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RESEARCH PAPERS

Engine Performance Monitoring and Troubleshooting Techniques for the CF-18 Aircraft

[+] Author and Article Information
R. W. Cue

Canadian Forces, Ottawa, Canada

D. E. Muir

GasTOPS Ltd., Ottawa, Canada

J. Eng. Gas Turbines Power 113(1), 11-19 (Jan 01, 1991) (9 pages) doi:10.1115/1.2906519 History: Received January 23, 1990; Online April 24, 2008

Abstract

The F404-GE-400 engines of the CF-18 aircraft are the first engines of the Canadian Forces to be maintained under a formal on-condition maintenance program. In support of this program, the Canadian Forces are developing advanced troubleshooting and performance monitoring procedures based on information recorded by the aircraft In-flight Engine Condition Monitoring System (IECMS). A suite of computer programs has been developed that enables maintenance personnel to access, display, and analyze in-flight event data recorded by the IECMS and to track the performance of individual engines based on “health indices” derived from the IECMS take-off ground roll recordings. The new techniques have been under evaluation at each of the CF-18 main operating bases for a period of approximately 14 months. Results to date indicate that the IECMS recordings provide a considerable amount of information of benefit to engine technicians and maintenance planners.

Copyright © 1991 by The American Society of Mechanical Engineers
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