SAE ARP6461
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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
Hardcopy , PDF
28-02-2024
English
19-09-2013
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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
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.
| DocumentType |
Standard
|
| Pages |
95
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
This document is applicable 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.For the purpose of this document, SHM is defined as “the process of acquiring and analyzing data from on-board sensors to evaluate the health of a structure.” The suite of on-board sensors could include any presently installed aircraft sensors as well as new sensors to be defined in the future.
| RTCA DO 200B : 2015 | STANDARDS FOR PROCESSING AERONAUTICAL DATA |
| SAE ARP5150 | 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 ARP4754A | 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 ARP4761 | GUIDELINES AND METHODS FOR CONDUCTING 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 AIR4175B | 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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