SAE ARP5120
Current
The latest, up-to-date edition.
Aircraft Gas Turbine Engine Health Management System Development and Integration Guide
Hardcopy , PDF
English
05-03-2016
1. SCOPE
2. REFERENCES
3. CONCEPTS AND CONSIDERATIONS
4. RECOMMENDED PRACTICES FOR DESIGN, DEVELOPMENT,
AND TEST
5. RECOMMENDED PRACTICES FOR IMPLEMENTATION
6. CONCLUSION
7. NOTES
APPENDIX A - HEALTH MANAGEMENT STANDARDS
APPENDIX B - SENSOR PARAMETER AND SIGNAL PERFORMANCE
REQUIREMENTS (SENSE/ACQUIRE)
APPENDIX C - EXAMPLE EGT MARGIN CALCULATION
APPENDIX D - DATA MANIPULATION DESIGN AND PERFORMANCE
REQUIREMENTS (ANALYSIS/ACT)
Gives recommended best practices, procedures, and technology to guide the physical and functional design, development, integration, verification, and validation of highly reliable Engine Health Management (EHM) systems for aircraft engines and Auxiliary Power Units (APUs).
DevelopmentNote |
Supersedes SAE AIR 4061, SAE AIR 4175 & SAE AIR 5120. (11/2016) Supersedes SAE AIR 1873. (12/2016)
|
DocumentType |
Standard
|
Pages |
87
|
PublisherName |
SAE International
|
Status |
Current
|
ARP5120 provides recommended best practices, procedures, and technology to guide the physical and functional design, development, integration, verification, and validation of highly reliable Engine Health Management (EHM) systems for aircraft engines and Auxiliary Power Units (APUs). This SAE Aerospace Recommended Practice (ARP) also serves as a concise reference of considerations, approaches, activities, and requirements for producing the end-to-end engine health management system comprised of both on and off-board subsystems for the sensing, acquisition, analysis, detection, and data handling functions for EHM. These functions may also be used to effect continued operation or return to service decisions when demonstrated as compliant with the applicable airworthiness requirements defined by the responsible Aviation Authority. Where practical, this document delineates between military and commercial practices.
SAE AIR4174A | A Guide to Aircraft Power Train Monitoring |
SAE AIR5317 | A Guide to APU Health Management |
RTCA DO 278 : A2011 | SOFTWARE INTEGRITY ASSURANCE CONSIDERATIONS FOR COMMUNICATION, NAVIGATION, SURVEILLANCE AND AIR TRAFFIC MANAGEMENT (CNS/ATM) SYSTEMS |
RTCA DO 330 : 2011 | SOFTWARE TOOL QUALIFICATION CONSIDERATIONS |
RTCA DO 178 : C2011 | SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION |
MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
GEIA HB 649 : 2005 | CONFIGURATION MANAGEMENT STANDARD IMPLEMENTATION GUIDE |
MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
SAE ARP4754A | Guidelines for Development of Civil Aircraft and Systems |
RTCA DO 254 : 2000 | DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
SAE AIR1873A | Guide to Limited Engine Monitoring Systems for Aircraft Gas Turbine Engines |
SAE ARP4761 | GUIDELINES AND METHODS FOR CONDUCTING THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT |
MIL-STD-464 Revision C:2010 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS |
SAE ARP 5783 : 2012 | HEALTH AND USAGE MONITORING METRICS, MONITORING THE MONITOR |
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 |
EIA 836 CD : B2010(R2015) | CONFIGURATION MANAGEMENT DATA EXCHANGE AND INTEROPERABILITY |
RTCA DO 248 : C2011 | SUPPORTING INFORMATION FOR DO-178C AND DO-278A |
SAE ARP6275 | Determination of Cost Benefits from Implementing an Integrated Vehicle Health Management System |
IEEE 1012-2012 | IEEE Standard for System and Software Verification and Validation |
RTCA DO 333 : 2011 | FORMAL METHODS SUPPLEMENT TO DO-178C AND DO-278A |
JSSG-2010-2 Base Document:1998 | Crew Systems Crew Station Automation, Information and Control/Display Management Handbook |
RTCA DO 331 : 2011 | MODEL-BASED DEVELOPMENT AND VERIFICATION SUPPLEMENT TO DO-178C AND DO-278A |
GEIA STD 0009 : 2008 | RELIABILITY PROGRAM STANDARD FOR SYSTEMS DESIGN, DEVELOPMENT AND MANUFACTURING |
IEEE 1451.0 : 2007 | SMART TRANSDUCER INTERFACE FOR SENSORS AND ACTUATORS - COMMON FUNCTIONS, COMMUNICATION PROTOCOLS, AND TRANSDUCER ELECTRONIC DATA SHEET (TEDS) FORMATS |
MIL-HDBK-470 Revision A:1997 | Designing and Developing Maintainable Products and Systems, Volume I |
IEEE 1362-1998 | IEEE Guide for Information Technology - System Definition - Concept of Operations (ConOps) Document |
SAE ARP4176A | Determination of Costs and Benefits from Implementing an Engine Health Management System |
SAE AS8034B | Minimum Performance Standard for Airborne Multipurpose Electronic Displays |
ASD S2000M : 2005 | INTERNATIONAL SPECIFICATION FOR MATERIAL MANAGEMENT - INTEGRATED DATA PROCESSING |
GEIA EIA649B:2011 | CONFIGURATION MANAGEMENT STANDARD |
SAE ARP 4102 : 1988 | FLIGHT DECK PANELS, CONTROLS, AND DISPLAYS |
SAE ARP1587B | Aircraft Gas Turbine Engine Health Management System Guide |
RTCA DO 332 : 2011 | OBJECT-ORIENTED TECHNOLOGY AND RELATED TECHNIQUES SUPPLEMENT TO DO-178C AND DO-278A |
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