Knowledge · Damage mechanisms

How metals degrade,
and how to tell them apart.

100 categorised metal damage and failure mechanisms — each with a concise review, an original conceptual diagram, and source-qualified context.

Every mechanism keeps its original review fields and an original conceptual diagram. Photographs are being sourced separately; each will carry its source, licence, date and a credibility tier (80 = TWI/ASNT/ASME/ASTM/API/EPRI/peer-reviewed & recognised standards; 70 = Wikipedia/Wikimedia; 50 = other inspection & case sources; 20 = general web).

What the failure statistics actually say

These are investigation-cohort percentages with their own denominators — they describe the cases each organisation examined, not a worldwide incidence rate. They are not additive.

Oil, gas & maritime

DNV • published 2020 · More than 1,000 investigated component failures

Fatigue30%
Corrosion19%

Fatigue leads the reported mechanism classes in this investigation cohort.

Referral case series, not a random sample of operating assets. Exact n is not disclosed. Only the reported percentages are plotted.

Alberta pipelines

AER • 2025 failures · 229 pipeline failures (leaks or ruptures)

Internal corrosion38%
External corrosion13%
Pipe body failure9%
Construction deficiency8%
Valve or fitting failure8%

Internal corrosion is the leading reported category in this pipeline population.

Regulatory failure categories mix mechanisms, component labels and construction deficiencies. Rounded percentages; not all categories are shown.

Rolling bearings

SKF • published 2022 · Identified bearing failure modes in SKF investigations

Abrasive wear26%
Surface-initiated fatigue16%
Moisture corrosion14%
Adhesive wear7%
Current leakage7%

Abrasive wear leads the reported bearing modes; 16% is surface-initiated fatigue, not all rolling-contact fatigue.

Sample size is not disclosed. These are shares of investigated damage modes, not probabilities that an installed bearing will fail.

Helicopter components

Davies et al. • 2013 · Failures in a 30-year AgustaWestland investigation review

Fatigue (approximately)55%

Fatigue dominates this manufacturer-specific review, not necessarily other equipment populations.

Approximately 55%; exact n is unavailable in the accessible text. A selected component-investigation cohort, not a fatal-accident or fleet-wide failure rate.

100 shown
DM-001Uniform aqueous corrosionAqueous & localized corrosion · General metal loss
Umbrella damage mechanism

Mechanism pathway

Service conditions

Conductive water; oxidant or reducible species; no single acid required

Physical processes

  • Anodic metal dissolution
  • Coupled cathodic reaction over the wetted surface

Observable damage

Broad thinning; rust or scale; weight loss

Possible failure mode

Perforation or pressure rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
General corrosion; general wastage
Industries / exposed sectors
Water; chemical processing; marine; utilities
Typically affected parts
Tank walls; piping; exposed wetted surfaces
Susceptible materials
Iron and steel; other susceptible metals require environment-specific assessment
Required chemicals / environment
Conductive water; oxidant or reducible species; no single acid required
Influencing parameters
pH; temperature; oxygen; salinity; wetting time
Physical explanation (1–3 processes)
  1. Anodic metal dissolution
  2. Coupled cathodic reaction over the wetted surface
Signs and symptoms
Broad thinning; rust or scale; weight loss
Prevention / slowing the damage
Keep surfaces dry where practical; use suitable barriers and engineered cathodic protection
Typical failure outcome
Perforation or pressure rupture
Possible consequences
Release; contamination; reduced load capacity
Can be mistaken for
Erosion-corrosion; oxidation; localized corrosion
How to distinguish it
Map thickness over a grid; identify electrolyte and products; separate general loss from isolated pits
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-002Atmospheric corrosionAqueous & localized corrosion · Thin-film corrosion
Damage mechanism

Mechanism pathway

Service conditions

Atmospheric moisture and deposited marine salts

Physical processes

  • Thin electrolyte films enable electrochemical attack
  • Wet/dry cycling concentrates contaminants

Observable damage

Rust; coating undercutting; section loss

Possible failure mode

Structural fracture or collapse after sufficient section loss

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Weathering corrosion; atmospheric rusting
Industries / exposed sectors
Infrastructure; transport; marine; storage
Typically affected parts
Exposed bridge steel and comparable outdoor steelwork
Susceptible materials
Mild steel; painted or thermally sprayed aluminium-coated steel
Required chemicals / environment
Atmospheric moisture and deposited marine salts
Influencing parameters
Sheltering; orientation; coastal distance; salt deposition and weather
Physical explanation (1–3 processes)
  1. Thin electrolyte films enable electrochemical attack
  2. Wet/dry cycling concentrates contaminants
Signs and symptoms
Rust; coating undercutting; section loss
Prevention / slowing the damage
Drainage; durable coatings; wash salt deposits; select exposure-appropriate alloys
Typical failure outcome
Structural fracture or collapse after sufficient section loss
Possible consequences
Reduced structural capacity; falling components
Can be mistaken for
CUI; filiform corrosion; soil corrosion
How to distinguish it
Establish exposure and wetting pattern; inspect coating and sheltered surfaces
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-003Soil corrosionAqueous & localized corrosion · Buried-electrolyte corrosion
Damage mechanism

Mechanism pathway

Service conditions

Moist soil electrolyte; oxygen gradients; microbes may contribute

Physical processes

  • Unequal soil exposure creates coupled anodic and cathodic regions

Observable damage

External pits; coating disbondment; thinning at soil transitions

Possible failure mode

Leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Buried external corrosion
Industries / exposed sectors
Pipelines; water; foundations; power
Typically affected parts
Buried steel pipes, piles and reinforced infrastructure
Susceptible materials
Carbon steel; cast iron; metallic coatings
Required chemicals / environment
Moist soil electrolyte; oxygen gradients; microbes may contribute
Influencing parameters
Soil resistivity; moisture; pH; drainage; coating condition
Physical explanation (1–3 processes)
  1. Unequal soil exposure creates coupled anodic and cathodic regions
Signs and symptoms
External pits; coating disbondment; thinning at soil transitions
Prevention / slowing the damage
Coating plus monitored cathodic protection; drainage; compatible backfill
Typical failure outcome
Leak or rupture
Possible consequences
Soil/water contamination; supply interruption
Can be mistaken for
MIC; stray-current corrosion; graphitic corrosion
How to distinguish it
Excavation evidence; soil/CP surveys; morphology and metallography; do not diagnose from resistivity alone
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-004Galvanic corrosionAqueous & localized corrosion · Electrically coupled corrosion
Damage mechanism

Mechanism pathway

Service conditions

Shared electrolyte and electrical continuity are necessary

Physical processes

  • Electrical coupling drives anodic dissolution of the less noble member

Observable damage

Preferential attack beside dissimilar-metal contact

Possible failure mode

Local perforation; joint failure

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Bimetallic corrosion; dissimilar-metal corrosion
Industries / exposed sectors
Marine; aerospace; utilities; process plants
Typically affected parts
Mixed-metal joints; fasteners; exchanger tubesheets
Susceptible materials
A less noble metal coupled to a more noble conductive surface
Required chemicals / environment
Shared electrolyte and electrical continuity are necessary
Influencing parameters
Relative electrochemical potential; exposed anode-to-cathode area; continuity of protection
Physical explanation (1–3 processes)
  1. Electrical coupling drives anodic dissolution of the less noble member
Signs and symptoms
Preferential attack beside dissimilar-metal contact
Prevention / slowing the damage
Electrically isolate joints; compatible alloys; coat both members appropriately; avoid small-anode/large-cathode geometry
Typical failure outcome
Local perforation; joint failure
Possible consequences
Leak; loss of attachment
Can be mistaken for
Crevice corrosion; selective leaching
How to distinguish it
Confirm electrical continuity, electrolyte and polarity; compare attack on both coupled metals
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-005Pitting corrosionAqueous & localized corrosion · Localized passive-film breakdown
Damage mechanism

Mechanism pathway

Service conditions

Electrolyte plus film-destabilizing chemistry; chloride common, not mandatory

Physical processes

  • Local failure of passivity permits concentrated attack into the metal

Observable damage

Deep isolated cavities; small openings may hide large subsurface pits

Possible failure mode

Pinhole leak; rupture of a severely weakened section

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Localized penetration; pit attack
Industries / exposed sectors
Chemical; marine; food; water
Typically affected parts
Chemical tanks and other wetted alloy equipment
Susceptible materials
Passivating alloys; the verified case concerns 316Ti stainless steel
Required chemicals / environment
Electrolyte plus film-destabilizing chemistry; chloride common, not mandatory
Influencing parameters
Temperature; potential; halides; surface finish; stagnation
Physical explanation (1–3 processes)
  1. Local failure of passivity permits concentrated attack into the metal
Signs and symptoms
Deep isolated cavities; small openings may hide large subsurface pits
Prevention / slowing the damage
Control halides/deposits; select resistant alloys; passivate appropriately; inspect locally
Typical failure outcome
Pinhole leak; rupture of a severely weakened section
Possible consequences
Containment loss; hidden strength reduction; pits may initiate subsequent fatigue or SCC
Can be mistaken for
MIC; crevice corrosion; erosion craters
How to distinguish it
Measure pit depth and distribution; cross-section; analyse deposits and chemistry; morphology alone is insufficient
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-006Crevice corrosionAqueous & localized corrosion · Shielded localized attack
Damage mechanism

Mechanism pathway

Service conditions

Conductive liquid trapped in a restrictive gap; chlorides often aggravate

Physical processes

  • Oxygen depletion inside a crevice
  • Acidification and ion concentration destabilize passivity

Observable damage

Attack under gaskets or overlaps; intact adjacent open surface

Possible failure mode

Perforation; joint leakage

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Occluded-cell corrosion
Industries / exposed sectors
Marine; chemical; water; desalination
Typically affected parts
Gaskets, washers, threads, lap joints and clamps
Susceptible materials
Stainless steels; aluminium; other passivating alloys
Required chemicals / environment
Conductive liquid trapped in a restrictive gap; chlorides often aggravate
Influencing parameters
Gap geometry; temperature; stagnation; oxygen access
Physical explanation (1–3 processes)
  1. Oxygen depletion inside a crevice
  2. Acidification and ion concentration destabilize passivity
Signs and symptoms
Attack under gaskets or overlaps; intact adjacent open surface
Prevention / slowing the damage
Eliminate crevices; seal-weld where suitable; resistant alloys; clean deposits
Typical failure outcome
Perforation; joint leakage
Possible consequences
Release; loss of sealing/support
Can be mistaken for
Pitting; under-deposit corrosion
How to distinguish it
Demonstrate correspondence with the physical gap; section the joint and map the attack
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-007Under-deposit corrosionAqueous & localized corrosion · Deposit-created microenvironment
Location-defined damage family

Mechanism pathway

Service conditions

Wetted deposits; corrosive species may concentrate beneath them

Physical processes

  • Boiling beneath porous deposits can concentrate aggressive dissolved species

Observable damage

Local wall loss beneath deposits

Possible failure mode

Leak or local rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Deposit-associated localized corrosion
Industries / exposed sectors
Boilers; cooling water; oil/gas; chemical
Typically affected parts
Tube surfaces; low-flow pipe sections; tank bottoms
Susceptible materials
Carbon steel; low-alloy and stainless steels
Required chemicals / environment
Wetted deposits; corrosive species may concentrate beneath them
Influencing parameters
Deposit porosity; heat flux; flow; bulk and local chemistry
Physical explanation (1–3 processes)
  1. Boiling beneath porous deposits can concentrate aggressive dissolved species
Signs and symptoms
Local wall loss beneath deposits
Prevention / slowing the damage
Control fouling and water chemistry; maintain flow; qualified cleaning
Typical failure outcome
Leak or local rupture
Possible consequences
Tube failure; process cross-contamination
Can be mistaken for
MIC; caustic gouging; oxygen pitting
How to distinguish it
Preserve deposits; analyse layers and local conditions; distinguish the specific chemical driver
How often is it seen?
Alberta, 2025: 19% of internal-corrosion pipeline failures were assigned to this mechanism. Denominator: internal-corrosion failures, NOT all 229 pipeline failures or all industries. No representative worldwide rate identified.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-008Corrosion under insulationAqueous & localized corrosion · Hidden external attack
Location-defined damage family

Mechanism pathway

Service conditions

Water ingress; salts can intensify damage

Physical processes

  • Wet insulation retains an electrolyte against metal
  • Concentration during drying intensifies localized attack

Observable damage

Rust staining; damaged jackets; concealed thinning

Possible failure mode

Leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
CUI; external corrosion under insulation
Industries / exposed sectors
Refining; chemical; power; offshore
Typically affected parts
Insulated piping; vessels; supports; penetrations
Susceptible materials
Carbon/low-alloy steel; stainless steel can develop chloride SCC
Required chemicals / environment
Water ingress; salts can intensify damage
Influencing parameters
Wetting/drying; temperature cycles; jacket integrity; drainage
Physical explanation (1–3 processes)
  1. Wet insulation retains an electrolyte against metal
  2. Concentration during drying intensifies localized attack
Signs and symptoms
Rust staining; damaged jackets; concealed thinning
Prevention / slowing the damage
Maintain an engineered moisture barrier and inspect concealed surfaces; TSA coatings have been studied for CUI mitigation
Typical failure outcome
Leak or rupture
Possible consequences
Unexpected loss of containment; difficult inspection
Can be mistaken for
Atmospheric corrosion; external chloride SCC; soil attack
How to distinguish it
Inspect beneath insulation; thickness mapping; distinguish metal loss from cracking in stainless steel
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-009Microbiologically influenced corrosionAqueous & localized corrosion · Biologically influenced electrochemistry
Damage mechanism

Mechanism pathway

Service conditions

Microbial activity in a compatible wet environment; nutrient and redox conditions vary

Physical processes

  • Microbial activity changes local corrosion reactions and chemistry

Observable damage

Localized attack under biofilms; deposits; sometimes tubercles

Possible failure mode

Pinhole leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
MIC; biocorrosion
Industries / exposed sectors
Water, wastewater, marine and hydrocarbon/process systems
Typically affected parts
Deadlegs; tanks; pipelines; heat exchangers
Susceptible materials
Steels; stainless steels; copper and aluminium alloys
Required chemicals / environment
Microbial activity in a compatible wet environment; nutrient and redox conditions vary
Influencing parameters
Biofilm; stagnation; temperature; redox conditions; treatment history
Physical explanation (1–3 processes)
  1. Microbial activity changes local corrosion reactions and chemistry
Signs and symptoms
Localized attack under biofilms; deposits; sometimes tubercles
Prevention / slowing the damage
Control biofilms and deposits; suitable treatment; flow management; compatible materials
Typical failure outcome
Pinhole leak or rupture
Possible consequences
Contamination; release; downtime
Can be mistaken for
Abiotic pitting; under-deposit attack; sulfide corrosion
How to distinguish it
Combine microbiology, chemistry, metallography and operations evidence; finding microbes alone does not prove MIC
How often is it seen?
Alberta, 2025: 7% of internal-corrosion pipeline failures were assigned to this mechanism. Denominator: internal-corrosion failures, NOT all 229 pipeline failures or all industries. No representative worldwide rate identified.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-010DC stray-current corrosionAqueous & localized corrosion · Electrical interference
Damage mechanism

Mechanism pathway

Service conditions

Electrolyte and unintended DC current path

Physical processes

  • Metal dissolves where conventional current leaves the structure into the electrolyte

Observable damage

Concentrated external pits; time-varying structure-to-soil potentials

Possible failure mode

Perforation or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Electrolytic corrosion; stray direct-current attack
Industries / exposed sectors
Pipelines and infrastructure near DC transit or other current sources
Typically affected parts
Buried steel pipes, tanks and electrically continuous piles
Susceptible materials
Conductive metals exposed to an electrolyte
Required chemicals / environment
Electrolyte and unintended DC current path
Influencing parameters
Current magnitude/direction; coating holidays; rail-return design
Physical explanation (1–3 processes)
  1. Metal dissolves where conventional current leaves the structure into the electrolyte
Signs and symptoms
Concentrated external pits; time-varying structure-to-soil potentials
Prevention / slowing the damage
Identify current source; engineered drainage/bonding; insulation; coordinated CP
Typical failure outcome
Perforation or rupture
Possible consequences
Leak; shortened asset life
Can be mistaken for
Soil corrosion; AC corrosion; galvanic corrosion
How to distinguish it
Time-synchronized potential/current surveys linked to source operation; locate current-discharge areas
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-011AC-induced corrosionAqueous & localized corrosion · Electrical interference
Damage mechanism

Mechanism pathway

Service conditions

Soil electrolyte plus induced/conducted AC

Physical processes

  • Proposed explanations include nonlinear electrochemical rectification and cyclic changes to surface films; no single model explains all AC corrosion.

