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contributor authorR. W. Cue
contributor authorD. E. Muir
date accessioned2017-05-08T23:35:33Z
date available2017-05-08T23:35:33Z
date copyrightJanuary, 1991
date issued1991
identifier issn1528-8919
identifier otherJETPEZ-26683#11_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/108562
description abstractThe 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.
publisherThe American Society of Mechanical Engineers (ASME)
titleEngine Performance Monitoring and Troubleshooting Techniques for the CF-18 Aircraft
typeJournal Paper
journal volume113
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2906519
journal fristpage11
journal lastpage19
identifier eissn0742-4795
keywordsEngines
keywordsCarbon fibers
keywordsAircraft
keywordsMaintenance
keywordsForce
keywordsFlight
keywordsComputer software AND Condition monitoring
treeJournal of Engineering for Gas Turbines and Power:;1991:;volume( 113 ):;issue: 001
contenttypeFulltext


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