home  /  insights  /  delayed-brittle-fracture-in-high-strength-bolts
Mechanical & Component

Delayed brittle fracture in high-strength bolts

Hydrogen embrittlement and stress corrosion cracking both produce delayed, largely intergranular fastener fractures. Fractography, hardness and the plating record separate them.

July 30, 2026 · 8 min read

The short answer

A delayed brittle fracture in a high-strength bolt is usually attributed to one of two dominant mechanisms, hydrogen embrittlement or stress corrosion cracking, which produce fracture surfaces similar enough that they are routinely confused. Separating them is a matter of fractography, hardness, process history and environment, in roughly that order. Internal hydrogen embrittlement needs hydrogen already in the steel at installation, a susceptible high-strength microstructure and the sustained stress of the preload, and the fracture happens with no external agent at all; stress corrosion cracking needs an environment in continuing contact with the metal and leaves corrosion product in and around the crack, often with branched secondary cracking. Hardness and tensile testing show whether the bolt was heat treated to the grade stamped on its head, and the plating and baking record makes or breaks a hydrogen hypothesis. The distinction matters because hydrogen embrittlement and stress corrosion cracking point at very different parties.

What this article establishes

  • A high-strength bolt that fractures under an essentially static clamp load, with no cycling and almost no ductility, days or months after installation, points to an environmentally assisted mechanism such as hydrogen embrittlement or stress corrosion cracking rather than ductile overload or fatigue, and timing alone will not separate the two.
  • Internal hydrogen embrittlement needs no external agent, only hydrogen already in the steel at installation (introduced during acid pickling, electroplating or melting), a susceptible microstructure (generally a quenched and tempered high-strength steel), and the sustained tensile stress of the preload, whereas stress corrosion cracking needs an environment in continuing contact with the metal and stops when that environment is removed.
  • Hydrogen embrittlement and stress corrosion cracking both commonly produce intergranular fracture in quenched and tempered steel, so fracture appearance alone is not enough; the location of the crack origin matters as much as the fracture morphology.
  • Fasteners around 1,000 MPa tensile strength and above are where internal hydrogen embrittlement is a live concern, and hardness and tensile testing under ASTM F606/F606M shows whether a bolt was heat treated to its marked grade; an over-hard bolt moves attention toward the manufacturer.
  • Plating line records, bake time and temperature, the interval between plating and baking, and the lot certification make or break a hydrogen embrittlement hypothesis, while confirmatory tests such as ASTM F1624 and ISO 15330 establish whether a mechanism was available at all, not what happened to the failed part.
  • A delayed bolt fracture opinion that states which mechanisms were considered, which were excluded and on what evidence survives the challenges such opinions predictably face; a conclusion resting on the appearance of a single fracture surface does not.

What does it mean when a correctly installed high-strength bolt breaks a week later?

When a high-strength bolt that was torqued correctly and passed inspection splits in two a week later, something was driving a crack while the joint sat still, which makes it a different forensic problem from a bolt that broke under load. That delay narrows the field immediately. Two mechanisms dominate delayed fracture of high-strength bolts, hydrogen embrittlement and stress corrosion cracking, and they produce fracture surfaces similar enough that they are routinely confused.

Hydrogen embrittlement and stress corrosion cracking also point at very different parties. Separating the two mechanisms in a failed bolt is a matter of fractography, hardness, process history and environment, in roughly that order.

Why is the delay before a bolt fractures the first clue to what caused it?

The delay is the first clue because a bolt that fractures under an essentially static clamp load, with no cycling and almost no ductility, has been cracking slowly for reasons that neither ductile overload nor fatigue explains. Ductile overload of a bolt is immediate and obvious: gross plastic deformation, necking or thread stripping, shear lips, and a dimpled surface under the electron microscope. Fatigue is progressive but requires cyclic loading and leaves beach marks recording it.

What remains for a delayed bolt fracture is an environmentally assisted mechanism, in which sustained tensile stress well below yield drives a crack that would not otherwise propagate. Both hydrogen embrittlement and stress corrosion cracking fit that description, and timing alone will not separate them: either mechanism can surface days or months after the bolt was installed.

What does hydrogen embrittlement need in order to crack a bolt?

Internal hydrogen embrittlement of a bolt needs three things: hydrogen already in the steel at installation, a susceptible microstructure, and sustained tensile stress. The hydrogen is introduced during acid pickling, electroplating or melting; the susceptible microstructure is generally a quenched and tempered high-strength steel; and the sustained tensile stress is supplied by the bolt preload itself. Hydrogen migrates to regions of high triaxial stress, typically the first engaged thread root or the head-to-shank fillet.

The signature of internal hydrogen embrittlement is delay with no external agent at all: the bolt is dry, the environment is benign, and the fracture happens anyway. Where the fastener was electroplated and post-plate baking was omitted or delayed, ASTM B850 and ISO 4042 describe the relief treatment that should have followed.