Observable damage

Severe localized loss at small coating defects

Possible failure mode

Pinhole leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Alternating-current corrosion
Industries / exposed sectors
Pipelines beside AC power lines or rail systems
Typically affected parts
Coating holidays on buried steel pipelines
Susceptible materials
Cathodically protected carbon steel
Required chemicals / environment
Soil electrolyte plus induced/conducted AC
Influencing parameters
AC/DC current density; holiday size; soil chemistry; CP level
Physical explanation (1–3 processes)
  1. Proposed explanations include nonlinear electrochemical rectification and cyclic changes to surface films; no single model explains all AC corrosion.
Signs and symptoms
Severe localized loss at small coating defects
Prevention / slowing the damage
AC-interference assessment; engineered grounding/decoupling; monitor coupons and CP
Typical failure outcome
Pinhole leak or rupture
Possible consequences
Pipeline release; electrical safety hazard may coexist
Can be mistaken for
DC corrosion; ordinary external corrosion
How to distinguish it
Measure AC and DC current/potential, coupon loss and coating defects; adequate CP potential alone does not exclude AC damage
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-012Intergranular corrosionAqueous & localized corrosion · Grain-boundary selective attack
Damage mechanism

Mechanism pathway

Service conditions

Corrosive electrolyte compatible with the depleted/segregated boundary region

Physical processes

  • Boundary segregation or precipitation creates locally susceptible regions
  • Selective boundary dissolution can detach otherwise intact grains

Observable damage

Boundary attack, grain loss and reduced mechanical integrity

Possible failure mode

Leak or brittle-appearing separation

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
IGC; intercrystalline corrosion
Industries / exposed sectors
Chemical; aerospace; heat treatment; food
Typically affected parts
Sensitized weld HAZ; heat-exchanger tubes; alloy sheet
Susceptible materials
Susceptible stainless steels and aluminium alloys
Required chemicals / environment
Corrosive electrolyte compatible with the depleted/segregated boundary region
Influencing parameters
Thermal history; sensitization; chemistry; temperature
Physical explanation (1–3 processes)
  1. Boundary segregation or precipitation creates locally susceptible regions
  2. Selective boundary dissolution can detach otherwise intact grains
Signs and symptoms
Boundary attack, grain loss and reduced mechanical integrity
Prevention / slowing the damage
Control alloy composition and thermal exposure; appropriate solution treatment; validated corrosion testing
Typical failure outcome
Leak or brittle-appearing separation
Possible consequences
Unexpected loss of ductility and containment
Can be mistaken for
SCC; liquation cracking; exfoliation
How to distinguish it
Metallographic boundary attack plus sensitization/chemistry evidence; assess whether tensile stress was essential
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-013Exfoliation corrosionAqueous & localized corrosion · Advanced intergranular corrosion
Damage mechanism

Mechanism pathway

Service conditions

Corrosive moisture, often chloride-bearing

Physical processes

  • Intergranular attack follows elongated grain paths
  • Expanding corrosion products lift surface layers

Observable damage

Leaf-like lifting; bulging; delamination

Possible failure mode

Component separation or fracture after section degradation

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
EXCO; layer lifting
Industries / exposed sectors
Aerospace; transport; marine
Typically affected parts
Heavily worked aluminium sections, especially exposed end grains at edges or holes
Susceptible materials
Susceptible high-strength aluminium with flattened, elongated grains
Required chemicals / environment
Corrosive moisture, often chloride-bearing
Influencing parameters
Grain orientation; temper; residual stress; salt wetting
Physical explanation (1–3 processes)
  1. Intergranular attack follows elongated grain paths
  2. Expanding corrosion products lift surface layers
Signs and symptoms
Leaf-like lifting; bulging; delamination
Prevention / slowing the damage
Resistant temper/alloy; coatings and sealants; drainage; inspect lap joints
Typical failure outcome
Component separation or fracture after section degradation
Possible consequences
Reduced structural capacity
Can be mistaken for
Lamination defects; blistering; general IGC
How to distinguish it
Cross-section shows corrosion along elongated grain boundaries and wedging products, not a clean manufacturing interface
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-014DezincificationAqueous & localized corrosion · Dealloying
Damage mechanism

Mechanism pathway

Service conditions

Aqueous electrolyte; chemistry determines susceptibility

Physical processes

  • Net zinc loss produces a copper-rich porous layer; dissolution and copper redeposition can contribute.

Observable damage

Porous copper-rich layers or localized plugs; strength loss

Possible failure mode

Leak; brittle-appearing fitting break

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Selective zinc leaching from brass
Industries / exposed sectors
Water; plumbing; marine; process
Typically affected parts
Brass valves; fittings; tubes; fasteners
Susceptible materials
Susceptible copper-zinc alloys
Required chemicals / environment
Aqueous electrolyte; chemistry determines susceptibility
Influencing parameters
Temperature; stagnation; chloride; pH; alloy phase balance
Physical explanation (1–3 processes)
  1. Net zinc loss produces a copper-rich porous layer; dissolution and copper redeposition can contribute.
Signs and symptoms
Porous copper-rich layers or localized plugs; strength loss
Prevention / slowing the damage
Dezincification-resistant brass; water chemistry control; suitable alternative alloy
Typical failure outcome
Leak; brittle-appearing fitting break
Possible consequences
Flooding; loss of isolation
Can be mistaken for
General brass corrosion; ammonia SCC
How to distinguish it
Cross-section and elemental analysis show zinc depletion/porosity rather than a stress-driven crack
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-015Graphitic corrosion of cast ironAqueous & localized corrosion · Dealloying
Damage mechanism

Mechanism pathway

Service conditions

Corrosive water or moist soil

Physical processes

  • Iron dissolves around the pre-existing graphite network
  • Graphite and corrosion products preserve shape while strength falls

Observable damage

Soft dark surface; original shape despite severe weakening

Possible failure mode

Crushing; brittle break; leakage

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Graphitic selective leaching; graphitic corrosion
Industries / exposed sectors
Water; wastewater; buried services
Typically affected parts
Cast-iron mains; valves; pump bodies
Susceptible materials
Graphite-containing cast iron, especially grey iron
Required chemicals / environment
Corrosive water or moist soil
Influencing parameters
Time; soil/water chemistry; graphite morphology
Physical explanation (1–3 processes)
  1. Iron dissolves around the pre-existing graphite network
  2. Graphite and corrosion products preserve shape while strength falls
Signs and symptoms
Soft dark surface; original shape despite severe weakening
Prevention / slowing the damage
Protective linings/coatings; appropriate CP; condition assessment and replacement
Typical failure outcome
Crushing; brittle break; leakage
Possible consequences
Sudden main break; flooding
Can be mistaken for
Thermal graphitization: a different metallurgical process
How to distinguish it
Metallography reveals removed iron around pre-existing graphite; thermal graphitization instead precipitates new graphite in steel
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-016DenickelificationAqueous & localized corrosion · Dealloying
Damage mechanism

Mechanism pathway

Service conditions

Corrosive process condensate; particular deposited/hot-spot environments

Physical processes

  • Preferential nickel loss creates a copper-rich weakened layer

Observable damage

Porosity; local wall loss; copper-rich residue

Possible failure mode

Tube leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Selective nickel leaching
Industries / exposed sectors
Refining; heat exchange; marine systems
Typically affected parts
Copper-nickel condenser tubes at deposit-associated hot spots
Susceptible materials
Susceptible copper-nickel alloys, including 70/30 Cu-Ni
Required chemicals / environment
Corrosive process condensate; particular deposited/hot-spot environments
Influencing parameters
Temperature differences; deposits; local chemistry; thermal coupling
Physical explanation (1–3 processes)
  1. Preferential nickel loss creates a copper-rich weakened layer
Signs and symptoms
Porosity; local wall loss; copper-rich residue
Prevention / slowing the damage
Address deposits, hot spots and stagnant regions within an approved operating programme
Typical failure outcome
Tube leak or rupture
Possible consequences
Cross-contamination; process outage
Can be mistaken for
Dezincification; general Cu-Ni corrosion
How to distinguish it
Elemental mapping confirms nickel depletion, not zinc loss; correlate with temperature/deposit pattern
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-017Filiform corrosionAqueous & localized corrosion · Coating-underfilm attack
Damage mechanism

Mechanism pathway

Service conditions

Moisture penetrates a breached or permeable surface coating

Physical processes

  • An active filament head advances under the coating
  • Differential aeration separates head and trailing products

Observable damage

Thread-like tracks below paint; cosmetic blistering

Possible failure mode

Coating disbondment or cosmetic rejection; structural failure is not inevitable

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Underfilm filamentary corrosion
Industries / exposed sectors
Automotive; aerospace; coated products
Typically affected parts
Painted aluminium, steel or magnesium sheet
Susceptible materials
Coated reactive metals
Required chemicals / environment
Moisture penetrates a breached or permeable surface coating
Influencing parameters
Coating defects, moisture permeability and adhesion
Physical explanation (1–3 processes)
  1. An active filament head advances under the coating
  2. Differential aeration separates head and trailing products
Signs and symptoms
Thread-like tracks below paint; cosmetic blistering
Prevention / slowing the damage
Use a well-adhered coating with appropriate resistance to water-vapour transmission
Typical failure outcome
Coating disbondment or cosmetic rejection; structural failure is not inevitable
Possible consequences
Appearance degradation; reduced coating protection
Can be mistaken for
General underfilm corrosion; scratch marks; fungal growth
How to distinguish it
Lift coating locally and examine corrosion filaments and metal attack; do not identify from paint pattern alone
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-018Carbon dioxide corrosionProcess-specific aqueous corrosion · Acid-gas aqueous corrosion
Damage mechanism

Mechanism pathway

Service conditions

Free water and dissolved CO2; impurities can change behaviour

Physical processes

  • Dissolved CO2 establishes an acidic aqueous environment
  • Iron dissolution competes with protective carbonate-scale formation

Observable damage

General thinning; local pits or mesa-like attack

Possible failure mode

Leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
CO2 corrosion; sweet corrosion
Industries / exposed sectors
Oil and gas production and wet CO2-containing process streams
Typically affected parts
Wet pipelines; production tubing; vessels
Susceptible materials
Carbon and low-alloy steels
Required chemicals / environment
Free water and dissolved CO2; impurities can change behaviour
Influencing parameters
CO2 and other gas composition; water chemistry; operating conditions; material
Physical explanation (1–3 processes)
  1. Dissolved CO2 establishes an acidic aqueous environment
  2. Iron dissolution competes with protective carbonate-scale formation
Signs and symptoms
General thinning; local pits or mesa-like attack
Prevention / slowing the damage
Manage water and impurities; validated inhibitors; resistant materials; monitor scale/flow
Typical failure outcome
Leak or rupture
Possible consequences
Hydrocarbon/CO2 release; shutdown
Can be mistaken for
Wet H2S corrosion; oxygen corrosion; erosion-corrosion
How to distinguish it
Analyse gas/liquid and carbonate scale; morphology alone does not identify CO2
How often is it seen?
Alberta, 2025: 6% of internal-corrosion pipeline failures were assigned to this mechanism. Denominator: internal-corrosion failures, NOT all 229 pipeline failures or all industries. No representative worldwide rate identified.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-019Wet hydrogen sulfide corrosionProcess-specific aqueous corrosion · Acid-gas aqueous corrosion
Damage mechanism

Mechanism pathway

Service conditions

Water and H2S

Physical processes

  • Iron dissolution forms iron-sulfide products
  • Film damage or unstable scales permit continued attack

Observable damage

Black sulfide deposits; thinning or pitting

Possible failure mode

Leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Sour corrosion; aqueous H2S metal loss
Industries / exposed sectors
Sour oil/gas and associated process equipment
Typically affected parts
Pipelines; separators; sour-water piping
Susceptible materials
Carbon/low-alloy steel; other alloys depending on environment
Required chemicals / environment
Water and H2S
Influencing parameters
pH; H2S activity; temperature; flow; sulfide-film stability
Physical explanation (1–3 processes)
  1. Iron dissolution forms iron-sulfide products
  2. Film damage or unstable scales permit continued attack
Signs and symptoms
Black sulfide deposits; thinning or pitting
Prevention / slowing the damage
Sour-service materials; chemistry and flow control; suitable inhibition; monitoring
Typical failure outcome
Leak or rupture
Possible consequences
Toxic H2S release; outage
Can be mistaken for
Sulfidation; SSC; HIC; CO2 corrosion
How to distinguish it
Prove wet service and metal loss; test separately for hydrogen-assisted cracking; black scale alone is not diagnostic
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-020Hydrochloric acid corrosionProcess-specific aqueous corrosion · Mineral-acid corrosion
Damage mechanism

Mechanism pathway

Service conditions

Aqueous hydrochloric acid

Physical processes

  • Acid-driven electrochemical dissolution consumes susceptible metal

Observable damage

Rapid thinning; rough etched surfaces; localized attack

Possible failure mode

Leak; local rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
HCl attack; hydrochloric-acid dewpoint corrosion
Industries / exposed sectors
Chemical processing
Typically affected parts
Overhead condensers; piping; acid tanks
Susceptible materials
Carbon steel; many stainless grades; alloy resistance depends on concentration
Required chemicals / environment
Aqueous hydrochloric acid
Influencing parameters
Acid concentration; temperature; oxidizing impurities
Physical explanation (1–3 processes)
  1. Acid-driven electrochemical dissolution consumes susceptible metal
Signs and symptoms
Rapid thinning; rough etched surfaces; localized attack
Prevention / slowing the damage
Control chloride sources and condensate chemistry; engineered wash/neutralization; qualified alloy selection
Typical failure outcome
Leak; local rupture
Possible consequences
Acid exposure; process contamination
Can be mistaken for
NH4Cl corrosion; other acid attack
How to distinguish it
Sample initial condensate and deposits; determine chloride, acidity and temperature history
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-021Sulfuric acid corrosionProcess-specific aqueous corrosion · Mineral-acid corrosion
Damage mechanism

Mechanism pathway

Service conditions

Sulfuric acid with water; oxidants/impurities modify attack

Physical processes

  • Acidic electrochemical attack depends on alloy and the stability of protective surface films

Observable damage

Thinning; etched surfaces; local erosion-corrosion

Possible failure mode

Leak; rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
H2SO4 attack
Industries / exposed sectors
Fertilizer; chemical; mineral processing; batteries
Typically affected parts
Acid tanks; pumps; piping; exchangers
Susceptible materials
Steel and corrosion-resistant alloys, depending strongly on acid concentration
Required chemicals / environment
Sulfuric acid with water; oxidants/impurities modify attack
Influencing parameters
Acid concentration, temperature, impurities and flow
Physical explanation (1–3 processes)
  1. Acidic electrochemical attack depends on alloy and the stability of protective surface films
Signs and symptoms
Thinning; etched surfaces; local erosion-corrosion
Prevention / slowing the damage
Select alloy/lining for the actual concentration-temperature envelope; prevent unintended dilution
Typical failure outcome
Leak; rupture
Possible consequences
Acid burns; environmental release
Can be mistaken for
Acid-dewpoint corrosion; HCl attack
How to distinguish it
Analyse acid concentration and impurities; reconstruct dilution/temperature excursions
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-022Hydrofluoric acid corrosionProcess-specific aqueous corrosion · Mineral-acid corrosion
Damage mechanism

Mechanism pathway

Service conditions

HF-containing service; water and contaminants change severity

Physical processes

  • Metal dissolution and fluoride-film formation compete
  • Local film instability accelerates metal loss

Observable damage

Thinning; scale; isolated highly corroded components

Possible failure mode

Leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
HF corrosion
Industries / exposed sectors
Refinery alkylation; fluorochemical processing
Typically affected parts
HF-alkylation piping, including elbows
Susceptible materials
Carbon-steel components; residual copper/nickel chemistry matters
Required chemicals / environment
HF-containing service; water and contaminants change severity
Influencing parameters
Component composition and actual HF-service conditions
Physical explanation (1–3 processes)
  1. Metal dissolution and fluoride-film formation compete
  2. Local film instability accelerates metal loss
Signs and symptoms
Thinning; scale; isolated highly corroded components
Prevention / slowing the damage
Strict chemistry/material control; component-level inspection; engineered containment and isolation
Typical failure outcome
Leak or rupture
Possible consequences
Highly toxic release; fire if hydrocarbons are present
Can be mistaken for
HCl corrosion; localized erosion; weld-related attack
How to distinguish it
Verify HF duty, water history and component chemistry; thickness-map individual fittings
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
Philadelphia Energy Solutions, 21 June 2019: a severely corroded HF-service elbow ruptured, causing explosions/fire and an HF release. CSB linked accelerated corrosion to component chemistry.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-023Phosphoric acid corrosionProcess-specific aqueous corrosion · Mineral-acid corrosion
Damage mechanism

Mechanism pathway

Service conditions

Aqueous phosphoric acid with process-dependent sulfate, metal-ion, fluoride and chloride impurities

Physical processes

  • Acid dissolution attacks insufficiently resistant alloys
  • Impurities can destabilize passive films

