it is simply not true in relation to fast jet engines - you are tracing both cycles and flight hours with split on work regimes - it means time of normal work, military power and afterburner work is noted separately and used for overhaul schedule establishing to make things more difficult also calendar is used to establish life limits for specific engine parts, and in fact does no matter if you are speaking about western and eastern engines of course there are nuances in a way of making calculations, methodology on west is much more flexible - especially in relation to newer generation of engines equipped in digital control and advanced health monitoring systems - but simple statement that western engines are in "on condition maintenance" is a kind of understatementBut turbine engines are overhauled on cycles, not hours, and every engine start is a cycle.
In very simple terms this is because every start causes shock heating of the hot section components and every shutdown causes shock cooling. These stress the materials used which results in failures