The fracture surface is the black box of a failure: reading its marks reveals the root cause
A machine component that breaks in service carries the story of its failure on the fracture surface: where the crack started, how it propagated, the type and magnitude of the load, and even manufacturing defects in the material can be read from it. Failure analysis evaluates these marks with systematic methods to establish the root cause — the goal is not to assign blame, but to prevent the failure from recurring.
A failure investigation is not about assigning blame; it is about producing a single, consistent scenario that explains every observation, so that the same part does not break again. A broken component carries its own history on its fracture surface — where the crack started, how it grew, how highly it was stressed and often how long it took. The work consists of reading that record without destroying it.
The sequence matters, because each step decides where the next one takes its sample, and because the irreversible operations (cutting, etching, mechanical testing) can only be done once.
| Type | Macro appearance | Micro mechanism | Typical condition |
|---|---|---|---|
| Ductile | Visible plastic deformation, necking, 45° shear lip, dull fibrous surface | Microvoid coalescence (dimples) | Overload, tough material |
| Brittle | No deformation, flat bright crystalline surface, chevron marks | Cleavage or intergranular separation | Impact, low temperature, high hardness, notch |
| Fatigue | Flat propagation zone with beach marks, small final fracture area | Cyclic slip, striations | Repeated load far below static strength |
| Environmental | Discolouration, branched cracks, corrosion products | SCC, hydrogen embrittlement, corrosion fatigue | Corrosive medium plus tensile stress |
The majority of service failures are fatigue: machines are rarely overloaded once, but they are loaded and unloaded millions of times. That is why macro fractography concentrates on reading fatigue marks.
Beach marks are the arrest lines of the crack front; they curve around the origin, so they point back to where the failure started. Ratchet marks — steps between adjacent origins — count the starting points: many origins mean a high stress concentration or a very high nominal stress.
The ratio of the final fracture area to the total section is the single most informative measurement on the surface. A small final zone means the part was lightly stressed and the crack grew for a long time; a large final zone means the nominal stress was high. Combined with the number of origins, this separates a design problem from an overload event before any laboratory work begins.
In the SEM, dimples indicate ductile tearing, cleavage facets with river patterns indicate brittle transgranular fracture, and smooth grain facets indicate intergranular failure — which always demands an explanation: temper embrittlement, hydrogen, SCC, creep or grain-boundary films. Striations confirm fatigue but are frequently obliterated by rubbing, corrosion or post-failure damage, so their absence proves nothing. EDS identifies foreign elements (chlorine, sulphur, sodium) that point to the environment, but it analyses what is on the surface now — including contamination introduced after the failure.
A defensible report separates observations from interpretation, states the methods and standards used, shows scaled images, and ends with corrective actions that are specific enough to implement. Any finding that does not fit the conclusion is reported with its explanation — that is what distinguishes an investigation from an argument.
The technical note below (A4 PDF, in Turkish) develops these subjects in depth with original diagrams prepared for this series.