Observable damage

General loss; pits or preferential weld attack

Possible failure mode

Leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
H3PO4 attack
Industries / exposed sectors
Fertilizer; phosphates; chemical processing
Typically affected parts
Fertilizer-grade phosphoric-acid evaporator tubing and related process equipment
Susceptible materials
Steels; stainless and nickel alloys depending on purity
Required chemicals / environment
Aqueous phosphoric acid with process-dependent sulfate, metal-ion, fluoride and chloride impurities
Influencing parameters
Acid concentration, temperature, impurity content and deposits
Physical explanation (1–3 processes)
  1. Acid dissolution attacks insufficiently resistant alloys
  2. Impurities can destabilize passive films
Signs and symptoms
General loss; pits or preferential weld attack
Prevention / slowing the damage
Select against actual wet-process acid, not reagent-acid data alone; control impurities and flow
Typical failure outcome
Leak or rupture
Possible consequences
Acid/slurry release; production loss
Can be mistaken for
Slurry erosion; HCl/HF corrosion
How to distinguish it
Analyse acid impurities and solids; compare shielded and impinged areas; inspect weld/base metal
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-024Caustic corrosionProcess-specific aqueous corrosion · Concentrated-alkali corrosion
Damage mechanism

Mechanism pathway

Service conditions

Locally concentrated sodium hydroxide in boiler water

Physical processes

  • Concentrated caustic dissolves protective magnetite, exposing steel to continued metal loss

Observable damage

Irregular gouges or thinning

Possible failure mode

Tube leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Caustic gouging; alkaline metal loss
Industries / exposed sectors
Boilers; refining; chemical; pulp
Typically affected parts
Boiler tubes under deposits; caustic piping; evaporators
Susceptible materials
Carbon/low-alloy steels; susceptible stainless alloys
Required chemicals / environment
Locally concentrated sodium hydroxide in boiler water
Influencing parameters
Local concentration; temperature; deposits; heat flux; dryout
Physical explanation (1–3 processes)
  1. Concentrated caustic dissolves protective magnetite, exposing steel to continued metal loss
Signs and symptoms
Irregular gouges or thinning
Prevention / slowing the damage
Prevent caustic concentration/dryout; control deposits and chemistry; suitable materials
Typical failure outcome
Tube leak or rupture
Possible consequences
Hot fluid release; outage
Can be mistaken for
Caustic SCC; acid phosphate corrosion; FAC
How to distinguish it
Metallography distinguishes wall loss from stress-driven cracks; analyse deposit chemistry and heat-flux pattern
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-025Amine-unit corrosionProcess-specific aqueous corrosion · Solvent-system corrosion
Damage mechanism

Mechanism pathway

Service conditions

Aqueous amine with acid gases/degradation products; heat-stable salts can aggravate

Physical processes

  • Heat-stable salts can increase solution corrosiveness; the effect depends on salt identity and concentration

Observable damage

Metal loss; morphology must be confirmed for the actual solvent

Possible failure mode

Leak or equipment rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Amine corrosion; acid-gas treating corrosion
Industries / exposed sectors
Gas sweetening; refining; carbon capture
Typically affected parts
Regenerators; reboilers; rich-amine lines; exchangers
Susceptible materials
Carbon steel and304 stainless steel in the verified MEA study; alloy response is chemistry-dependent
Required chemicals / environment
Aqueous amine with acid gases/degradation products; heat-stable salts can aggravate
Influencing parameters
Temperature and acid-gas composition; solvent and heat-stable-salt composition
Physical explanation (1–3 processes)
  1. Heat-stable salts can increase solution corrosiveness; the effect depends on salt identity and concentration
Signs and symptoms
Metal loss; morphology must be confirmed for the actual solvent
Prevention / slowing the damage
Control solvent quality and heat-stable salts; oxygen exclusion where appropriate; flow and material review
Typical failure outcome
Leak or equipment rupture
Possible consequences
Toxic/flammable release; solvent contamination
Can be mistaken for
Amine SCC; wet H2S corrosion; CO2 corrosion
How to distinguish it
Analyse solvent, gas loading and salts; distinguish cracks from metal loss
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-026Ammonium bisulfide corrosionProcess-specific aqueous corrosion · Sour-water salt corrosion
Damage mechanism

Mechanism pathway

Service conditions

Water containing ammonia and hydrogen sulfide/bisulfide species

Physical processes

  • Electrochemical iron loss accompanies formation of sulfide-containing corrosion products

Observable damage

Rapid thinning; localized grooves; sulfide products

Possible failure mode

Leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
NH4HS corrosion; ammonium hydrosulfide corrosion
Industries / exposed sectors
Hydroprocessing; refining; sour-water stripping
Typically affected parts
Sour-water ammonia-rectifier heat-exchanger nozzle in the verified case
Susceptible materials
Carbon steel in the verified nozzle investigation
Required chemicals / environment
Water containing ammonia and hydrogen sulfide/bisulfide species
Influencing parameters
Salt concentration; temperature; turbulence; velocity; wash-water distribution
Physical explanation (1–3 processes)
  1. Electrochemical iron loss accompanies formation of sulfide-containing corrosion products
Signs and symptoms
Rapid thinning; localized grooves; sulfide products
Prevention / slowing the damage
Engineered water-wash distribution; concentration/flow control; appropriate materials and thickness mapping
Typical failure outcome
Leak or rupture
Possible consequences
Toxic/flammable release; exchanger outage
Can be mistaken for
Wet H2S corrosion; erosion-corrosion; NH4Cl attack
How to distinguish it
Analyse NH4HS-related chemistry, products and flow locations; check for concurrent HIC
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
Published 2026 refinery case: metallurgical/electrochemical investigation attributed sour-water exchanger damage to NH4HS-related corrosion. A fatal/offsite catastrophe was not established in that paper.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-027Ammonium chloride corrosionProcess-specific aqueous corrosion · Hygroscopic-salt corrosion
Damage mechanism

Mechanism pathway

Service conditions

Solid ammonium chloride deposits that absorb environmental moisture

Physical processes

  • Hygroscopic salt wetting establishes a concentrated corrosive environment

Observable damage

Localized thinning beneath salt; pits; plugging

Possible failure mode

Leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
NH4Cl salt corrosion
Industries / exposed sectors
Refining; hydroprocessing
Typically affected parts
Hydroprocessing reactor-effluent equipment exposed to NH4Cl deposits
Susceptible materials
Carbon steel and susceptible stainless/alloy materials; response differs by material
Required chemicals / environment
Solid ammonium chloride deposits that absorb environmental moisture
Influencing parameters
Relative humidity, temperature and alloy
Physical explanation (1–3 processes)
  1. Hygroscopic salt wetting establishes a concentrated corrosive environment
Signs and symptoms
Localized thinning beneath salt; pits; plugging
Prevention / slowing the damage
Limit salt precursors; engineered water washing; avoid dry salt accumulation; inspect deposition zones
Typical failure outcome
Leak or rupture
Possible consequences
Toxic/flammable release; blockage
Can be mistaken for
HCl dewpoint corrosion; NH4HS corrosion
How to distinguish it
Identify chloride-rich salt and wetting conditions; distinguish first-condensate attack from hygroscopic salt wetting
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-028Flue-gas acid-dewpoint corrosionProcess-specific aqueous corrosion · Condensate corrosion
Damage mechanism

Mechanism pathway

Service conditions

Sulfur oxides and water in sulfur-bearing-fuel combustion gas

Physical processes

  • Acid condenses on sufficiently cold surfaces
  • Liquid acid consumes exposed metal

Observable damage

Cold-end thinning; rust/acid deposits; perforation

Possible failure mode

Perforation; duct leakage or collapse

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Cold-end corrosion; sulfuric-acid dewpoint corrosion
Industries / exposed sectors
Power; boilers; furnaces; incineration
Typically affected parts
Air heaters; economizers; ducts; stacks
Susceptible materials
Carbon/low-alloy steels; unsuitable linings/alloys
Required chemicals / environment
Sulfur oxides and water in sulfur-bearing-fuel combustion gas
Influencing parameters
Metal temperature relative to actual acid dewpoint; fuel chemistry; deposits
Physical explanation (1–3 processes)
  1. Acid condenses on sufficiently cold surfaces
  2. Liquid acid consumes exposed metal
Signs and symptoms
Cold-end thinning; rust/acid deposits; perforation
Prevention / slowing the damage
Control cold spots and combustion chemistry; suitable coatings/materials; drainage
Typical failure outcome
Perforation; duct leakage or collapse
Possible consequences
Flue-gas escape; efficiency loss; outage
Can be mistaken for
Atmospheric corrosion; high-temperature hot corrosion
How to distinguish it
Compare surface temperature with measured/composition-based acid dew point and examine acidic condensate
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-029Oxygen pitting in boiler/feedwater systemsProcess-specific aqueous corrosion · Oxidant-driven localized corrosion
Damage mechanism

Mechanism pathway

Service conditions

Dissolved oxygen in water

Physical processes

  • Cathodic oxygen reduction supports anodic iron dissolution

Observable damage

Localized pits, sometimes beneath oxide caps

Possible failure mode

Tube or pipe leak

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Dissolved-oxygen attack; oxygen corrosion
Industries / exposed sectors
Power; industrial steam; district heating
Typically affected parts
Feedwater lines, economizers and boiler tubes
Susceptible materials
Carbon/low-alloy steels
Required chemicals / environment
Dissolved oxygen in water
Influencing parameters
Oxygen ingress; stagnation; temperature; pH; deposits
Physical explanation (1–3 processes)
  1. Cathodic oxygen reduction supports anodic iron dissolution
Signs and symptoms
Localized pits, sometimes beneath oxide caps
Prevention / slowing the damage
Control unintended oxygen ingress and use a plant-specific operating and layup programme
Typical failure outcome
Tube or pipe leak
Possible consequences
Steam/water release; shutdown
Can be mistaken for
MIC; chloride pitting; under-deposit corrosion
How to distinguish it
Correlate oxygen/layup records, pit/deposit chemistry and biological evidence; tubercles alone do not establish MIC
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-030Acid phosphate corrosionProcess-specific aqueous corrosion · Deposit-related boiler corrosion
Damage mechanism

Mechanism pathway

Service conditions

Locally concentrated acidic phosphate beneath deposits

Physical processes

  • Deposits and local phosphate chemistry dissolve the protective magnetite layer

Observable damage

Gouging under adherent deposits; maricite may identify the reaction products

Possible failure mode

Tube leakage or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
APC; acid-phosphate boiler-tube attack
Industries / exposed sectors
Power; industrial boilers
Typically affected parts
Deposited boiler waterwalls and HRSG evaporator tubes
Susceptible materials
Carbon and low-alloy boiler steels
Required chemicals / environment
Locally concentrated acidic phosphate beneath deposits
Influencing parameters
Phosphate treatment history; local Na:P balance; hideout; heat flux
Physical explanation (1–3 processes)
  1. Deposits and local phosphate chemistry dissolve the protective magnetite layer
Signs and symptoms
Gouging under adherent deposits; maricite may identify the reaction products
Prevention / slowing the damage
Qualified boiler chemistry programme; avoid inappropriate phosphate dosing; manage deposits
Typical failure outcome
Tube leakage or rupture
Possible consequences
Forced outage; hot-fluid release
Can be mistaken for
Caustic gouging; oxygen pitting; boiler hydrogen damage
How to distinguish it
Preserve deposits for phase analysis and compare treatment/hideout history; phosphate hideout alone is insufficient
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-031Chloride stress corrosion crackingEnvironment-assisted cracking & hydrogen · Anodic environment-assisted cracking
Damage mechanism

Mechanism pathway

Service conditions

Chloride-bearing moisture plus tensile stress and a susceptible microstructure

Physical processes

  • Film rupture and localized dissolution assist crack initiation/growth
  • Crack-tip chemistry and deformation sustain environmentally assisted propagation

Observable damage

Often branched transgranular cracks; small leaks; little general corrosion

Possible failure mode

Leak or brittle-appearing rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Chloride SCC; Cl-SCC
Industries / exposed sectors
Chemical; refining; marine; power
Typically affected parts
Hot stainless piping; exchangers; insulated surfaces
Susceptible materials
Susceptible austenitic stainless steels; susceptibility varies by alloy
Required chemicals / environment
Chloride-bearing moisture plus tensile stress and a susceptible microstructure
Influencing parameters
Temperature; chloride concentration; potential; evaporation; residual stress
Physical explanation (1–3 processes)
  1. Film rupture and localized dissolution assist crack initiation/growth
  2. Crack-tip chemistry and deformation sustain environmentally assisted propagation
Signs and symptoms
Often branched transgranular cracks; small leaks; little general corrosion
Prevention / slowing the damage
Prevent chloride concentration; resistant materials; stress reduction where qualified; inspect cracking-prone locations
Typical failure outcome
Leak or brittle-appearing rupture
Possible consequences
Unexpected containment loss
Can be mistaken for
Thermal fatigue; other SCC; intergranular corrosion
How to distinguish it
Combine crack-path metallography, chloride evidence and tensile-stress history; branching alone is not proof
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-032Caustic stress corrosion crackingEnvironment-assisted cracking & hydrogen · Alkaline environment-assisted cracking
Damage mechanism

Mechanism pathway

Service conditions

Concentrated hydroxide plus tensile stress

Physical processes

  • Stress-assisted passive-film breakdown promotes localized cracking
  • Preferential grain-boundary attack can support propagation

Observable damage

Frequently intergranular, branched cracks near stressed regions

Possible failure mode

Leak or sudden rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Caustic SCC; caustic embrittlement
Industries / exposed sectors
Refining; boilers; chemical; pulp
Typically affected parts
Welds; concentrated-caustic piping; vessels
Susceptible materials
Carbon/low-alloy steel; susceptible stainless and nickel alloys
Required chemicals / environment
Concentrated hydroxide plus tensile stress
Influencing parameters
Temperature; caustic concentration; stress; deposits; alloy condition
Physical explanation (1–3 processes)
  1. Stress-assisted passive-film breakdown promotes localized cracking
  2. Preferential grain-boundary attack can support propagation
Signs and symptoms
Frequently intergranular, branched cracks near stressed regions
Prevention / slowing the damage
Control concentration and temperature; suitable alloy; qualified stress relief; avoid deposits/dryout
Typical failure outcome
Leak or sudden rupture
Possible consequences
Hot caustic exposure; outage
Can be mistaken for
Caustic gouging; weld H cracking; carbonate SCC
How to distinguish it
Cracks rather than gouges; confirm caustic chemistry and stress/thermal history; section weld and HAZ
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-033Ammonia stress corrosion cracking of copper alloysEnvironment-assisted cracking & hydrogen · Ammoniacal environment-assisted cracking
Damage mechanism

Mechanism pathway

Service conditions

Ammoniacal moisture; oxygen/oxidizing conditions commonly participate

Physical processes

  • Ammonia-containing chemistry destabilizes stressed surface regions
  • Localized dissolution and film rupture support crack growth

Observable damage

Intergranular or transgranular cracks; tarnish may occur

Possible failure mode

Fitting fracture or tube leak

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Season cracking; ammonia SCC of brass
Industries / exposed sectors
Refrigeration surroundings; marine; chemical; storage
Typically affected parts
Brass fittings; tubes; stressed fasteners
Susceptible materials
Susceptible brasses and other copper alloys; not all Cu-Ni equally susceptible
Required chemicals / environment
Ammoniacal moisture; oxygen/oxidizing conditions commonly participate
Influencing parameters
Residual stress; alloy composition; ammonia activity; pH; temperature
Physical explanation (1–3 processes)
  1. Ammonia-containing chemistry destabilizes stressed surface regions
  2. Localized dissolution and film rupture support crack growth
Signs and symptoms
Intergranular or transgranular cracks; tarnish may occur
Prevention / slowing the damage
Exclude ammoniacal contamination; reduce residual stress; qualified resistant materials
Typical failure outcome
Fitting fracture or tube leak
Possible consequences
Loss of containment; component separation
Can be mistaken for
Dezincification; fatigue; general ammoniacal corrosion
How to distinguish it
Use metallography and zinc mapping; prove ammonia exposure and stress; accelerated tests rank susceptibility, not life
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-034Carbonate stress corrosion crackingEnvironment-assisted cracking & hydrogen · Alkaline environment-assisted cracking
Environment-specific SCC subtype

Mechanism pathway

Service conditions

Aqueous carbonate/bicarbonate chemistry plus tensile stress

Physical processes

  • Active/passive electrochemistry enables stress-assisted localized dissolution

Observable damage

Often intergranular branched cracks near stressed weld regions

Possible failure mode

Leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Carbonate SCC; carbonate/bicarbonate cracking
Industries / exposed sectors
Refining; CO2-removal/chemical plants
Typically affected parts
Carbonate-solvent equipment; wet process piping; welds
Susceptible materials
Carbon steel
Required chemicals / environment
Aqueous carbonate/bicarbonate chemistry plus tensile stress
Influencing parameters
pH; potential; temperature; carbonate concentration; weld stress
Physical explanation (1–3 processes)
  1. Active/passive electrochemistry enables stress-assisted localized dissolution
Signs and symptoms
Often intergranular branched cracks near stressed weld regions
Prevention / slowing the damage
Control the actual solvent/process chemistry; qualified stress relief and inspection
Typical failure outcome
Leak or rupture
Possible consequences
Process release; outage
Can be mistaken for
Caustic SCC; amine SCC; high-pH pipeline SCC
How to distinguish it
Establish service chemistry and potential; compare crack path with weld condition; do not infer carbonate solely from deposits
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-035Polythionic acid stress corrosion crackingEnvironment-assisted cracking & hydrogen · Shutdown-related intergranular SCC
Damage mechanism

