DocumentCode :
3466466
Title :
Application of integrated diagnostic process to non-avionics systems
Author :
Gartner, Don L. ; Dibbert, Stephen E.
Author_Institution :
Boeing Co., Seattle, WA, USA
fYear :
2001
fDate :
2001
Firstpage :
229
Lastpage :
238
Abstract :
Most efforts to improve the diagnostic performance of military aircraft systems/subsystems and off-aircraft maintenance have focused mainly on avionics systems/subsystems. From that effort a process (Integrated Diagnostics) has evolved to address some of the major contributors to poor diagnostic performance and has been implemented at The Boeing Company with demonstrated success. Even though the tools used were developed based on avionics, the tools should benefit non-avionics systems. This paper documents the results of applying those tools to a fighter aircraft hydraulic system
Keywords :
aircraft instrumentation; aircraft maintenance; aircraft testing; fault diagnosis; hydraulic systems; military aircraft; ADVISE; Boeing Company; ambiguity groups; failure modes; fault detection/isolation; fighter aircraft hydraulic system; integrated diagnostic process; military aircraft subsystems; military aircraft systems; nonavionics systems; prognostics; testability; Aerospace electronics; Cost function; Fault detection; Hardware; Hydraulic systems; Isolation technology; Military aircraft; Supply chains; System testing; Weapons;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
AUTOTESTCON Proceedings, 2001. IEEE Systems Readiness Technology Conference
Conference_Location :
Valley Forge, PA
ISSN :
1080-7225
Print_ISBN :
0-7803-7094-5
Type :
conf
DOI :
10.1109/AUTEST.2001.948967
Filename :
948967
Link To Document :
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