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SAE AIR4175B

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.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

Available format(s)

Hardcopy , PDF

Withdrawn date

12-11-2016

Language(s)

English

Published date

01-01-2016

€150.75
Excluding VAT

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Withdrawn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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