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- W2318781617 abstract "The paper examines the adequacy of the U.S. Air Force damage tolerance inspection criterion for protecting the safety of the flight of an aging military trainer aircraft. This is done through a risk assessment based on cracks found in teardown inspections of retired wings. The crack population is combined with stress probabilities representing service experience to determine single flight probability of failure and the single aircraft probability of failure after a given time. These quantities are then used as a basis for judging the required inspection interval. For the case studied, the 0.9 probability of detection inspection criterion in the Air Force damage tolerance requirements may be nnconsewative." @default.
- W2318781617 created "2016-06-24" @default.
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- W2318781617 date "1984-05-14" @default.
- W2318781617 modified "2023-09-26" @default.
- W2318781617 title "Risk assessment of an aging military aircraft" @default.
- W2318781617 doi "https://doi.org/10.2514/6.1984-851" @default.
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