Mechanism pathway

Service conditions

Sulfide scales exposed to moisture and oxygen; tensile stress

Physical processes

  • Sulfide scales react during wet air exposure
  • Acidic sulfur species attack chromium-depleted boundaries under tensile stress

Observable damage

Intergranular cracking, commonly discovered during/after shutdown

Possible failure mode

Leak or rupture on restart

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
PASCC; polythionic SCC
Industries / exposed sectors
Refining; petrochemical; sulfur-bearing high-temperature service
Typically affected parts
Sensitized stainless furnace tubes; piping; weld HAZ
Susceptible materials
Sensitized austenitic stainless and susceptible nickel alloys
Required chemicals / environment
Sulfide scales exposed to moisture and oxygen; tensile stress
Influencing parameters
Shutdown wetting; sensitization; air entry; sulfur scale
Physical explanation (1–3 processes)
  1. Sulfide scales react during wet air exposure
  2. Acidic sulfur species attack chromium-depleted boundaries under tensile stress
Signs and symptoms
Intergranular cracking, commonly discovered during/after shutdown
Prevention / slowing the damage
Qualified shutdown protection; exclude moist oxygen; avoid sensitization; approved neutralization procedures
Typical failure outcome
Leak or rupture on restart
Possible consequences
Hydrocarbon release; fire; outage
Can be mistaken for
IGC; chloride SCC; high-temperature cracking
How to distinguish it
Demonstrate sensitization, sulfur scale and wet shutdown exposure; section grain-boundary cracks
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-036Near-neutral-pH pipeline stress corrosion crackingEnvironment-assisted cracking & hydrogen · External pipeline SCC
Damage mechanism

Mechanism pathway

Service conditions

Groundwater with dissolved CO2 beneath shielding coatings; tensile stress

Physical processes

  • Environmental dissolution and hydrogen effects assist cracking
  • Cyclic loading can accelerate transgranular crack growth

Observable damage

Axial crack colonies; often transgranular cracks with some corrosion

Possible failure mode

Leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Low-pH pipeline SCC; near-neutral SCC
Industries / exposed sectors
Gas and liquid transmission
Typically affected parts
Pipe exterior beneath disbonded coatings
Susceptible materials
Carbon-steel linepipe
Required chemicals / environment
Groundwater with dissolved CO2 beneath shielding coatings; tensile stress
Influencing parameters
Pressure cycles; local pH; coating disbondment; hydrogen entry
Physical explanation (1–3 processes)
  1. Environmental dissolution and hydrogen effects assist cracking
  2. Cyclic loading can accelerate transgranular crack growth
Signs and symptoms
Axial crack colonies; often transgranular cracks with some corrosion
Prevention / slowing the damage
Coating rehabilitation; pressure-cycle review; suitable SCC inspection and mitigation
Typical failure outcome
Leak or rupture
Possible consequences
Product release; possible fire/explosion
Can be mistaken for
High-pH SCC; corrosion fatigue; HIC
How to distinguish it
Combine external coating/soil evidence with crack path and chemistry; operating stress is essential context
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-037High-pH pipeline stress corrosion crackingEnvironment-assisted cracking & hydrogen · External alkaline pipeline SCC
Damage mechanism

Mechanism pathway

Service conditions

Concentrated carbonate/bicarbonate electrolyte plus tensile stress

Physical processes

  • Active/passive film rupture and dissolution support predominantly intergranular cracking

Observable damage

Axial crack colonies; intergranular paths in characteristic chemistry

Possible failure mode

Leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Classical pipeline SCC
Industries / exposed sectors
Gas and liquid transmission
Typically affected parts
Pipe surfaces beneath disbonded coatings
Susceptible materials
Carbon-steel linepipe
Required chemicals / environment
Concentrated carbonate/bicarbonate electrolyte plus tensile stress
Influencing parameters
Temperature; potential; concentration; stress cycles; coating shielding
Physical explanation (1–3 processes)
  1. Active/passive film rupture and dissolution support predominantly intergranular cracking
Signs and symptoms
Axial crack colonies; intergranular paths in characteristic chemistry
Prevention / slowing the damage
Coating/CP coordination; temperature and cycling review; validated crack detection
Typical failure outcome
Leak or rupture
Possible consequences
Loss of containment; potential fire
Can be mistaken for
Near-neutral SCC; carbonate SCC in process equipment; fatigue
How to distinguish it
Intergranular path plus external alkaline environment; do not use crack orientation alone
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-038Primary-water stress corrosion crackingEnvironment-assisted cracking & hydrogen · Nuclear primary-water SCC
Damage mechanism

Mechanism pathway

Service conditions

High-temperature primary water plus tensile stress

Physical processes

  • Grain-boundary oxidation and crack-tip deformation interact under tensile loading

Observable damage

Often intergranular cracking; leakage products; limited external warning

Possible failure mode

Leak; possible pressure-boundary rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
PWSCC
Industries / exposed sectors
Pressurized-water nuclear plants
Typically affected parts
Penetrations; nozzle welds; pressurizer heaters; steam-generator tubes
Susceptible materials
Susceptible nickel alloys, notably Alloy 600 and weld metals 82/182
Required chemicals / environment
High-temperature primary water plus tensile stress
Influencing parameters
Temperature; dissolved hydrogen/oxygen potential; cold work; microstructure
Physical explanation (1–3 processes)
  1. Grain-boundary oxidation and crack-tip deformation interact under tensile loading
Signs and symptoms
Often intergranular cracking; leakage products; limited external warning
Prevention / slowing the damage
Resistant qualified alloys; stress mitigation; primary-water control; targeted volumetric inspection
Typical failure outcome
Leak; possible pressure-boundary rupture
Possible consequences
Unplanned outage; nuclear safety challenge
Can be mistaken for
Thermal fatigue; fabrication cracks; boric-acid metal loss
How to distinguish it
Identify alloy and primary-water exposure; metallography and crack-location evidence; inspect beyond surface staining
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-039Hydrogen embrittlementEnvironment-assisted cracking & hydrogen · Hydrogen-assisted loss of ductility
Umbrella damage mechanism

Mechanism pathway

Service conditions

Absorbed hydrogen from corrosion, processing, CP or gaseous hydrogen

Physical processes

  • Hydrogen-enhanced localized plasticity (HELP)
  • Hydrogen-enhanced decohesion (HEDE)
  • Other coupled mechanisms may contribute; no single model explains every alloy

Observable damage

Delayed brittle-appearing cracks; reduced ductility/toughness

Possible failure mode

Sudden fracture or leak

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
HE; hydrogen-assisted cracking; hydrogen stress cracking
Industries / exposed sectors
Fasteners; energy; plating; marine; hydrogen systems
Typically affected parts
High-strength bolts; springs; welds; pressure boundaries
Susceptible materials
High-strength steels; susceptible titanium, nickel and other alloys
Required chemicals / environment
Absorbed hydrogen from corrosion, processing, CP or gaseous hydrogen
Influencing parameters
Hydrogen availability; strength; tensile stress; trapping; temperature
Physical explanation (1–3 processes)
  1. Hydrogen-enhanced localized plasticity (HELP)
  2. Hydrogen-enhanced decohesion (HEDE)
  3. Other coupled mechanisms may contribute; no single model explains every alloy
Signs and symptoms
Delayed brittle-appearing cracks; reduced ductility/toughness
Prevention / slowing the damage
Control hydrogen entry and strength; qualified processing/baking; avoid excessive CP; hydrogen-service testing
Typical failure outcome
Sudden fracture or leak
Possible consequences
Loss of load/containment; injury potential
Can be mistaken for
SSC; brittle cleavage; fatigue; HTHA
How to distinguish it
Exposure/processing history plus fractography and material testing; low measured hydrogen after delay does not exclude prior hydrogen
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-040Sulfide stress crackingEnvironment-assisted cracking & hydrogen · Wet-H2S hydrogen-assisted cracking
Damage mechanism

Mechanism pathway

Service conditions

Wet H2S plus tensile stress

Physical processes

  • Sour corrosion promotes hydrogen entry
  • Hydrogen-assisted fracture occurs in a stressed susceptible material

Observable damage

Brittle-appearing cracks; little warning; possible weld/HAZ concentration

Possible failure mode

Sudden break or leak

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
SSC; sulphide stress cracking
Industries / exposed sectors
Oil/gas; refining; sour service
Typically affected parts
Bolts; weld HAZ; tubing; valves; pressure equipment
Susceptible materials
Susceptible high-strength/hard steels; some other alloys
Required chemicals / environment
Wet H2S plus tensile stress
Influencing parameters
Hardness; microstructure; pH; H2S partial pressure; stress
Physical explanation (1–3 processes)
  1. Sour corrosion promotes hydrogen entry
  2. Hydrogen-assisted fracture occurs in a stressed susceptible material
Signs and symptoms
Brittle-appearing cracks; little warning; possible weld/HAZ concentration
Prevention / slowing the damage
Qualified sour-service material and hardness; weld control; environment management
Typical failure outcome
Sudden break or leak
Possible consequences
Toxic/flammable release; loss of restraint
Can be mistaken for
HIC; SOHIC; weld hydrogen cracking
How to distinguish it
Assess hardness/stress and sour exposure; distinguish stress-driven cracks from rolling-plane HIC arrays
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-041Hydrogen-induced crackingEnvironment-assisted cracking & hydrogen · Internal hydrogen damage
Damage mechanism

Mechanism pathway

Service conditions

Hydrogen charging, commonly wet H2S

Physical processes

  • Hydrogen accumulates at internal traps and recombines
  • Internal pressure creates planar cracks which can link stepwise

Observable damage

Internal laminarlike cracks parallel to rolling; possible blistering

Possible failure mode

Leak or rupture after linked cracking

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
HIC; stepwise cracking
Industries / exposed sectors
Sour oil/gas; refining
Typically affected parts
Linepipe walls; vessel plates; wet sour-service equipment
Susceptible materials
Susceptible rolled carbon/low-alloy steel with traps/inclusions
Required chemicals / environment
Hydrogen charging, commonly wet H2S
Influencing parameters
Steel cleanliness; trapping sites; pH; charging severity
Physical explanation (1–3 processes)
  1. Hydrogen accumulates at internal traps and recombines
  2. Internal pressure creates planar cracks which can link stepwise
Signs and symptoms
Internal laminarlike cracks parallel to rolling; possible blistering
Prevention / slowing the damage
HIC-resistant clean steel; appropriate sour-service control; qualified testing and UT
Typical failure outcome
Leak or rupture after linked cracking
Possible consequences
Loss of containment; reduced pressure capacity
Can be mistaken for
Laminations; SOHIC; lamellar tearing
How to distinguish it
Section cracks and inclusions; establish charging history; applied tensile stress is not required for HIC initiation
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-042Stress-oriented hydrogen-induced crackingEnvironment-assisted cracking & hydrogen · Stress-directed hydrogen damage
Damage mechanism

Mechanism pathway

Service conditions

Hydrogen charging, typically wet H2S, plus tensile stress

Physical processes

  • Hydrogen forms small internal cracks
  • Tensile stress promotes stacked crack arrays linking through thickness

Observable damage

Ladder-like stacked HIC arrays; through-wall linkage near welds

Possible failure mode

Leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
SOHIC
Industries / exposed sectors
Refining; sour oil/gas; chemical
Typically affected parts
Pressure-vessel plates near welds; stressed sour piping
Susceptible materials
Susceptible carbon/low-alloy steels
Required chemicals / environment
Hydrogen charging, typically wet H2S, plus tensile stress
Influencing parameters
Triaxial/residual stress; weld geometry; hydrogen flux; cleanliness
Physical explanation (1–3 processes)
  1. Hydrogen forms small internal cracks
  2. Tensile stress promotes stacked crack arrays linking through thickness
Signs and symptoms
Ladder-like stacked HIC arrays; through-wall linkage near welds
Prevention / slowing the damage
Reduce local stress; select tested resistant steel; control sour conditions; qualified volumetric inspection
Typical failure outcome
Leak or rupture
Possible consequences
Toxic/flammable release
Can be mistaken for
HIC; SSC; lamellar tearing
How to distinguish it
Cross-sections show stress-oriented stacks linking through wall; distinguish from single rolling-plane laminations
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-043Hydrogen blisteringEnvironment-assisted cracking & hydrogen · Internal hydrogen damage
Damage mechanism

Mechanism pathway

Service conditions

Hydrogen entry, often from wet acidic/sour corrosion

Physical processes

  • Hydrogen recombines to gas at internal discontinuities
  • Gas pressure deforms or separates the overlying metal

Observable damage

Bulges; domed blisters; planar subsurface separations

Possible failure mode

Blister rupture; leak

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Blister damage; hydrogen pressure blistering
Industries / exposed sectors
Refining; wet sour service; chemical
Typically affected parts
Vessel plates; piping walls; tank shells
Susceptible materials
Susceptible carbon steels with internal traps/laminations
Required chemicals / environment
Hydrogen entry, often from wet acidic/sour corrosion
Influencing parameters
Hydrogen flux; inclusion/lamination population; wall restraint
Physical explanation (1–3 processes)
  1. Hydrogen recombines to gas at internal discontinuities
  2. Gas pressure deforms or separates the overlying metal
Signs and symptoms
Bulges; domed blisters; planar subsurface separations
Prevention / slowing the damage
Limit hydrogen charging; clean HIC-resistant materials; evaluate remaining ligament and connected cracks
Typical failure outcome
Blister rupture; leak
Possible consequences
Containment loss; reduced ligament capacity
Can be mistaken for
Coating blisters; HIC; fabrication laminations
How to distinguish it
Verify metal-wall bulging and subsurface gas cavity; distinguish from paint-only blisters
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-044Liquid metal embrittlementEnvironment-assisted cracking & hydrogen · Liquid-metal environment-assisted fracture
Damage mechanism

Mechanism pathway

Service conditions

A compatible embrittling liquid metal wetting a stressed susceptible solid

Physical processes

  • Liquid metal reaches highly stressed surface/crack regions
  • Adsorption/penetration assists loss of cohesion and crack advance

Observable damage

Rapid low-ductility cracks, often intergranular

Possible failure mode

Sudden fracture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
LME; liquid-metal-assisted cracking
Industries / exposed sectors
Galvanizing; welding; chemical; metal processing
Typically affected parts
Loaded steel during galvanizing; contaminated welds; susceptible liquid-metal equipment
Susceptible materials
Specific couples, e.g. steel/liquid zinc or copper; aluminium/liquid mercury
Required chemicals / environment
A compatible embrittling liquid metal wetting a stressed susceptible solid
Influencing parameters
Wetting; temperature above liquidus; stress; contact chemistry
Physical explanation (1–3 processes)
  1. Liquid metal reaches highly stressed surface/crack regions
  2. Adsorption/penetration assists loss of cohesion and crack advance
Signs and symptoms
Rapid low-ductility cracks, often intergranular
Prevention / slowing the damage
Exclude incompatible metal contamination; qualified galvanizing/welding practices; reduce restraint
Typical failure outcome
Sudden fracture
Possible consequences
Loss of structural support or containment
Can be mistaken for
Solidification cracking; reheat cracking; ordinary brittle fracture
How to distinguish it
Identify embrittling metal on/in crack path and liquid-state exposure; preserve evidence before cleaning
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No verified LME catastrophe assigned here. Flixborough (1 June 1974) is not used as a proven LME case: the regulator’s account describes failure of a temporary bypass, not an established LME root cause.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-045Irradiation-assisted stress corrosion crackingEnvironment-assisted cracking & hydrogen · Radiation/environment interaction
Damage mechanism

Mechanism pathway

Service conditions

Reactor water, neutron exposure and tensile stress

Physical processes

  • Radiation changes grain-boundary chemistry and hardening
  • Localized deformation/oxidation under water promotes intergranular cracking

Observable damage

Intergranular cracks; bolt/internal-component failures

Possible failure mode

Bolt fracture; component separation; loss of structural function

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
IASCC
Industries / exposed sectors
Nuclear power
Typically affected parts
Core internals; baffle-former bolts; irradiated structural parts
Susceptible materials
Irradiated austenitic stainless steels and susceptible alloys
Required chemicals / environment
Reactor water, neutron exposure and tensile stress
Influencing parameters
Dose; temperature; water chemistry; stress; microstructure
Physical explanation (1–3 processes)
  1. Radiation changes grain-boundary chemistry and hardening
  2. Localized deformation/oxidation under water promotes intergranular cracking
Signs and symptoms
Intergranular cracks; bolt/internal-component failures
Prevention / slowing the damage
Qualified irradiation-resistant materials; chemistry/stress management; targeted in-service inspection
Typical failure outcome
Bolt fracture; component separation; loss of structural function
Possible consequences
Loose parts; internal support degradation; outage
Can be mistaken for
Irradiation embrittlement; fatigue; unirradiated SCC
How to distinguish it
Confirm dose and aqueous exposure; correlate boundary cracking and material changes; irradiation alone is not proof of IASCC
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-046High-temperature oxidationHigh-temperature chemical damage · Gas/metal reaction
Damage mechanism

Mechanism pathway

Service conditions

Oxygen-bearing hot gas; liquid water is unnecessary

Physical processes

  • Oxide grows by interfacial reaction and diffusion
  • Cracking/spallation exposes fresh metal and renews consumption

