During service, TBC can suffer degradation by CMAS, FOD, erosion or spallation.
Whereas the first three are due to foreign particles, the last one is related to thermal cycling. When
subjected to high temperature exposures followed by rapid coolings under oxidizing conditions, a
TBC system undergoes morphological changes and stress development. This will initiate cracks
which propagate and finally lead to failure by spallation. Consequently, the aim of the present study
is to understand better the mechanisms responsible for such spallation events. Two kinds of TBC
systems with different bond coatings (NiCoCrAlYTa or Pt-modified nickel aluminide bond
coatings) are thermally cycled. Subsequently, SEM investigations on TBC systems after spallation
concentrate on failure path, defect, morphological and microstructural changes to propose way for
improving TBC system lifetime.