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Defects

Fatigue Crack — Definition & NDT Use

A crack initiated and propagated by repeated cyclic loading below the static yield strength of material. Fatigue cracks typically initiate at stress concentrations (welds, notches) and propagate gradually until sudden failure occurs. NDT methods like eddy current and liquid penetrant are excellent for detecting surface fatigue cracks. Early detection is critical in fatigue-critical applications like aircraft and rotating machinery.

How Fatigue Crack Works in Practice

In service, Fatigue Crack starts as a discontinuity that may or may not breach the acceptance criteria of the governing code; the NDT method's job is to detect it, characterise it, and size it so an engineer can decide whether to repair, monitor, or accept. Capillary action draws the penetrant into surface-breaking openings during the dwell; emulsifier or solvent removes the surface excess; the developer then provides a contrasting blotter that pulls the trapped penetrant back out, broadening the indication so it becomes visible to the inspector. As the alternating coil approaches the conductive surface it drives circulating eddy currents; any change in the part — a crack, a thickness change, a permeability shift — perturbs those currents and registers as a phase-and-amplitude shift on the impedance plane. Crack sizing is the high-stakes call: amplitude alone is not enough, so techniques such as TOFD, tip-diffraction, or 6dB drop are stacked to bound the height and length used in the engineering critical assessment. The fitness-for-service decision typically pairs the NDT call with material data and stress information; the inspector's job is to give the engineer a clean characterisation rather than to make the keep-or-reject call alone.

When to Apply It

The decision tree around Fatigue Crack runs: detect, characterise, size, and refer to the acceptance table in the governing code; only the last step decides repair, accept-as-is, or fitness-for-service review. On welded fabrication it is most often paired with VT and one volumetric method (RT or UT) so surface and internal defects are both addressed. Whenever a crack is suspected the inspection plan upgrades from screening to characterisation — TOFD, MT, or tip-diffraction sizing — because the engineering critical assessment needs height and length, not just a yes/no.

Related Standards & Code References
  • AWS D1.1

    Structural Welding Code — Steel; defines visual and NDE acceptance for static and dynamically loaded welds.

  • ASME Section IX

    Welding, brazing, and fusing qualifications referenced by every U.S. pressure-equipment code.

  • ASTM E165 / E1417

    Standard practice for liquid penetrant testing.

  • ISO 3452

    Non-destructive testing — penetrant testing (general principles).

Common Mistakes & Misconceptions

Confusing fatigue crack with a generic "indication" is a recurring error; the term carries an engineering implication, and the report should distinguish the discontinuity (what was seen) from the disposition (what code says about it).

Frequently Asked

What does "Fatigue Crack" mean in NDT?

A crack initiated and propagated by repeated cyclic loading below the static yield strength of material. Fatigue cracks typically initiate at stress concentrations (welds, notches) and propagate gradually until sudden failure occurs

Is fatigue crack always rejectable?

No. Whether a fatigue crack indication is rejectable depends on the acceptance criteria of the governing code (AWS D1.1, ASME Section VIII, API 1104, etc.), the size and orientation of the indication, and any fitness-for-service evaluation the engineer chooses to apply.

What other NDT concepts should I read alongside Fatigue Crack?

The most directly related entries in this glossary are "crack", "stress concentration", "cyclic loading"; reading those together gives you the surrounding vocabulary used in inspection reports and procedures.

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