SAE AIR4175B
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
A GUIDE TO THE DEVELOPMENT OF A GROUND STATION FOR ENGINE CONDITION MONITORING
Hardcopy , PDF
12-11-2016
English
01-01-2016
FOREWORD
1 SCOPE
1.1 Purpose
2 REFERENCES
2.1 Applicable Documents
2.1.1 SAE Publications
2.2 Glossary of Terms
3 OPERATIONAL CONSIDERATIONS
4 SYSTEM FUNCTIONAL REQUIREMENTS
4.1 Exceedance/Event Diagnosis
4.2 Parameter Trending and Trend Analysis
4.3 Engine Parts Life Management
4.4 Flight Profile Monitoring
4.5 Data Storage
4.6 Initialization of On-Board Systems and Interface Devices
5 INPUT DATA
5.1 Continuous Recorded Flight Data
5.2 Processed Flight Data
5.3 Logistics Data
5.4 Maintenance Data
5.5 Data Validation
6 DATABASE MANAGEMENT SYSTEM
6.1 Database Structure
6.2 Size of Active Database
6.3 Data Archiving, Backup and Retrieval
6.4 Security and Storage
7 OUTPUT DATA REQUIREMENTS
7.1 Maintenance Data
7.2 Logistics Data
8 ADVANCED CAPABILITIES
8.1 Expert Troubleshooting Systems
8.2 Module Performance Analysis
8.3 Integrated Logistic Support Disciplines
8.4 On-Line Maintenance Manuals
9 USER CONSIDERATIONS
9.1 User Requirements Analysis
9.2 Human Factors
9.3 User Access Control Considerations
9.4 User Instruction
10 SYSTEM DEVELOPMENT CONSIDERATIONS
10.1 Software
10.2 Hardware
10.3 Supportability
10.4 Software/System Criticality
10.5 Integration With Other Systems
10.6 Software Documentation Requirements
10.7 System Testing
10.8 Updating System Software
11 NOTES
Reviews the main EMS functions and discusses the operating requirements used to determine the basis design of a GSS, including the interfaces with other maintenance or logistic systems.
Committee |
E-32
|
DocumentType |
Standard
|
Pages |
40
|
PublisherName |
SAE International
|
Status |
Withdrawn
|
SAE ARP 4176 : 2013 | DETERMINATION OF COSTS AND BENEFITS FROM IMPLEMENTING AN ENGINE HEALTH MANAGEMENT SYSTEM |
SAE ARP 6275 : 2014 | DETERMINATION OF COST BENEFITS FROM IMPLEMENTING AN INTEGRATED VEHICLE HEALTH MANAGEMENT SYSTEM |
SAE AIR 6212 : 2016 | USE OF HEALTH MONITORING SYSTEMS TO DETECT AIRCRAFT EXPOSURE TO VOLCANIC EVENTS |
SAE AS 4831 : 2009 | SOFTWARE INTERFACES FOR GROUND-BASED MONITORING SYSTEMS |
SAE ARP 1839 : 2015 | A GUIDE TO AIRCRAFT TURBINE ENGINE VIBRATION MONITORING SYSTEMS |
SAE ARP1587B | AIRCRAFT GAS TURBINE ENGINE HEALTH MANAGEMENT SYSTEM GUIDE |
SAE AIR4061C | GUIDELINES FOR INTEGRATING TYPICAL ENGINE HEALTH MANAGEMENT FUNCTIONS WITHIN AIRCRAFT SYSTEMS |
SAE ARP 6461 : 2013 | GUIDELINES FOR IMPLEMENTATION OF STRUCTURAL HEALTH MONITORING ON FIXED WING AIRCRAFT |
SAE AIR4061C | GUIDELINES FOR INTEGRATING TYPICAL ENGINE HEALTH MANAGEMENT FUNCTIONS WITHIN AIRCRAFT SYSTEMS |
SAE AIR 5120 : 2016 | ENGINE MONITORING SYSTEM RELIABILITY AND VALIDITY |
SAE AIR 1873 : 2016 | GUIDE TO LIMITED ENGINE MONITORING SYSTEMS FOR AIRCRAFT GAS TURBINE ENGINES |
SAE AIR 4174 : 2002 | A GUIDE TO AIRCRAFT POWER TRAIN MONITORING |
SAE AIR1839D | A GUIDE TO AIRCRAFT TURBINE ENGINE VIBRATION MONITORING SYSTEMS |
SAE AS4831A | SOFTWARE INTERFACES FOR GROUND-BASED MONITORING SYSTEMS |
SAE AIR1871C | LESSONS LEARNED FROM DEVELOPING, IMPLEMENTING, AND OPERATING A HEALTH MANAGEMENT SYSTEM FOR PROPULSION AND DRIVE TRAIN SYSTEMS |
SAE AS 8054 : 1996 | AIRBORNE ENGINE VIBRATION MONITORING (EVM) SYSTEM, GUIDELINES FOR PERFORMANCE STANDARD FOR |
SAE AIR1828B | GUIDE TO ENGINE LUBRICATION SYSTEM MONITORING |
SAE ARP1587B | AIRCRAFT GAS TURBINE ENGINE HEALTH MANAGEMENT SYSTEM GUIDE |
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