A case study of failure mode and effects analysis for aircraft turbine engine

Arthasartsri, S and Ren, H 2009, 'A case study of failure mode and effects analysis for aircraft turbine engine', in Thirteenth Australian International Aerospace Congress AIAC-13, Melbourne, Australia, 9-12 March 2009, pp. 1-9.


Document type: Conference Paper
Collection: Conference Papers

Title A case study of failure mode and effects analysis for aircraft turbine engine
Author(s) Arthasartsri, S
Ren, H
Year 2009
Conference name AIAC-13 Thirteenth Australian International Aerospace Congress
Conference location Melbourne, Australia
Conference dates 9-12 March 2009
Proceedings title Thirteenth Australian International Aerospace Congress AIAC-13
Publisher Defence Science and Technology Organisation
Place of publication Melbourne, Australia
Start page 1
End page 9
Total pages 9
Abstract Failure Mode and Effects Analysis (FMEA) and Reliability Centred Maintenance (RCM) decision logic have been effectively applied by commercial and military aviation industry for over four decades to develop maintenance program for new aircraft and its systems. It is used to analyse the reliability, maintainability and safety of the aircraft. In this case study, the analysis of aircraft engine FMEA emphasis on engine structure level, based on its major modules and functions. This paper presents the analysis procedure of FMEA with the result worksheets using RCMcost Simulation Software. The application of this engine FMEA analysis is also implemented in maintenance simulation hence yield the results of cost optimization and the best selection of the maintenance program strategy.
Subjects Aerospace Structures
Air Transportation and Freight Services
Keyword(s) FEMA
engine maintenance
failure analysis
GP7200 engine
failure analysis introduction system
ISBN 9780980321555
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