIREMENTS
    6. VALIDATION AND VERIFICATION
    7. CERTIFICATION
    8. NOTES
    APPENDIX A - CONSIDERATIONS FOR SHM MILITARY APPLICATIONS
    APPENDIX B - RELATED PUBLICATIONS

    Abstract - (Show below) - (Hide below)

    Pertains to civil aerospace airframe structural applications where stakeholders are seeking guidance on the definition, development and certification of Structural Health Monitoring (SHM) technologies for aircraft health management applications.

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

    Committee G-11SHM
    Document Type Standard
    Publisher SAE International
    Status Superseded
    Superseded By

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

    RTCA DO 200B : 2015 STANDARDS FOR PROCESSING AERONAUTICAL DATA
    SAE ARP 5150 : 2013 SAFETY ASSESSMENT OF TRANSPORT AIRPLANES IN COMMERCIAL SERVICE
    RTCA DO 278 : A2011 SOFTWARE INTEGRITY ASSURANCE CONSIDERATIONS FOR COMMUNICATION, NAVIGATION, SURVEILLANCE AND AIR TRAFFIC MANAGEMENT (CNS/ATM) SYSTEMS
    RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
    RTCA DO-201A : 2000 STANDARDS FOR AERONAUTICAL INFORMATION
    MIL-HDBK-1823 Revision A:2009 NONDESTRUCTIVE EVALUATION SYSTEM, RELIABILITY ASSESSMENT
    MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
    SAE ARP 4754 : 2010 GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
    FAA AC 20-77 : 2016 USE OF MANUFACTURERS' MAINTENANCE MANUALS
    FAA AC 91-82 : 2012 FATIGUE MANAGEMENT PROGRAMS FOR IN-SERVICE ISSUES
    FAA AC 121-22 : 2012 MAINTENANCE REVIEW BOARDS, MAINTENANCE TYPE BOARDS, AND OEM/TCH RECOMMENDED MAINTENANCE PROCEDURES
    RTCA DO 254 : 2000 DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
    MIL-HDBK-781 Revision A:1996 RELIABILITY TEST METHODS, PLANS, AND ENVIRONMENTS FOR ENGINEERING DEVELOPMENT, QUALIFICATION AND PRODUCTION
    FAA AC 20-152 : 2005 RTCA, INC., DOCUMENT RTCA/DO-254, DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
    FAA AC 20-156 : 2006 AVIATION DATABUS ASSURANCE
    FAA AC 25-19 : 2011 CERTIFICATION MAINTENANCE REQUIREMENTS
    SAE ARP 4761 : 1996 GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT
    FAA AC 20-107 : 2009 COMPOSITE AIRCRAFT STRUCTURE
    FAA AC 25.1529-1 : 2007 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS OF STRUCTURAL REPAIRS ON TRANSPORT AIRPLANES
    FAA AC 25.571-1 : 2011 DAMAGE TOLERANCE AND FATIGUE EVALUATION OF STRUCTURE
    MIL-HDBK-217 Revision F:1991 RELIABILITY PREDICTION OF ELECTRONIC EQUIPMENT
    MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
    FAA 8110.37 : 2011 DESIGNATED ENGINEERING REPRESENTATIVE (DER) HANDBOOK
    FAA AC 20-65 : 0 U.S. AIRWORTHINESS CERTIFICATES AND AUTHORIZATIONS FOR OPERATION OF DOMESTIC AND FOREIGN AIRCRAFT
    FAA AC 29-2 : 2008 CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT
    ENV 13005 : DRAFT 1999 GUIDE TO THE EXPRESSION OF UNCERTAINTY IN MEASUREMENT
    MIL-STD-1472 Revision G:2012 HUMAN ENGINEERING
    ISO 5725:1986 Precision of test methods Determination of repeatability and reproducibility for a standard test method by inter-laboratory tests
    FAA AC 25.1309-1 : 0 SYSTEM DESIGN AND ANALYSIS
    FAA 8100.8 : 2011 DESIGNEE MANAGEMENT HANDBOOK
    FAA AC 20-115 : 2017 AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
    FAA AC 25.981-1 : 2008 FUEL TANK IGNITION SOURCE PREVENTION GUIDELINES
    SAE AIR 4175 : 2016 A GUIDE TO THE DEVELOPMENT OF A GROUND STATION FOR ENGINE CONDITION MONITORING
    FAA 8110.54 : 2010 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS RESPONSIBILITIES, REQUIREMENTS, AND CONTENTS
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