What does stress corrosion cracking need that hydrogen embrittlement does not?

Stress corrosion cracking of a bolt needs something internal hydrogen embrittlement does not: an environment in continuing contact with the metal, such as chlorides, sulfides, caustics, or moisture concentrated in a crevice beneath a washer. Like hydrogen embrittlement, stress corrosion cracking also needs sustained stress and a susceptible alloy. Remove the environment and a stress corrosion crack stops, whereas hydrogen already dissolved in the steel needs nothing further from outside.

That dependence on the environment is the practical discriminator between stress corrosion cracking and internal hydrogen embrittlement. Stress corrosion cracking leaves corrosion product in and around the crack, often branched secondary cracking away from the main fracture, and attack consistent with the service exposure. A recently installed bolt in a clean, dry interior joint is a poor candidate for stress corrosion cracking.

Can the fracture surface alone tell hydrogen embrittlement from stress corrosion cracking in a bolt?

No, the appearance of a bolt fracture surface alone is not enough, because hydrogen embrittlement and stress corrosion cracking both commonly produce intergranular fracture in quenched and tempered steel. A hydrogen embrittlement fracture typically shows relatively clean intergranular facets with tear ridges and little corrosion product near the origin. A stress corrosion cracking surface is usually oxidized and branched, and may be transgranular depending on alloy and environment.

The location of the fracture origin matters as much as the fracture morphology. Hydrogen embrittlement cracking initiates subsurface or wherever triaxial stress peaks; stress corrosion cracking initiates where the environment reached the metal, often a pit, a crevice, or a coating breach.

Which bolts are susceptible to hydrogen embrittlement, and what does hardness testing show?

Fasteners around 1,000 MPa tensile strength and above are the population in which internal hydrogen embrittlement is a live concern, because sensitivity to hydrogen rises steeply with strength. That population covers SAE J429 Grade 8, ISO 898-1 property classes 10.9 and 12.9, and comparable aerospace alloys.

Hardness and tensile testing of a failed fastener under ASTM F606/F606M answers a second question: whether the fastener was heat treated to the grade stamped on its head. An over-hard bolt is more brittle than the design assumed and far more sensitive to hydrogen, and that finding moves attention toward the manufacturer.

What records make or break a hydrogen embrittlement explanation for a failed bolt?

The documents that make or break a hydrogen embrittlement hypothesis for a failed bolt are the plating line records, the bake time and temperature, the interval between plating and baking, and the lot certification. ASTM F1940 covers process control verification for plated fasteners, and ASTM F519 covers the specimen-based evaluation of plating and coating processes.

Where a bolt was zinc-electroplated and installed within a shift with no relief bake recorded, the hydrogen embrittlement hypothesis is testable rather than speculative. Where a bolt was mechanically galvanized, the internal hydrogen route is far less available.

What can confirmatory testing establish about a delayed bolt fracture?

Confirmatory testing establishes whether a proposed mechanism for a delayed bolt fracture was available at all, not what happened to the failed part. On the hydrogen embrittlement side, ASTM F1624 measures a hydrogen embrittlement threshold by incremental step loading and is the usual route to establishing whether the material as supplied was susceptible, and ISO 15330 provides a preloading test for detecting embrittlement in finished fasteners. On the corrosion side, the ASTM G-series specimen tests characterize alloy susceptibility in a defined environment.

None of these confirmatory tests establishes what happened to the failed bolt. Establishing whether the proposed mechanism was available at all is what separates a supported opinion from an inference drawn from appearance.

Can hydrogen embrittle a bolt in service rather than during manufacture?

Yes, hydrogen can also be generated in service, by corrosion reactions at the metal surface or by cathodic protection, and then embrittle the same high-strength steel. This environmentally assisted variant sits between internal hydrogen embrittlement and stress corrosion cracking, and the distinguishing evidence is whether hydrogen entered the bolt before service or during it. The process record and the corrosion state of the joint address that question together.

Where are expert opinions on delayed bolt fractures challenged?

Expert opinions on delayed bolt fractures are predictably challenged on four points: that intergranular fracture was equated with hydrogen without excluding stress corrosion or temper embrittlement; that no hardness or composition data ties the part to its marked grade; that the plating and baking record was never obtained; and that one fastener was examined without comparison to unfailed siblings from the same lot.

Delayed bolt fracture work that states which mechanisms were considered, which were excluded, and on what evidence survives that scrutiny. A conclusion resting on the appearance of a single fracture surface does not.

This article is general technical orientation, not a failure analysis, an engineering opinion, or advice on any specific matter. Determining the cause of a particular incident requires hands-on examination by a credentialed expert.

For informational purposes only. Not engineering or legal advice, and not an opinion on the cause of any specific failure or on the conduct of any party.

Related

The practice area

failure-analysis assistanttriage · not a substitute for an expert
Happy to. Tell me what failed, how it failed, and whether the failed part and the scene are still preserved. That last one often decides what can still be established.