Observable damage

Scale; section loss; spalled flakes; dimensional change

Possible failure mode

Thinning-related rupture; scale blockage

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Dry oxidation; scaling
Industries / exposed sectors
Power; furnaces; steel processing; aerospace
Typically affected parts
Furnace tubes; exhausts; turbine parts; hot structures
Susceptible materials
Steels; nickel alloys; other metals with inadequate oxide protection
Required chemicals / environment
Oxygen-bearing hot gas; liquid water is unnecessary
Influencing parameters
Temperature; time; oxygen potential; thermal cycling; alloy chemistry
Physical explanation (1–3 processes)
  1. Oxide grows by interfacial reaction and diffusion
  2. Cracking/spallation exposes fresh metal and renews consumption
Signs and symptoms
Scale; section loss; spalled flakes; dimensional change
Prevention / slowing the damage
Oxidation-resistant alloy/coating; temperature control; reduce severe cycling; monitor scale and remaining wall
Typical failure outcome
Thinning-related rupture; scale blockage
Possible consequences
Overheating; debris damage; outage
Can be mistaken for
Hot corrosion; sulfidation; atmospheric rust
How to distinguish it
Identify scale phases and hot-service exposure; verify whether molten salts or sulfur caused the attack
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-047Steam-side oxidation and exfoliationHigh-temperature chemical damage · Steam/metal reaction
Damage mechanism

Mechanism pathway

Service conditions

High-temperature steam

Physical processes

  • Steam-side oxide thickens and consumes metal
  • Growth/thermal mismatch causes oxide spallation

Observable damage

Internal scale; exfoliated particles; restricted tube flow

Possible failure mode

Tube rupture or flow blockage by exfoliated scale

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Steam oxidation; oxide-scale exfoliation
Industries / exposed sectors
Fossil power; heat recovery; high-temperature steam
Typically affected parts
Superheater/reheater tubes; steam piping
Susceptible materials
Ferritic and austenitic heat-resistant steels
Required chemicals / environment
High-temperature steam
Influencing parameters
Temperature; time; alloy chromium; surface condition; thermal transients
Physical explanation (1–3 processes)
  1. Steam-side oxide thickens and consumes metal
  2. Growth/thermal mismatch causes oxide spallation
Signs and symptoms
Internal scale; exfoliated particles; restricted tube flow
Prevention / slowing the damage
Appropriate steam-resistant alloy/surface treatment; manage temperature and cycling; inspect scale/blockage
Typical failure outcome
Tube rupture or flow blockage by exfoliated scale
Possible consequences
Overheating; outage; downstream erosion or turbine damage from detached scale
Can be mistaken for
Creep; fireside oxidation; deposit fouling
How to distinguish it
Locate oxide on steam side; analyse scale layers and deposits; separate oxidation loss from creep cavities
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-048High-temperature sulfidationHigh-temperature chemical damage · Sulfur/metal reaction
Damage mechanism

Mechanism pathway

Service conditions

Reactive sulfur species at elevated temperature; no water required

Physical processes

  • Metal reacts to form sulfide scale
  • Insufficiently protective scale permits continuing wall loss

Observable damage

Sulfide scale; broad thinning; individual components may corrode faster

Possible failure mode

Leak or catastrophic rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Sulfidic corrosion; sulfur corrosion
Industries / exposed sectors
Refining; petrochemical; high-temperature processing
Typically affected parts
Crude-unit piping; furnace tubes; sulfur-bearing process equipment
Susceptible materials
Carbon/low-alloy steels; susceptibility depends on alloy chemistry
Required chemicals / environment
Reactive sulfur species at elevated temperature; no water required
Influencing parameters
Temperature; sulfur species; silicon/chromium content; flow
Physical explanation (1–3 processes)
  1. Metal reacts to form sulfide scale
  2. Insufficiently protective scale permits continuing wall loss
Signs and symptoms
Sulfide scale; broad thinning; individual components may corrode faster
Prevention / slowing the damage
Verify materials component-by-component; resistant alloys; targeted thickness monitoring
Typical failure outcome
Leak or catastrophic rupture
Possible consequences
Hydrocarbon release; fire
Can be mistaken for
Wet H2S corrosion; naphthenic acid corrosion; oxidation
How to distinguish it
Confirm hot service, sulfide scale and alloy chemistry; inspect fittings individually, not only adjacent pipe
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
Chevron Richmond, 6 August 2012: severe sulfidation thinning in low-silicon carbon-steel piping led to rupture and a major refinery fire. CSB completed its investigation in 2015.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-049Hot corrosion by molten saltsHigh-temperature chemical damage · Salt-assisted high-temperature corrosion
Damage mechanism

Mechanism pathway

Service conditions

Aggressive deposits, often sulfates or vanadium-bearing salts

Physical processes

  • Molten deposits dissolve or destabilize protective oxides
  • Accelerated oxidation/sulfidation consumes exposed alloy

Observable damage

Pitted scale; undercut coatings; sulfide/oxide penetration

Possible failure mode

Blade/tube fracture or perforation

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Type I/Type II hot corrosion; deposit-induced hot corrosion
Industries / exposed sectors
Gas turbines; aviation; boilers; incineration
Typically affected parts
Turbine blades/vanes; combustors; hot tubes
Susceptible materials
Nickel/cobalt superalloys; heat-resistant steels
Required chemicals / environment
Aggressive deposits, often sulfates or vanadium-bearing salts
Influencing parameters
Salt chemistry; temperature/melting behaviour; oxygen/sulfur potential; deposit flux
Physical explanation (1–3 processes)
  1. Molten deposits dissolve or destabilize protective oxides
  2. Accelerated oxidation/sulfidation consumes exposed alloy
Signs and symptoms
Pitted scale; undercut coatings; sulfide/oxide penetration
Prevention / slowing the damage
Fuel/air contaminant control; resistant coatings/alloys; approved deposit removal
Typical failure outcome
Blade/tube fracture or perforation
Possible consequences
Rotor damage; forced outage
Can be mistaken for
Ordinary oxidation; sulfidation; erosion
How to distinguish it
Analyse deposit and scale chemistry; confirm relevant molten-salt regime; temperature alone cannot assign Type I/II
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-050Naphthenic acid corrosionHigh-temperature chemical damage · Hot-oil acid attack
Damage mechanism

Mechanism pathway

Service conditions

Reactive organic acids in hot oil; aqueous phase unnecessary

Physical processes

  • Organic acids react with iron to form oil-soluble iron carboxylates
  • Film stability and sulfur interactions govern local attack

Observable damage

Sharp grooves; localized or broad wall loss in hot-oil circuits

Possible failure mode

Leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
NAC; hot organic-acid corrosion
Industries / exposed sectors
Crude refining; heavy-oil processing
Typically affected parts
Hot crude/vacuum distillation piping; transfer lines; pumps
Susceptible materials
Carbon/low-alloy steel; alloy resistance depends on molybdenum and environment
Required chemicals / environment
Reactive organic acids in hot oil; aqueous phase unnecessary
Influencing parameters
Acid structure; temperature; flow; sulfur chemistry; scale stability
Physical explanation (1–3 processes)
  1. Organic acids react with iron to form oil-soluble iron carboxylates
  2. Film stability and sulfur interactions govern local attack
Signs and symptoms
Sharp grooves; localized or broad wall loss in hot-oil circuits
Prevention / slowing the damage
Evaluate real feed corrosivity, not TAN alone; appropriate resistant alloys; control flow/hot spots
Typical failure outcome
Leak or rupture
Possible consequences
Hot hydrocarbon release; fire
Can be mistaken for
Sulfidation; erosion-corrosion
How to distinguish it
Correlate acid/sulfur chemistry, temperature and morphology; total acid number alone is not diagnostic
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-051High-temperature hydrogen/hydrogen-sulfide corrosionHigh-temperature chemical damage · High-temperature gas-phase corrosion
Environment-specific sulfidation subtype

Mechanism pathway

Service conditions

Hot H2/H2S gas; liquid water not required

Physical processes

  • Sulfur-bearing hot gas reacts with alloy constituents
  • Sulfide formation consumes or penetrates the load-bearing metal

Observable damage

Wall loss and internal sulfide penetration

Possible failure mode

Leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
H2/H2S corrosion; reducing-gas sulfidation
Industries / exposed sectors
Hydrotreating; hydrocracking; gas processing
Typically affected parts
Reactor-effluent piping; heater tubes; hot exchangers
Susceptible materials
Steels and heat-resistant alloys; resistance depends on alloy and gas conditions
Required chemicals / environment
Hot H2/H2S gas; liquid water not required
Influencing parameters
Temperature; exposure; gas composition; sulfur/oxygen potentials; alloy chemistry
Physical explanation (1–3 processes)
  1. Sulfur-bearing hot gas reacts with alloy constituents
  2. Sulfide formation consumes or penetrates the load-bearing metal
Signs and symptoms
Wall loss and internal sulfide penetration
Prevention / slowing the damage
Duty-qualified alloys; chemistry/temperature management; thickness monitoring
Typical failure outcome
Leak or rupture
Possible consequences
Hydrogen/hydrocarbon/H2S release; fire
Can be mistaken for
HTHA; wet H2S corrosion; ordinary sulfidation
How to distinguish it
Prove gas-phase hot reducing exposure; metallography separates surface loss from internal methane damage
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-052High-temperature hydrogen attackHigh-temperature chemical damage · Methane-forming internal damage
Damage mechanism

Mechanism pathway

Service conditions

Hydrogen at elevated temperature and sufficient activity/partial pressure

Physical processes

  • Hydrogen reacts with carbon to form trapped methane
  • Methane cavities grow and link while steel decarburizes

Observable damage

Internal fissures/cavities; decarburization; late-stage cracking

Possible failure mode

Brittle-appearing rupture or leak

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
HTHA; hot hydrogen attack
Industries / exposed sectors
Refining; hydrogen processing; ammonia
Typically affected parts
Hot hydrogen vessels; exchanger shells; piping; weld regions
Susceptible materials
Carbon/low-alloy steels with insufficient carbide stability for the duty
Required chemicals / environment
Hydrogen at elevated temperature and sufficient activity/partial pressure
Influencing parameters
Temperature; hydrogen pressure; time; carbides; weld condition
Physical explanation (1–3 processes)
  1. Hydrogen reacts with carbon to form trapped methane
  2. Methane cavities grow and link while steel decarburizes
Signs and symptoms
Internal fissures/cavities; decarburization; late-stage cracking
Prevention / slowing the damage
Use duty-qualified resistant materials; verify operating envelope; specialized validated inspection
Typical failure outcome
Brittle-appearing rupture or leak
Possible consequences
Major fire/explosion; fatalities possible
Can be mistaken for
Ambient HE; creep; thermal decarburization
How to distinguish it
Metallography identifies methane-type cavities and carbon depletion; no single negative NDT test proves absence
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
Tesoro Anacortes, 2 April 2010: HTHA in a heat-exchanger shell caused a catastrophic rupture/fire; seven workers died.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-053CarburizationHigh-temperature chemical damage · Interstitial uptake
Damage mechanism

Mechanism pathway

Service conditions

Carbon-rich gas with sufficiently high carbon activity

Physical processes

  • Carbon enters the exposed alloy
  • Carburized microstructure changes local properties; defects in a protective coating can concentrate attack

Observable damage

Subsurface carburization; locally deep attack at protective-coating defects

Possible failure mode

Cracking or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Carbon uptake; internal carburization
Industries / exposed sectors
Petrochemical cracking; reforming; heat-treatment furnaces
Typically affected parts
Furnace tubes; retorts; high-temperature internals
Susceptible materials
Heat-resistant nickel alloys; steels in related carbon-uptake service
Required chemicals / environment
Carbon-rich gas with sufficiently high carbon activity
Influencing parameters
Temperature; carbon activity; time; oxide protection
Physical explanation (1–3 processes)
  1. Carbon enters the exposed alloy
  2. Carburized microstructure changes local properties; defects in a protective coating can concentrate attack
Signs and symptoms
Subsurface carburization; locally deep attack at protective-coating defects
Prevention / slowing the damage
Control carbon potential; resistant alloy/coating; preserve protective scale; monitor microstructure
Typical failure outcome
Cracking or rupture
Possible consequences
Tube failure; fire/outage
Can be mistaken for
Metal dusting; intentional case hardening; sigma embrittlement
How to distinguish it
Carbon profiles and carbide identification; distinguish intact carburized metal from disintegrating metal dusting
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-054DecarburizationHigh-temperature chemical damage · Interstitial loss
Damage mechanism

Mechanism pathway

Service conditions

Atmosphere able to remove carbon, e.g. oxidizing/wet gases; environment-specific

Physical processes

  • Carbon diffuses toward a low-carbon-potential surface
  • Surface reactions remove carbon, reducing hardenability/strength

Observable damage

Soft ferritic surface layer; reduced hardness; fatigue initiation

Possible failure mode

Wear-out, distortion or later fatigue fracture; immediate failure is not inevitable

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Carbon depletion; surface decarburization
Industries / exposed sectors
Heat treatment; forging; high-temperature service
Typically affected parts
Spring surfaces; forgings; tubes; steel components
Susceptible materials
Carbon and low-alloy steels
Required chemicals / environment
Atmosphere able to remove carbon, e.g. oxidizing/wet gases; environment-specific
Influencing parameters
Temperature; time; carbon potential; scale integrity
Physical explanation (1–3 processes)
  1. Carbon diffuses toward a low-carbon-potential surface
  2. Surface reactions remove carbon, reducing hardenability/strength
Signs and symptoms
Soft ferritic surface layer; reduced hardness; fatigue initiation
Prevention / slowing the damage
Control furnace atmosphere and thermal exposure; verify the affected depth before acceptance
Typical failure outcome
Wear-out, distortion or later fatigue fracture; immediate failure is not inevitable
Possible consequences
Reduced life; potential component break
Can be mistaken for
HTHA decarburization; overtempering; carburization gradients
How to distinguish it
Compare carbon-sensitive microstructure and hardness depth profiles; distinguish surface carbon loss from internal methane-cavity damage
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-055Metal dustingHigh-temperature chemical damage · Carbon-driven disintegration
Damage mechanism

Mechanism pathway

Service conditions

Strongly carburizing gas; carbon activity above graphite equilibrium

Physical processes

  • Carbon supersaturation/carburization destabilizes near-surface metal
  • Metal breaks down into particles associated with coke/carbon

Observable damage

Pits; metal powder in coke; rapid local wastage

Possible failure mode

Perforation or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Catastrophic carburization; carbon-induced disintegration
Industries / exposed sectors
Syngas; reforming; petrochemical; heat treatment
Typically affected parts
Process tubes; heat exchangers; furnace internals
Susceptible materials
Iron, nickel and cobalt alloys under susceptible conditions
Required chemicals / environment
Strongly carburizing gas; carbon activity above graphite equilibrium
Influencing parameters
Temperature; CO/H2 chemistry; water content; surface scale
Physical explanation (1–3 processes)
  1. Carbon supersaturation/carburization destabilizes near-surface metal
  2. Metal breaks down into particles associated with coke/carbon
Signs and symptoms
Pits; metal powder in coke; rapid local wastage
Prevention / slowing the damage
Control gas chemistry and temperatures; resistant materials/coatings; maintain protective scales
Typical failure outcome
Perforation or rupture
Possible consequences
Syngas release; fire; outage
Can be mistaken for
Carburization without dusting; erosion; sulfidation
How to distinguish it
Identify metal particles/carbon and disintegrated microstructure; correlate with carbon activity and process conditions
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-056Uncontrolled nitriding damageHigh-temperature chemical damage · Interstitial uptake
Uncontrolled uptake / property degradation

Mechanism pathway

Service conditions

Nitrogen-bearing gas with sufficient nitriding potential, often NH3-containing

Physical processes

  • Ammonia dissociation supplies nitrogen that enters the alloy
  • Brittle nitride formation and protective-oxide defects promote cracking

Observable damage

Brittle nitride formation; cracks; quasi-cleavage in the reported coil case

Possible failure mode

Cracking or brittle break

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
In-service nitridation; nitrogen uptake
Industries / exposed sectors
Ammonia; chemical; high-temperature processing
Typically affected parts
Heating coils; ammonia-service hot components
Susceptible materials
FeCrAl heating alloys; other nitride-forming alloys require service-specific assessment
Required chemicals / environment
Nitrogen-bearing gas with sufficient nitriding potential, often NH3-containing
Influencing parameters
Temperature; exposure; ammonia pressure; protective-oxide integrity
Physical explanation (1–3 processes)
  1. Ammonia dissociation supplies nitrogen that enters the alloy
  2. Brittle nitride formation and protective-oxide defects promote cracking
Signs and symptoms
Brittle nitride formation; cracks; quasi-cleavage in the reported coil case
Prevention / slowing the damage
Qualify alloy and protective surfaces for actual ammonia conditions; monitor cracking
Typical failure outcome
Cracking or brittle break
Possible consequences
Loss of containment or internal-component failure
Can be mistaken for
Carburization; sigma phase; intentional nitriding
How to distinguish it
Nitrogen profile and nitride identification; deliberate controlled nitriding is not automatically damage
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
A 2024 laboratory failure investigation attributed premature failure of FeCrAl heating coils in hot, pressurized ammonia to destructive nitridation. It is not a population incidence estimate or a public-accident report.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-057Creep deformation and cavitationCreep & metallurgical ageing · Time-dependent elevated-temperature damage
Umbrella damage mechanism

