1. Introduction
Life usage monitoring (LUM) of fracture critical parts is considered to have a great potential to save costs without compromising flight safety. The general ideas of LUM are now well established and have been documented in comprehensive reports [1], [2]. Although some of the existing systems have proved their cost effectiveness and are well accepted by their users, the need for continued adaptations of LUM algorithms to the experience gained during fleet operation and to changes of engine hardware requires an unexpectedly high amount of system maintenance.