Cost Based Risk Analysis to Identify Inspection and Restoration Intervals of Hidden Failures Subject to Aging
This paper develops a cost rate function (CRF) to identify the optimum interval and frequency of inspection and restoration of aircraft's repairable components which are undergoing aging, and whose failures are hidden, i.e. are detectable by inspection or upon demand. The paper considers two pr...
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| Published in | IEEE transactions on reliability Vol. 60; no. 1; pp. 197 - 209 |
|---|---|
| Main Authors | , |
| Format | Journal Article |
| Language | English |
| Published |
New York
IEEE
01.03.2011
The Institute of Electrical and Electronics Engineers, Inc. (IEEE) |
| Subjects | |
| Online Access | Get full text |
| ISSN | 0018-9529 1558-1721 1558-1721 |
| DOI | 10.1109/TR.2011.2104530 |
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| Abstract | This paper develops a cost rate function (CRF) to identify the optimum interval and frequency of inspection and restoration of aircraft's repairable components which are undergoing aging, and whose failures are hidden, i.e. are detectable by inspection or upon demand. The paper considers two prevalent strategies, namely Failure Finding Inspection (FFI), and a combination of FFI with restoration actions (FFI+Res), for both the "non-safety effect," and the "safety effect" categories of hidden failures. As-bad-as-old (ABAO) inspection effectiveness, and as-good-as-new (AGAN) restoration effectiveness are considered. In case of repair due to findings by inspection, as-bad-as-old repair effectiveness is considered. The proposed method considers inspection and repair times, and takes into account the costs associated with inspection, repair, and restoration; and the potential losses due to the inability to use the aircraft (maintenance downtime). It also considers the cost associated with accidents caused by the occurrence of multiple failure. The approach used in this study for risk constraint optimization is based on the mean fraction of time during which the unit is not functioning within inspection intervals (MFDT), and the average interval unavailability behavior within the restoration period. In the case of an operational limit, when it is not possible to remove the unit for restoration, or one needs to use the unit longer than the expected operating time, the paper introduces an approach to analyzing the possibility of and conditions for providing an extension to the restoration interval that satisfies the risk constraints and the business requirements at the same time. |
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| AbstractList | The analytical model presented in this paper aims to study possible maintenance strategies considering risk constrains, to preserve or assure availability of hidden functions of a repairable unit in aircraft systems considering ageing effect. The paper discusses two known strategies for hidden failure management aviation and other high risk industries, namely Failure Finding Inspection (FFI), and a combination of a series of FFI and restoration after a specific number of FFI cycles ( i.e., FFI-Rs strategy). Based on discussions, the paper introduces a new approach named Dynamic Failure Finding Inspection strategy (DFFI) to assure the acceptable level of risk and also the unit's hidden function availability continuously . The paper presents analytical methods to estimate optimal FFI, and optimal thresholds for restoration of degradation (refreshing risk level) within FFI-Rs strategy. It also discusses criteria used to select appropriate thresholds to change the FFI intervals within DFFI strategy, i.e. reducing inspection intervals after specific thresholds, to reduce the risk. The method is based on the mean proportion of time i.e. (Mean Functional Dead Time, MFDT) that the unit is not functioning during the inspection intervals and the average unavailability behavior within the restoration/discard period. The proposed method considers inspection, repair, and restoration times, and takes in to account costs associated with inspection, repair, restoration, potential losses due to non-availability of aircraft due to maintenance downtime or accident often caused multiple failures. This paper develops a cost rate function (CRF) to identify the optimum interval and frequency of inspection and restoration of aircraft's repairable components which are undergoing aging, and whose failures are hidden, i.e. are detectable by inspection or upon demand. The paper considers two prevalent strategies, namely Failure Finding Inspection (FFI), and a combination of FFI with restoration actions (FFI + Res), for both the "non-safety effect," and the "safety effect" categories of hidden failures. As-bad-as-old (ABAO) inspection effectiveness, and as-good-as-new (AGAN) restoration effectiveness are considered. In case of repair due to findings by inspection, as-bad-as-old repair effectiveness is considered. The proposed method considers inspection and repair times, and takes into account the costs associated with inspection, repair, and restoration; and the potential losses due to the inability to use the aircraft (maintenance downtime). It also considers the cost associated with accidents caused by the occurrence of multiple failure. The approach used in this study for risk constraint optimization is based on the mean fraction of time during which the unit is not functioning within inspection intervals (MFDT), and the average interval unavailability behavior within the restoration period. In the case of an operational limit, when it is not possible to remove the unit for restoration, or one needs to use the unit longer than the expected operating time, the paper introduces an approach to analyzing the possibility of and conditions for providing an extension to the restoration interval that satisfies the risk constraints and the business requirements at the same time. This paper develops a cost rate function (CRF) to identify the optimum interval and frequency of inspection and restoration of aircraft's repairable components which are undergoing aging, and whose failures are hidden, i.e. are detectable by inspection or upon demand. The paper considers two prevalent strategies, namely Failure Finding Inspection (FFI), and a combination of FFI with restoration actions (FFI[Formula Omitted]Res), for both the "non-safety effect," and the "safety effect" categories of hidden failures. As-bad-as-old (ABAO) inspection effectiveness, and as-good-as-new (AGAN) restoration effectiveness are considered. In case of repair due to findings by inspection, as-bad-as-old repair effectiveness is considered. The proposed method considers inspection and repair times, and takes into account the costs associated with inspection, repair, and restoration; and the potential losses due to the inability to use the aircraft (maintenance downtime). It also considers the cost associated with accidents caused by the occurrence of multiple failure. The approach used in this study for risk constraint optimization is based on the mean fraction of time during which the unit is not functioning within inspection intervals (MFDT), and the average interval unavailability behavior within the restoration period. In the case of an operational limit, when it is not possible to remove the unit for restoration, or one needs to use the unit longer than the expected operating time, the paper introduces an approach to analyzing the possibility of and conditions for providing an extension to the restoration interval that satisfies the risk constraints and the business requirements at the same time. |
| Author | Ahmadi, A Kumar, U |
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| References | ref12 ref14 nowlan (ref1) 1978 rausand (ref17) 2004 barroeta (ref13) 2005 (ref5) 2007 ref11 kumar (ref2) 2008 ref10 ascher (ref15) 1984 jardine (ref6) 2006 ref7 (ref18) 1994 ref9 ebeling (ref4) 1997 andrews (ref3) 2006 modarres (ref16) 2006 aven (ref19) 2007; 3 rigdon (ref8) 2000 |
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| SubjectTerms | Aging Aging aircraft Aircraft Aircraft components Atmospheric modeling Availability Combination of maintenance strategy cost rate function Drift och underhållsteknik Failure failure finding inspection hidden failures Inspection inspection interval interval extension Intervals Maintenance engineering mean fractional dead time multiple failure Operation and Maintenance Repair Repair & maintenance Restoration restoration task Risk risk constraint optimization Safety |
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| Title | Cost Based Risk Analysis to Identify Inspection and Restoration Intervals of Hidden Failures Subject to Aging |
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