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SAE ARP5120

Current

Current

The latest, up-to-date edition.

Aircraft Gas Turbine Engine Health Management System Development and Integration Guide

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

05-03-2016

€172.29
Excluding VAT

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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