Mechanism pathway

Service conditions

None essential; oxidation/corrosion may accelerate damage

Physical processes

  • Dislocation/diffusion-controlled deformation accumulates
  • Grain-boundary cavities can nucleate and link under stress

Observable damage

Bulging; elongation; cavitation; creep cracks; warning may be limited

Possible failure mode

Stress rupture; leak; excessive deformation

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Creep damage; time-dependent deformation; legacy title: creep and stress rupture
Industries / exposed sectors
Power; refining; turbines; high-temperature processing
Typically affected parts
Steam pipes; headers; tubes; turbine blades; hot bolts
Susceptible materials
Steels; nickel/cobalt alloys; other metals at material-dependent high homologous temperature
Required chemicals / environment
None essential; oxidation/corrosion may accelerate damage
Influencing parameters
Metal temperature; sustained stress; time; microstructure
Physical explanation (1–3 processes)
  1. Dislocation/diffusion-controlled deformation accumulates
  2. Grain-boundary cavities can nucleate and link under stress
Signs and symptoms
Bulging; elongation; cavitation; creep cracks; warning may be limited
Prevention / slowing the damage
Control metal temperature/stress; suitable alloy/heat treatment; life assessment and targeted inspection
Typical failure outcome
Stress rupture; leak; excessive deformation
Possible consequences
Steam/hydrocarbon release; blade failure; outage
Can be mistaken for
Short-term overheating; HTHA; creep-fatigue
How to distinguish it
Assess service history, dimensions, cavities and microstructure; surface replication alone may miss internal damage
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-058Creep-fatigue interactionCreep & metallurgical ageing · Time/cycle interaction
Damage mechanism

Mechanism pathway

Service conditions

None essential; oxidation often contributes

Physical processes

  • Cyclic plasticity initiates/grows cracks
  • Creep during hot holds damages boundaries
  • Interaction can shorten life beyond separate mechanisms

Observable damage

Mixed intergranular/transgranular cracking; cavities near cyclic cracks

Possible failure mode

Crack/leak; rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Creep–fatigue damage
Industries / exposed sectors
Flexible power generation; turbines; process heaters
Typically affected parts
Headers; thick-section joints; blades; thermal-transition regions
Susceptible materials
High-temperature steels and superalloys
Required chemicals / environment
None essential; oxidation often contributes
Influencing parameters
Hold times; strain range; temperature; cycling sequence; stress relaxation
Physical explanation (1–3 processes)
  1. Cyclic plasticity initiates/grows cracks
  2. Creep during hot holds damages boundaries
  3. Interaction can shorten life beyond separate mechanisms
Signs and symptoms
Mixed intergranular/transgranular cracking; cavities near cyclic cracks
Prevention / slowing the damage
Manage start/stop transients and dwell stress; joint design; validated interaction-life assessment
Typical failure outcome
Crack/leak; rupture
Possible consequences
Forced outage; hot-fluid release
Can be mistaken for
Thermal fatigue alone; creep alone; reheat cracking
How to distinguish it
Combine cycle/dwell records with fracture path and cavitation; do not assume linear damage addition is always valid
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-059Type IV creep crackingCreep & metallurgical ageing · Weld-HAZ creep subtype
Creep subtype

Mechanism pathway

Service conditions

None essential

Physical processes

  • Creep strain localizes in the weaker outer HAZ
  • Boundary cavities coalesce into a through-wall crack

Observable damage

HAZ cavity bands; cracks away from fusion boundary; limited overall strain

Possible failure mode

Leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Type IV weld failure
Industries / exposed sectors
Power; petrochemical steam systems
Typically affected parts
Fine-grained/intercritical HAZ in ferritic weldments
Susceptible materials
Cr-Mo and creep-strength-enhanced ferritic steels, including 9–12% Cr grades
Required chemicals / environment
None essential
Influencing parameters
Temperature; sustained stress; weld/PWHT microstructure; time
Physical explanation (1–3 processes)
  1. Creep strain localizes in the weaker outer HAZ
  2. Boundary cavities coalesce into a through-wall crack
Signs and symptoms
HAZ cavity bands; cracks away from fusion boundary; limited overall strain
Prevention / slowing the damage
Qualified material/weld/heat treatment; stress and temperature control; HAZ-targeted volumetric inspection
Typical failure outcome
Leak or rupture
Possible consequences
High-energy steam release; outage
Can be mistaken for
Reheat cracking; Type I/II/III weld creep; HTHA
How to distinguish it
Locate damage in fine/intercritical HAZ and demonstrate creep cavities; examine subsurface material
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-060Dissimilar-metal weld creep/interface failureCreep & metallurgical ageing · Dissimilar-joint creep subtype
Joint-specific creep family

Mechanism pathway

Service conditions

None essential; oxidation may assist exposed interfaces

Physical processes

  • Carbon migration creates a carbon-depleted zone with lower creep strength
  • Creep damage can localize beside the fusion boundary

Observable damage

Cracks near fusion boundary; carbide-depleted region; creep damage

Possible failure mode

Leak or weld separation

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
DMW creep; fusion-boundary creep damage
Industries / exposed sectors
Power; refining; high-temperature piping
Typically affected parts
Ferritic-to-austenitic/nickel welds; dissimilar ferritic joints
Susceptible materials
Dissimilar heat-resistant steels and nickel filler combinations
Required chemicals / environment
None essential; oxidation may assist exposed interfaces
Influencing parameters
Alloy/carbon-activity difference; heat treatment; operating stress; temperature; time
Physical explanation (1–3 processes)
  1. Carbon migration creates a carbon-depleted zone with lower creep strength
  2. Creep damage can localize beside the fusion boundary
Signs and symptoms
Cracks near fusion boundary; carbide-depleted region; creep damage
Prevention / slowing the damage
Qualify filler and heat treatment for the dissimilar joint; assess cross-weld creep strength
Typical failure outcome
Leak or weld separation
Possible consequences
Steam/hydrocarbon release; outage
Can be mistaken for
Type IV creep; lack of fusion; reheat cracking
How to distinguish it
Locate crack relative to fusion boundary and HAZ; carbon/hardness mapping plus cavities and service history
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-061Overheating-induced softening and rapid deformationCreep & metallurgical ageing · Acute thermal overload
Damage mechanism

Mechanism pathway

Service conditions

No corrosive species essential; deposits or blocked cooling can raise metal temperature

Physical processes

  • Acute overheating reduces the wall’s load-bearing capacity
  • Plastic flow under internal pressure can rapidly open a rupture

Observable damage

Bulging; thin-lipped burst in acute overheating; thermally altered microstructure

Possible failure mode

Tube burst

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Short-term overheating damage; legacy title: short-term overheating rupture
Industries / exposed sectors
Boilers; fired heaters; furnaces
Typically affected parts
Waterwall/superheater tubes; flame-impinged coils
Susceptible materials
Carbon/low-alloy steel; heat-resistant alloys
Required chemicals / environment
No corrosive species essential; deposits or blocked cooling can raise metal temperature
Influencing parameters
Peak metal temperature; duration; pressure; heat flux; cooling flow
Physical explanation (1–3 processes)
  1. Acute overheating reduces the wall’s load-bearing capacity
  2. Plastic flow under internal pressure can rapidly open a rupture
Signs and symptoms
Bulging; thin-lipped burst in acute overheating; thermally altered microstructure
Prevention / slowing the damage
Maintain cooling flow; prevent dryout/flame impingement; protective trips and temperature monitoring
Typical failure outcome
Tube burst
Possible consequences
Hot-fluid release; fire; forced outage
Can be mistaken for
Long-term creep; thinning-induced burst; thermal shock
How to distinguish it
Reconstruct excursion and remaining wall; metallography distinguishes acute heating from long-term cavitation
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-062Thermal graphitization of steelCreep & metallurgical ageing · Thermal microstructural degradation
Microstructural degradation

Mechanism pathway

Service conditions

None essential

Physical processes

  • Metastable carbides decompose
  • Graphite precipitates; linked particles/bands weaken the steel

Observable damage

Graphite particles or linked HAZ bands; associated loss of strength/toughness

Possible failure mode

Low-ductility rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Graphitisation; carbide decomposition
Industries / exposed sectors
Older power/process high-temperature systems
Typically affected parts
Carbon/carbon-molybdenum steel pipe; weld HAZ
Susceptible materials
Susceptible carbon and carbon-molybdenum steels
Required chemicals / environment
None essential
Influencing parameters
Long thermal exposure; composition; weld thermal history
Physical explanation (1–3 processes)
  1. Metastable carbides decompose
  2. Graphite precipitates; linked particles/bands weaken the steel
Signs and symptoms
Graphite particles or linked HAZ bands; associated loss of strength/toughness
Prevention / slowing the damage
Appropriate alloy selection; metallographic surveillance; replace critically affected material
Typical failure outcome
Low-ductility rupture
Possible consequences
High-energy release; structural failure
Can be mistaken for
Graphitic corrosion of cast iron; creep cavities; inclusions
How to distinguish it
Identify newly precipitated graphite in steel without selective external iron dissolution
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-063Spheroidization-related thermal softeningCreep & metallurgical ageing · Loss of strengthening microstructure
Property degradation family

Mechanism pathway

Service conditions

None essential

Physical processes

  • Lamellar cementite changes toward a spheroidal morphology during thermal exposure
  • Associated softening can reduce fatigue life at a given stress amplitude

Observable damage

Spheroidized carbides; reduced hardness; changed fatigue response

Possible failure mode

Excessive deformation; later creep rupture or fatigue fracture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Pearlite spheroidization; thermal softening; related carbide-coarsening softening
Industries / exposed sectors
Rail transport; hot-service steel equipment
Typically affected parts
Railway wheels; other thermally exposed pearlitic-steel parts
Susceptible materials
Pearlitic steels; direct study concerns railway wheelset steels
Required chemicals / environment
None essential
Influencing parameters
Temperature; time; initial microstructure; prior heat treatment
Physical explanation (1–3 processes)
  1. Lamellar cementite changes toward a spheroidal morphology during thermal exposure
  2. Associated softening can reduce fatigue life at a given stress amplitude
Signs and symptoms
Spheroidized carbides; reduced hardness; changed fatigue response
Prevention / slowing the damage
Limit thermal exposure; correct initial treatment; assess mechanical properties before continued service
Typical failure outcome
Excessive deformation; later creep rupture or fatigue fracture
Possible consequences
Reduced load/life margin
Can be mistaken for
Decarburization; normal annealed structure; graphitization
How to distinguish it
Compare carbide morphology and hardness with the original material; distinguish carbon depletion and intentionally spheroidized supply condition
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-064Temper embrittlementCreep & metallurgical ageing · Grain-boundary segregation embrittlement
Damage mechanism

Mechanism pathway

Service conditions

None essential

Physical processes

  • Impurities segregate to grain boundaries
  • Boundary cohesion decreases and brittle-transition behaviour worsens

Observable damage

Reduced notch toughness; intergranular brittle fracture; little hardness change may occur

Possible failure mode

Brittle fracture, especially during cool/pressurized conditions

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Reversible temper embrittlement
Industries / exposed sectors
Refining; power; heavy forgings
Typically affected parts
Cr-Mo vessels; turbine rotors; thick low-alloy steel
Susceptible materials
Susceptible alloy steels with impurity/chemistry combinations
Required chemicals / environment
None essential
Influencing parameters
Thermal exposure/cooling history; impurity content; alloy composition
Physical explanation (1–3 processes)
  1. Impurities segregate to grain boundaries
  2. Boundary cohesion decreases and brittle-transition behaviour worsens
Signs and symptoms
Reduced notch toughness; intergranular brittle fracture; little hardness change may occur
Prevention / slowing the damage
Low-impurity suitable steel; qualified heat treatment; toughness assessment and controlled startup
Typical failure outcome
Brittle fracture, especially during cool/pressurized conditions
Possible consequences
Major pressure-boundary failure
Can be mistaken for
Hydrogen embrittlement; irradiation embrittlement; cleavage
How to distinguish it
Toughness/transition testing, thermal history and boundary fracture; routine hardness alone is inadequate
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-065475°C embrittlementCreep & metallurgical ageing · Ferrite decomposition embrittlement
Microstructural embrittlement

Mechanism pathway

Service conditions

None essential

Physical processes

  • Ferrite separates into iron-rich and chromium-rich regions
  • Nanoscale decomposition hardens and embrittles ferrite

Observable damage

Toughness/ductility loss; hardening; often no obvious optical change

Possible failure mode

Brittle-appearing cracking/fracture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Alpha-prime embrittlement; 885°F embrittlement
Industries / exposed sectors
Chemical; power; duplex/high-chromium equipment
Typically affected parts
Ferritic/duplex stainless parts; ferrite in weld metal
Susceptible materials
Chromium-rich ferrite in ferritic/duplex stainless steels
Required chemicals / environment
None essential
Influencing parameters
Temperature-time exposure; ferrite composition; initial phase balance
Physical explanation (1–3 processes)
  1. Ferrite separates into iron-rich and chromium-rich regions
  2. Nanoscale decomposition hardens and embrittles ferrite
Signs and symptoms
Toughness/ductility loss; hardening; often no obvious optical change
Prevention / slowing the damage
Avoid unsuitable thermal exposure; validated material/heat-treatment selection; mechanical-property assessment
Typical failure outcome
Brittle-appearing cracking/fracture
Possible consequences
Reduced tolerance to defects and transients
Can be mistaken for
Sigma embrittlement; strain ageing; HE
How to distinguish it
Use exposure history and suitable microstructural/mechanical testing; ordinary optical microscopy may miss nanoscale decomposition
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-066Sigma/chi-phase embrittlementCreep & metallurgical ageing · Intermetallic precipitation
Microstructural embrittlement

Mechanism pathway

Service conditions

None essential; corrosion resistance can deteriorate afterward

Physical processes

  • Brittle sigma/chi phases precipitate during unsuitable thermal exposure
  • Phase formation changes hardness, toughness and corrosion response

Observable damage

Intermetallic particles; toughness loss; selective corrosion of depleted zones

Possible failure mode

Brittle fracture or subsequent localized-corrosion leak

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Intermetallic-phase embrittlement
Industries / exposed sectors
Chemical; refining; power; welded stainless equipment
Typically affected parts
Duplex components; stainless welds; heat-exchanger parts
Susceptible materials
Duplex/austenitic stainless and some high-alloy systems
Required chemicals / environment
None essential; corrosion resistance can deteriorate afterward
Influencing parameters
Thermal history; Cr/Mo content; phase balance; cooling rate
Physical explanation (1–3 processes)
  1. Brittle sigma/chi phases precipitate during unsuitable thermal exposure
  2. Phase formation changes hardness, toughness and corrosion response
Signs and symptoms
Intermetallic particles; toughness loss; selective corrosion of depleted zones
Prevention / slowing the damage
Correct welding/heat-treatment windows; qualified phase testing; avoid prolonged unsuitable temperature
Typical failure outcome
Brittle fracture or subsequent localized-corrosion leak
Possible consequences
Unexpected cracking; reduced corrosion margin
Can be mistaken for
475°C embrittlement; sensitization; carbides
How to distinguish it
Identify secondary phases using metallography and suitable compositional analysis; correlate with heat history and mechanical testing
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-067Strain-ageing embrittlementCreep & metallurgical ageing · Interstitial/dislocation interaction
Property degradation

Mechanism pathway

Service conditions

None essential

Physical processes

  • Carbon/nitrogen segregate to dislocations
  • Dislocation pinning raises yield response and can reduce ductility/toughness

Observable damage

Yield-point return; hardness/strength increase; toughness loss

Possible failure mode

Low-ductility cracking or fracture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Static strain ageing; strain aging
Industries / exposed sectors
Structural steel; fabrication; pipelines
Typically affected parts
Cold-worked/bent plates; formed parts; strain-hardened regions
Susceptible materials
Susceptible ferritic steels containing mobile carbon/nitrogen
Required chemicals / environment
None essential
Influencing parameters
Prior plastic strain; ageing time/temperature; free interstitial content
Physical explanation (1–3 processes)
  1. Carbon/nitrogen segregate to dislocations
  2. Dislocation pinning raises yield response and can reduce ductility/toughness
Signs and symptoms
Yield-point return; hardness/strength increase; toughness loss
Prevention / slowing the damage
Suitable killed/low-free-interstitial steel; control cold work; qualified processing and toughness checks
Typical failure outcome
Low-ductility cracking or fracture
Possible consequences
Reduced forming/service margin
Can be mistaken for
Temper embrittlement; cold-work hardening alone; HE
How to distinguish it
Compare prestrain/ageing history and mechanical response; do not infer from hardness alone
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-068Neutron irradiation embrittlementCreep & metallurgical ageing · Radiation-induced microstructural damage
Property degradation

Mechanism pathway

Service conditions

None chemically essential; energetic-neutron exposure

Physical processes

  • Neutron exposure changes the steel microstructure
  • Fracture toughness decreases, increasing sensitivity to existing flaws

