SAE ARP6275
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Determination of Cost Benefits from Implementing an Integrated Vehicle Health Management System
Hardcopy , PDF
22-02-2021
English
07-07-2014
1. SCOPE
2. REFERENCES
3. ACRONYMS
4. INTRODUCTION
5. FACTORS INFLUENCING COST BENEFIT STUDIES
AND ANALYSES
6. COSTS FOR CONSIDERATION IN AN AIRCRAFT
PHM COST BENEFIT STUDY
7. BENEFITS FOR CONSIDERATION IN AN AIR VEHICLE
PHM COST BENEFIT STUDY
8. CHALLENGES ASSOCIATED WITH COMPLETING A
COST BENEFIT STUDY
9. EXAMPLES OF PHM IMPLEMENTATION AND COST
ANALYSIS MODELS
10. SUMMARY
11. NOTES
Gives insights on how to perform a cost benefit analysis (CBA) to determine the return on investment that would result from implementing an integrated Health Management (HM) system on an air vehicle.
DocumentType |
Standard
|
Pages |
34
|
PublisherName |
SAE International
|
Status |
Superseded
|
SupersededBy |
This ARP provides insights on how to perform a cost benefit analysis (CBA) to determine the return on investment that would result from implementing an integrated Health Management (HM) system on an air vehicle. The word “integrated” refers to the combination or “roll up” of sub-systems health management tools to create a platform centric system. The document describes the complexity of features that can be considered in the analysis, the different tools and approaches for conducting a CBA and differentiates between military and commercial applications. This document is intended to help those who might not necessarily have a deep technical understanding or familiarity with HM systems but want to either quantify or understand the economic benefits (i.e., the value proposition) that a HM system could provide. Prognostics is a capability within some HM systems that provides an estimation of remaining useful life (RUL) or time to failure and so Prognostic Health Management (PHM) is used where this predictive element exists. IVHM refers to an integrated vehicle level system deployed on a fleet of platforms and might, but not necessarily, include predictive elements.
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SAE JA6268_201804 | Design & Run-Time Information Exchange for Health-Ready Components |
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SAE ARP5120 | Aircraft Gas Turbine Engine Health Management System Development and Integration Guide |
SAE AIR4174A | A Guide to Aircraft Power Train Monitoring |
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 |
SAE AIR4061C | Guidelines for Integrating Typical Engine Health Management Functions Within Aircraft Systems |
RTCA DO 254 : 2000 | DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE |
SAE AIR5871 | Prognostics for Gas Turbine Engines |
RTCA DO 248 : C2011 | SUPPORTING INFORMATION FOR DO-178C AND DO-278A |
SAE ARP4176A | Determination of Costs and Benefits from Implementing an Engine Health Management System |
SAE AIR4175B | A Guide to the Development of a Ground Station for Engine Condition Monitoring |
SAE AIR1871C | Lessons Learned from Developing, Implementing, and Operating a Health Management System for Propulsion and Drive Train Systems |
SAE ARP1587B | Aircraft Gas Turbine Engine Health Management System Guide |
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