Observable damage

Toughness/impact-property deterioration in surveillance specimens

Possible failure mode

Brittle fracture if loading exceeds degraded resistance

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Radiation embrittlement; vessel embrittlement
Industries / exposed sectors
Nuclear power
Typically affected parts
Reactor-vessel beltline and welds; irradiated structural parts
Susceptible materials
Reactor pressure-vessel steels and welds
Required chemicals / environment
None chemically essential; energetic-neutron exposure
Influencing parameters
Neutron fluence/flux; exposure temperature; steel chemistry and heat treatment
Physical explanation (1–3 processes)
  1. Neutron exposure changes the steel microstructure
  2. Fracture toughness decreases, increasing sensitivity to existing flaws
Signs and symptoms
Toughness/impact-property deterioration in surveillance specimens
Prevention / slowing the damage
Material surveillance, fluence and operating-envelope assessment; approved vessel-integrity programs
Typical failure outcome
Brittle fracture if loading exceeds degraded resistance
Possible consequences
Pressure-boundary safety challenge
Can be mistaken for
Temper embrittlement; IASCC; ordinary thermal ageing
How to distinguish it
Use dosimetry/surveillance and toughness data; IASCC additionally needs an environment-assisted crack process
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-069High-cycle fatigueFatigue · Cyclic crack initiation and growth
Damage mechanism

Mechanism pathway

Service conditions

None essential; corrosion can accelerate growth

Physical processes

  • Localized cyclic slip initiates a crack
  • Repeated loading grows it until remaining section fails

Observable damage

Progressive crack growth; striations in some materials; visual inspection can miss tight cracks

Possible failure mode

Final break; occasionally leak before break

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
HCF; nominally elastic fatigue
Industries / exposed sectors
Rotating machinery; transport; aerospace; structures
Typically affected parts
Shafts; weld toes; blades; bolts; structural joints
Susceptible materials
Most engineering metals
Required chemicals / environment
None essential; corrosion can accelerate growth
Influencing parameters
Stress range/mean; cycles; notch geometry; residual stress; surface defects
Physical explanation (1–3 processes)
  1. Localized cyclic slip initiates a crack
  2. Repeated loading grows it until remaining section fails
Signs and symptoms
Progressive crack growth; striations in some materials; visual inspection can miss tight cracks
Prevention / slowing the damage
Reduce stress concentration and cyclic loads; improve surface/joint quality; damage-tolerant inspection
Typical failure outcome
Final break; occasionally leak before break
Possible consequences
Rotor/structure failure; shutdown; injury potential
Can be mistaken for
LCF; vibration fatigue; SCC; overload
How to distinguish it
Fractography plus stress/cycle reconstruction; no beach marks does not exclude fatigue
How often is it seen?
DNV reports fatigue as 30% of >1,000 oil/gas-maritime investigations; it does not disclose an HCF-only percentage. Do not assign 30% to this subtype.
Historical case / verification status
Aloha Flight 243 (1988): undetected fatigue/disbonding caused fuselage separation and one fatality. This is a verified fatigue example; the cited accident summary does not classify local HCF versus LCF strain.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-070Low-cycle fatigueFatigue · Cyclic plastic deformation
Damage mechanism

Mechanism pathway

Service conditions

None essential

Physical processes

  • Repeated plastic strain localizes damage
  • Cracks propagate under successive large strain excursions

Observable damage

Fatigue cracks associated with cyclic plastic strain; cyclic hardening/softening can occur

Possible failure mode

Fracture or through-wall leak

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
LCF; plastic-strain fatigue
Industries / exposed sectors
Power cycling; aerospace; pressure equipment
Typically affected parts
Notches; vessel/nozzle transitions; turbine discs; highly strained joints
Susceptible materials
Structural metals; direct cited experiments used 42CrMo4 steel
Required chemicals / environment
None essential
Influencing parameters
Plastic strain range; mean strain; cycles; temperature; hold time
Physical explanation (1–3 processes)
  1. Repeated plastic strain localizes damage
  2. Cracks propagate under successive large strain excursions
Signs and symptoms
Fatigue cracks associated with cyclic plastic strain; cyclic hardening/softening can occur
Prevention / slowing the damage
Limit strain concentration and severe transients; strain-based design; suitable material and inspection
Typical failure outcome
Fracture or through-wall leak
Possible consequences
Loss of containment or load capacity
Can be mistaken for
HCF; ratcheting; creep-fatigue
How to distinguish it
Reconstruct local strain history and crack growth; cycle count alone does not distinguish the fatigue regime
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-071Very-high-cycle fatigueFatigue · Long-life fatigue regime
Fatigue life-regime subtype

Mechanism pathway

Service conditions

None essential

Physical processes

  • Small defects or microstructural regions initiate cracks after long cycling
  • Internal cracks may grow into fish-eye/FGA features before final fracture

Observable damage

Internal origins; fish-eye regions in some alloys; absence does not exclude VHCF

Possible failure mode

Unexpected fracture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
VHCF; gigacycle fatigue
Industries / exposed sectors
Aerospace; bearings; rail; high-speed machinery
Typically affected parts
Shafts; bearings; high-cycle loaded internal defects
Susceptible materials
High-strength steels; titanium/aluminium and other alloys
Required chemicals / environment
None essential
Influencing parameters
Very large cycle counts; inclusion size/location; stress gradient; surface condition
Physical explanation (1–3 processes)
  1. Small defects or microstructural regions initiate cracks after long cycling
  2. Internal cracks may grow into fish-eye/FGA features before final fracture
Signs and symptoms
Internal origins; fish-eye regions in some alloys; absence does not exclude VHCF
Prevention / slowing the damage
Control inclusions/defects; use applicable long-life data; do not assume universal infinite endurance
Typical failure outcome
Unexpected fracture
Possible consequences
High-speed component failure
Can be mistaken for
HCF; inclusion-origin overload; hydrogen-assisted fatigue
How to distinguish it
Fractography of origin plus demonstrated loading duration/cycles; fish-eye is not universal
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-072Thermal fatigueFatigue · Temperature-gradient-driven fatigue
Damage mechanism

Mechanism pathway

Service conditions

None essential

Physical processes

  • Nonuniform thermal expansion creates cyclic stress/strain
  • Repeated local strain initiates and advances cracks

Observable damage

Surface crack networks; cracks at thermal mixing or gradients

Possible failure mode

Leak or fracture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Thermal cycling damage; heat checking
Industries / exposed sectors
Power; nuclear; refining; tooling
Typically affected parts
Mixing tees; boiler ligaments; dies; hot/cold interfaces
Susceptible materials
Steels; cast irons; stainless and heat-resistant alloys
Required chemicals / environment
None essential
Influencing parameters
Temperature swing; gradient; ramp rate; restraint; cycle count
Physical explanation (1–3 processes)
  1. Nonuniform thermal expansion creates cyclic stress/strain
  2. Repeated local strain initiates and advances cracks
Signs and symptoms
Surface crack networks; cracks at thermal mixing or gradients
Prevention / slowing the damage
Reduce gradients/ramp severity; improve mixing/design; compatible expansion; inspect hot spots
Typical failure outcome
Leak or fracture
Possible consequences
Hot-fluid release; tool or plant outage
Can be mistaken for
Thermal shock; mechanical fatigue; chloride SCC
How to distinguish it
Correlate crack map with thermal transients and restraint; test for corrosive species when plausible
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-073Corrosion fatigueFatigue · Corrosion/cycle interaction
Damage mechanism

Mechanism pathway

Service conditions

Corrosive environment plus cyclic loading

Physical processes

  • Corrosion pits/film breakdown accelerate initiation
  • Environment-assisted crack growth combines with cyclic loading

Observable damage

Pit-origin or multiple cracks; corroded fracture features

Possible failure mode

Break or leak

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Environment-assisted fatigue
Industries / exposed sectors
Offshore; marine; pipelines; pumps; power
Typically affected parts
Welded risers; shafts; wet cyclically loaded joints
Susceptible materials
Steels; aluminium and other engineering alloys
Required chemicals / environment
Corrosive environment plus cyclic loading
Influencing parameters
Frequency; stress range; electrochemical potential; pH; hydrogen; temperature
Physical explanation (1–3 processes)
  1. Corrosion pits/film breakdown accelerate initiation
  2. Environment-assisted crack growth combines with cyclic loading
Signs and symptoms
Pit-origin or multiple cracks; corroded fracture features
Prevention / slowing the damage
Control both corrosion and cyclic stress; compatible protection; environment-specific fatigue assessment
Typical failure outcome
Break or leak
Possible consequences
Loss of structure/containment
Can be mistaken for
SCC; dry fatigue; hydrogen-assisted cracking
How to distinguish it
Demonstrate cyclic loading and exposure; growth behaviour/frequency effects help separate from sustained-load SCC
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-074Fretting fatigueFatigue · Oscillatory-contact fatigue
Damage mechanism

Mechanism pathway

Service conditions

None essential; oxidation often accompanies fretting

Physical processes

  • Oscillatory contact creates high local tractions and surface damage
  • Cracks initiate near contact edges and grow under cyclic bulk loading

Observable damage

Contact-edge cracks; polished/dark wear patches; oxide debris

Possible failure mode

Fatigue break

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Contact-assisted fatigue
Industries / exposed sectors
Aerospace; turbines; rail; rotating machinery
Typically affected parts
Blade roots; press fits; bolted joints; splines
Susceptible materials
Steels; titanium; aluminium and other metallic contacts
Required chemicals / environment
None essential; oxidation often accompanies fretting
Influencing parameters
Microslip; contact pressure; bulk cyclic stress; contact geometry
Physical explanation (1–3 processes)
  1. Oscillatory contact creates high local tractions and surface damage
  2. Cracks initiate near contact edges and grow under cyclic bulk loading
Signs and symptoms
Contact-edge cracks; polished/dark wear patches; oxide debris
Prevention / slowing the damage
Manage contact geometry/preload and microslip; qualified coatings/lubrication; appropriate material pairing
Typical failure outcome
Fatigue break
Possible consequences
Blade/shaft/joint failure
Can be mistaken for
Fretting wear alone; ordinary fatigue; corrosion fatigue
How to distinguish it
Locate fatigue origin at the contact edge and establish small-amplitude slip plus cyclic stress
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-075Rolling-contact fatigueFatigue · Repeated Hertzian-contact fatigue
Damage mechanism

Mechanism pathway

Service conditions

None essential; lubricant contamination and water modify severity

Physical processes

  • Repeated contact shear initiates surface or subsurface cracks
  • Cracks link to release flakes/spalls

Observable damage

Pitting/spalling on contact tracks; vibration; debris

Possible failure mode

Bearing wear-out or seizure; possible secondary fracture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
RCF; contact spalling; surface/subsurface fatigue
Industries / exposed sectors
Bearings; gears; rail; wind turbines
Typically affected parts
Raceways; rolling elements; gear flanks; wheel/rail contacts
Susceptible materials
Bearing/gear steels; surface-hardened contact materials
Required chemicals / environment
None essential; lubricant contamination and water modify severity
Influencing parameters
Contact stress; lubrication; roughness; inclusions; alignment; cycles
Physical explanation (1–3 processes)
  1. Repeated contact shear initiates surface or subsurface cracks
  2. Cracks link to release flakes/spalls
Signs and symptoms
Pitting/spalling on contact tracks; vibration; debris
Prevention / slowing the damage
Correct load/alignment; clean adequate lubricant; suitable hardness/cleanliness; condition monitoring
Typical failure outcome
Bearing wear-out or seizure; possible secondary fracture
Possible consequences
Machine failure; secondary damage
Can be mistaken for
Electrical erosion; indentation; abrasive wear
How to distinguish it
Cross-section and microscopy locate crack origins; compare with fluting/melt craters and contamination
How often is it seen?
SKF (2022) assigns 16% of identified bearing failure modes to surface-initiated fatigue. This is not the fraction for all RCF or the probability a bearing will fail.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-076Vibration-induced fatigueFatigue · Dynamically excited fatigue
Loading-specific HCF subtype

Mechanism pathway

Service conditions

None essential

Physical processes

  • Dynamic excitation creates repeated stress
  • Local fatigue cracks grow, often at branch or weld notches

Observable damage

Cracks near supports/branches; vibration; intermittent leakage

Possible failure mode

Through-wall leak or fatigue break

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
VIF; acoustic/pulsation-induced fatigue
Industries / exposed sectors
Process piping; rotating machinery; aerospace
Typically affected parts
Small-bore branches; instrument connections; supports; compressor lines
Susceptible materials
Metals, especially welded/stress-concentrated details
Required chemicals / environment
None essential
Influencing parameters
Excitation frequency/amplitude; resonance; damping; support stiffness; weld geometry
Physical explanation (1–3 processes)
  1. Dynamic excitation creates repeated stress
  2. Local fatigue cracks grow, often at branch or weld notches
Signs and symptoms
Cracks near supports/branches; vibration; intermittent leakage
Prevention / slowing the damage
Measure excitation; address resonance/source; engineer supports; avoid merely adding unassessed restraints
Typical failure outcome
Through-wall leak or fatigue break
Possible consequences
Process release; detached parts
Can be mistaken for
Other HCF; thermal fatigue; overload
How to distinguish it
Operating vibration/modal measurements plus fracture origin; a vibrating component is not proof of causal fatigue
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-077Thermomechanical fatigueFatigue · Coupled thermal/mechanical cycling
Damage mechanism

Mechanism pathway

Service conditions

None essential; oxidation can interact

Physical processes

  • Mechanical and thermal strains cycle with a defined phase relationship
  • Temperature-dependent plasticity, oxidation and sometimes creep interact

Observable damage

Surface cracks; oxide-assisted cracking; evolving cyclic response

Possible failure mode

Cracking or fracture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
TMF; in-phase/out-of-phase TMF
Industries / exposed sectors
Turbines; engines; aerospace; high-temperature power
Typically affected parts
Hot-section blades; exhaust manifolds; constrained heated parts
Susceptible materials
Superalloys; heat-resistant steels; other thermally cycled metals
Required chemicals / environment
None essential; oxidation can interact
Influencing parameters
Temperature/strain phasing; mechanical strain range; dwell; gradient
Physical explanation (1–3 processes)
  1. Mechanical and thermal strains cycle with a defined phase relationship
  2. Temperature-dependent plasticity, oxidation and sometimes creep interact
Signs and symptoms
Surface cracks; oxide-assisted cracking; evolving cyclic response
Prevention / slowing the damage
Reduce thermal/mechanical strain mismatch; design for actual phase history; qualified coatings and life models
Typical failure outcome
Cracking or fracture
Possible consequences
Engine/turbine loss of function; outage
Can be mistaken for
Thermal fatigue; isothermal LCF; creep-fatigue
How to distinguish it
Reconstruct mechanical strain separately from free thermal strain and establish phasing; damage morphology alone is insufficient
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-078Adhesive wear and gallingWear, flow & surface damage · Sliding-contact damage
Wear family; galling is a severe form

Mechanism pathway

Service conditions

None essential; lubricant failure increases risk

Physical processes

  • Asperities form adhesive junctions
  • Junction tearing transfers metal; severe interaction can seize contact

Observable damage

Smeared/transferred metal; torn surfaces; rising friction

Possible failure mode

Seizure; leakage; secondary break

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Scuffing; seizure; adhesive transfer
Industries / exposed sectors
Fasteners; valves; pumps; machinery
Typically affected parts
Threads; valve trim; sliding guides; wear rings
Susceptible materials
Metal couples, including stainless and titanium pairs
Required chemicals / environment
None essential; lubricant failure increases risk
Influencing parameters
Contact load; sliding; material pairing; roughness; lubrication; alignment
Physical explanation (1–3 processes)
  1. Asperities form adhesive junctions
  2. Junction tearing transfers metal; severe interaction can seize contact
Signs and symptoms
Smeared/transferred metal; torn surfaces; rising friction
Prevention / slowing the damage
Compatible material pair/coating; correct lubrication; alignment; controlled assembly
Typical failure outcome
Seizure; leakage; secondary break
Possible consequences
Loss of motion/isolation; machine outage
Can be mistaken for
Abrasive wear; overheating; fretting wear
How to distinguish it
Look for metal transfer and torn junctions, not solely parallel scratches; inspect mating surface
How often is it seen?
SKF (2022): adhesive wear is 7% of identified bearing failure modes. This bearing-cohort result is not a galling incidence across all industries.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-079Abrasive wearWear, flow & surface damage · Hard-particle/asperity wear
Damage mechanism

Mechanism pathway

Service conditions

No reactive chemical required; hard particles/asperities are necessary

Physical processes

  • Hard particles cut or plough a surface
  • Repeated contact removes or displaces material

Observable damage

Grooves; polishing; dimensional loss; embedded particles

Possible failure mode

Wear-out; excessive clearance; eventual leak or break

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Two-body/three-body abrasion; scratching wear
Industries / exposed sectors
Mining; earthmoving; cement; bearings; machinery
Typically affected parts
Liners; chutes; tools; seals; contaminated bearings
Susceptible materials
Most metals; resistance depends on hardness, toughness and microstructure
Required chemicals / environment
No reactive chemical required; hard particles/asperities are necessary
Influencing parameters
Particle hardness/shape/size; load; sliding distance; impact
Physical explanation (1–3 processes)
  1. Hard particles cut or plough a surface
  2. Repeated contact removes or displaces material
Signs and symptoms
Grooves; polishing; dimensional loss; embedded particles
Prevention / slowing the damage
Exclude/filter abrasives; wear-resistant surfaces; suitable hardness-toughness balance; replaceable liners
Typical failure outcome
Wear-out; excessive clearance; eventual leak or break
Possible consequences
Reduced efficiency; contamination; downtime
Can be mistaken for
Adhesive wear; solid-particle erosion; machining marks
How to distinguish it
Match groove/particle geometry and relative motion; analyse debris and contact conditions
How often is it seen?
SKF (2022): abrasive wear is 26% of identified bearing failure modes, highest in its displayed dataset. Sample size and observation period are not disclosed.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-080Fretting wearWear, flow & surface damage · Small-amplitude contact wear
Damage mechanism

Mechanism pathway

Service conditions

No reactive species essential; air/moisture commonly oxidize debris

Physical processes

  • Oscillatory slip removes surface films and material
  • Wear debris oxidizes and can act as abrasive

Observable damage

Red/brown or dark debris; localized wear scars; roller-spaced marks

Possible failure mode

Loss of fit or wear-out; possible later fatigue break

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Fretting corrosion; false brinelling in some bearing contexts
Industries / exposed sectors
Bearings; turbines; transport; electrical/mechanical joints
Typically affected parts
Press fits; shaft seats; parked bearings; connectors
Susceptible materials
Metallic contacting surfaces
Required chemicals / environment
No reactive species essential; air/moisture commonly oxidize debris
Influencing parameters
Microslip amplitude; contact pressure; vibration; lubrication
Physical explanation (1–3 processes)
  1. Oscillatory slip removes surface films and material
  2. Wear debris oxidizes and can act as abrasive
Signs and symptoms
Red/brown or dark debris; localized wear scars; roller-spaced marks
Prevention / slowing the damage
Control unwanted microslip/vibration; appropriate fit/preload; lubrication and storage/transport measures
Typical failure outcome
Loss of fit or wear-out; possible later fatigue break
Possible consequences
Misalignment; vibration; reduced joint reliability
Can be mistaken for
Fretting fatigue; true brinelling; electrical fluting
How to distinguish it
Confirm oscillatory contact wear; section for fatigue cracks; plastic indentations without wear suggest brinelling
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-081Solid-particle erosionWear, flow & surface damage · Impact-driven material removal
Damage mechanism

Mechanism pathway

Service conditions

No corrosive chemical required; impinging particles in gas/flow

Physical processes

  • Particle impacts cut/plough ductile surfaces or fracture brittle regions

Observable damage

Directional wastage; impact craters; leading-edge thinning

Possible failure mode

Perforation; blade loss; wear-out

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Particle impingement erosion; gas-borne erosion
Industries / exposed sectors
Power; mining; pneumatic conveying; turbines
Typically affected parts
Duct bends; boiler tubes; turbine blades; chutes
Susceptible materials
Engineering metals and coatings
Required chemicals / environment
No corrosive chemical required; impinging particles in gas/flow
Influencing parameters
Velocity; impact angle; particle size/shape/hardness; temperature
Physical explanation (1–3 processes)
  1. Particle impacts cut/plough ductile surfaces or fracture brittle regions
Signs and symptoms
Directional wastage; impact craters; leading-edge thinning
Prevention / slowing the damage
Reduce particle loading/velocity; improve flow path; resistant liners/coatings; targeted inspections
Typical failure outcome
Perforation; blade loss; wear-out
Possible consequences
Release; turbine/boiler damage; downtime
Can be mistaken for
Slurry erosion; corrosion thinning; abrasion
How to distinguish it
Identify particles and impact trajectories; compare sheltered and impinged locations
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-082Slurry erosionWear, flow & surface damage · Liquid-borne particle damage
Damage mechanism

Mechanism pathway

Service conditions

Liquid carrying hard solids; corrosive liquid may add synergy

Physical processes

  • Liquid carries particles into sliding/impact contact
  • Cutting, ploughing or repeated impact removes metal

Observable damage

Localized grooves; impeller/outer-bend loss; dimensional wear

Possible failure mode

Leak; loss of pump performance; rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Slurry abrasion; solids-in-liquid wear
Industries / exposed sectors
Mining; dredging; mineral processing; slurry transport
Typically affected parts
Pump impellers; elbows; valves; liners
Susceptible materials
Steels; cast irons; alloys; metallic coatings
Required chemicals / environment
Liquid carrying hard solids; corrosive liquid may add synergy
Influencing parameters
Solids concentration; velocity; angle; particle distribution; material properties
Physical explanation (1–3 processes)
  1. Liquid carries particles into sliding/impact contact
  2. Cutting, ploughing or repeated impact removes metal
Signs and symptoms
Localized grooves; impeller/outer-bend loss; dimensional wear
Prevention / slowing the damage
Duty-specific pump/flow design; resistant liners; solids control; thickness monitoring
Typical failure outcome
Leak; loss of pump performance; rupture
Possible consequences
Slurry release; downtime
Can be mistaken for
Cavitation; erosion-corrosion; dry abrasion
How to distinguish it
Analyse slurry and flow paths; identify impact/wear features and any chemical contribution
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-083Cavitation erosionWear, flow & surface damage · Vapour-bubble-collapse damage
Damage mechanism

Mechanism pathway

Service conditions

A liquid capable of local vaporization; no corrosive chemistry essential

Physical processes

  • Low local pressure creates vapour cavities
  • Collapse near metal produces microjets/shock loads
  • Repeated impacts fatigue and remove surface material

Observable damage

Honeycomb-like craters; noise; vibration; performance loss

Possible failure mode

Through-wall leak; loss of component performance; possible secondary fracture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Cavitation pitting
Industries / exposed sectors
Pumps; hydropower; marine; valves
Typically affected parts
Impellers; propellers; turbine runners; throttling zones
Susceptible materials
Engineering metals exposed to cavitating liquid
Required chemicals / environment
A liquid capable of local vaporization; no corrosive chemistry essential
Influencing parameters
Pressure relative to vapour pressure; temperature; velocity; inlet conditions
Physical explanation (1–3 processes)
  1. Low local pressure creates vapour cavities
  2. Collapse near metal produces microjets/shock loads
  3. Repeated impacts fatigue and remove surface material
Signs and symptoms
Honeycomb-like craters; noise; vibration; performance loss
Prevention / slowing the damage
Correct suction/pressure conditions; suitable geometry/operation; resistant surfaces
Typical failure outcome
Through-wall leak; loss of component performance; possible secondary fracture
Possible consequences
Loss of flow/efficiency; equipment outage
Can be mistaken for
Corrosion pitting; droplet erosion; particle erosion
How to distinguish it
Establish cavitating hydraulics and crater distribution; no diagnosis from pits alone
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-084Liquid-droplet impingement erosionWear, flow & surface damage · Repeated liquid-impact damage
Damage mechanism

Mechanism pathway

Service conditions

High-relative-speed droplets or intermittent liquid impact

Physical processes

  • Droplet impact generates high transient surface stress
  • Repeated impacts deform/fatigue the surface and detach material

Observable damage

Leading-edge pits; roughened impact zone; progressing material loss

Possible failure mode

Loss of blade performance; possible blade fracture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Liquid impact erosion; droplet erosion
Industries / exposed sectors
Steam turbines; aviation; high-speed flow systems
Typically affected parts
Wet-steam blade leading edges; high-speed metallic surfaces
Susceptible materials
Steels; titanium; nickel and other blade alloys
Required chemicals / environment
High-relative-speed droplets or intermittent liquid impact
Influencing parameters
Impact velocity; droplet size; angle; exposure; material fatigue response
Physical explanation (1–3 processes)
  1. Droplet impact generates high transient surface stress
  2. Repeated impacts deform/fatigue the surface and detach material
Signs and symptoms
Leading-edge pits; roughened impact zone; progressing material loss
Prevention / slowing the damage
Reduce wetness/impact severity; erosion-resistant shields/coatings; inspect leading edges
Typical failure outcome
Loss of blade performance; possible blade fracture
Possible consequences
Turbine/engine damage; outage
Can be mistaken for
Cavitation; solid-particle erosion; corrosion
How to distinguish it
Relate attack to droplet trajectories and wetness; no vapour-collapse zone or abrasive particles is necessary
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-085Erosion-corrosionWear, flow & surface damage · Mechanical/chemical synergy
Damage mechanism

Mechanism pathway

Service conditions

Corrosive fluid plus mechanical surface/film damage

Physical processes

  • Mechanical action removes/damages protective films
  • Fresh metal corrodes; corrosion can facilitate further erosion

Observable damage

Flow-oriented grooves; local thinning; combined oxide/wear evidence

Possible failure mode

Leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Flow-assisted erosion–corrosion; tribocorrosion in flow
Industries / exposed sectors
Marine; chemical; refining; water/slurry systems
Typically affected parts
Elbows; pump impellers; valves; exchanger inlets
Susceptible materials
Steels; copper alloys; stainless and other metals
Required chemicals / environment
Corrosive fluid plus mechanical surface/film damage
Influencing parameters
Velocity; turbulence; particles/bubbles; chemistry; film recovery
Physical explanation (1–3 processes)
  1. Mechanical action removes/damages protective films
  2. Fresh metal corrodes; corrosion can facilitate further erosion
Signs and symptoms
Flow-oriented grooves; local thinning; combined oxide/wear evidence
Prevention / slowing the damage
Control chemistry and impingement; suitable flow design; resistant material/coating
Typical failure outcome
Leak or rupture
Possible consequences
Process release; loss of performance
Can be mistaken for
FAC; pure erosion; general corrosion
How to distinguish it
Demonstrate both mechanical damage and corrosion; distinguish magnetite-dissolution FAC from particle/bubble action
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-086Flow-accelerated corrosionWear, flow & surface damage · Oxide dissolution controlled by mass transfer
Damage mechanism

Mechanism pathway

Service conditions

Water or wet steam and chemistry allowing oxide dissolution

Physical processes

  • Protective magnetite dissolves into moving water
  • Re-forming oxide and continuing dissolution consume metal

Observable damage

Scalloped/orange-peel thinning; local severe wall loss

Possible failure mode

Pipe rupture or leak

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
FAC; flow-assisted corrosion
Industries / exposed sectors
Fossil/nuclear power; industrial steam
Typically affected parts
Carbon-steel feedwater; condensate; wet-steam piping; elbows
Susceptible materials
Carbon/low-alloy steels, strongly influenced by chromium content
Required chemicals / environment
Water or wet steam and chemistry allowing oxide dissolution
Influencing parameters
Temperature; pH; redox/oxygen; mass transfer; alloy chromium
Physical explanation (1–3 processes)
  1. Protective magnetite dissolves into moving water
  2. Re-forming oxide and continuing dissolution consume metal
Signs and symptoms
Scalloped/orange-peel thinning; local severe wall loss
Prevention / slowing the damage
Plant-specific water chemistry; resistant replacement alloy; predictive screening plus thickness inspection
Typical failure outcome
Pipe rupture or leak
Possible consequences
High-energy hot-water/steam release
Can be mistaken for
Erosion-corrosion; droplet erosion; caustic gouging
How to distinguish it
Confirm aqueous chemistry/flow context and oxide-dissolution loss; hard particles/cavitation are not required
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
Surry Unit 2, 9 December 1986: feedwater-system pipe rupture from wall thinning killed four workers; NRC documents the event in its erosion/corrosion operating-experience guidance.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-087Electrical erosion of bearingsWear, flow & surface damage · Discharge-driven surface damage
Damage mechanism

Mechanism pathway

Service conditions

No chemical necessary; current through the bearing is required

Physical processes

  • Electrical discharge locally melts/vaporizes contact spots
  • Repeated discharge and rolling develop pitting/fluting

Observable damage

Microscopic melt craters; washboard fluting; darkened lubricant; noise

Possible failure mode

Bearing wear-out or seizure

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Current leakage damage; electrical pitting; fluting
Industries / exposed sectors
Electric motors; generators; variable-speed drives; rail
Typically affected parts
Bearing raceways and rolling elements
Susceptible materials
Conductive bearing steels
Required chemicals / environment
No chemical necessary; current through the bearing is required
Influencing parameters
Shaft voltage; current density; lubricant film; grounding; drive switching
Physical explanation (1–3 processes)
  1. Electrical discharge locally melts/vaporizes contact spots
  2. Repeated discharge and rolling develop pitting/fluting
Signs and symptoms
Microscopic melt craters; washboard fluting; darkened lubricant; noise
Prevention / slowing the damage
Engineered shaft grounding; insulated/hybrid bearings where suitable; correct drive/cable installation
Typical failure outcome
Bearing wear-out or seizure
Possible consequences
Motor downtime; secondary shaft damage
Can be mistaken for
RCF; false brinelling; corrosion pitting
How to distinguish it
Microscopy for re-solidified craters plus shaft-current measurements; fluting alone is not uniquely diagnostic
How often is it seen?
SKF (2022): current leakage is 7% of identified bearing failure modes. Not an incidence for every motor or bearing installation.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-088Ductile overload fractureFracture & instability · Plastic fracture
Terminal fracture mechanism, not a root cause

Mechanism pathway

Service conditions

None essential

Physical processes

  • Plastic deformation nucleates voids at particles/interfaces
  • Void growth and coalescence form a tearing fracture

Observable damage

Dimples; shear lips; necking may occur but constraint can suppress it

Possible failure mode

Break or burst

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Microvoid-coalescence fracture; ductile tearing
Industries / exposed sectors
All industries using loaded metal components
Typically affected parts
Bolts; shafts; pressure boundaries; structural members
Susceptible materials
Ductile engineering metals
Required chemicals / environment
None essential
Influencing parameters
Load; stress triaxiality; temperature; defects; strain rate
Physical explanation (1–3 processes)
  1. Plastic deformation nucleates voids at particles/interfaces
  2. Void growth and coalescence form a tearing fracture
Signs and symptoms
Dimples; shear lips; necking may occur but constraint can suppress it
Prevention / slowing the damage
Avoid overload; adequate section/toughness; control defects and loading; protect against excursions
Typical failure outcome
Break or burst
Possible consequences
Loss of load/containment; possible injury
Can be mistaken for
Brittle fracture; fatigue final-overload zone; creep rupture
How to distinguish it
SEM dimples plus deformation/loading evidence; distinguish the final overload region from the initiating mechanism
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-089Brittle cleavage fractureFracture & instability · Rapid low-plasticity fracture
Terminal fracture mechanism

Mechanism pathway

Service conditions

None essential

Physical processes

  • A sharp defect initiates crystallographic cleavage
  • Crack propagates rapidly when driving force exceeds resistance

Observable damage

Cleavage facets/river patterns; little macroscopic deformation

Possible failure mode

Sudden break or vessel rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Cleavage; low-toughness fracture
Industries / exposed sectors
Structures; pressure equipment; transport; power
Typically affected parts
Notched/welded steel; thick sections; vessels; low-temperature parts
Susceptible materials
Susceptible ferritic steels and other cleavage-prone metals
Required chemicals / environment
None essential
Influencing parameters
Temperature; toughness; constraint; crack size; loading rate; stress
Physical explanation (1–3 processes)
  1. A sharp defect initiates crystallographic cleavage
  2. Crack propagates rapidly when driving force exceeds resistance
Signs and symptoms
Cleavage facets/river patterns; little macroscopic deformation
Prevention / slowing the damage
Toughness-qualified material; defect control; suitable temperature/load envelope; integrity assessment
Typical failure outcome
Sudden break or vessel rupture
Possible consequences
Fragment release; structural collapse; high-energy release
Can be mistaken for
Intergranular HE/embrittlement; fatigue; ductile overload
How to distinguish it
Fractography separates cleavage facets from dimples or boundary fracture; establish toughness and loading temperature
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-090Plastic collapse and pressure burstFracture & instability · Load-bearing instability
Terminal structural failure mode

Mechanism pathway

Service conditions

None essential; corrosion may create the weakness

Physical processes

  • Load exceeds the section’s plastic load-carrying capacity
  • Large deformation destabilizes the component or opens a rupture

Observable damage

Bulging; permanent deformation; ductile tearing; reduced wall

Possible failure mode

Burst; collapse; gross deformation

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Limit-load collapse; gross plastic instability
Industries / exposed sectors
Pressure equipment; pipelines; structures
Typically affected parts
Thinned pipes; vessels; overloaded members; weakened joints
Susceptible materials
Engineering metals with insufficient remaining section
Required chemicals / environment
None essential; corrosion may create the weakness
Influencing parameters
Pressure/load; wall thickness; geometry; yield/flow strength; temperature
Physical explanation (1–3 processes)
  1. Load exceeds the section’s plastic load-carrying capacity
  2. Large deformation destabilizes the component or opens a rupture
Signs and symptoms
Bulging; permanent deformation; ductile tearing; reduced wall
Prevention / slowing the damage
Design/protection against overload; adequate corrosion allowance; thickness/integrity assessment
Typical failure outcome
Burst; collapse; gross deformation
Possible consequences
Major release; loss of structure
Can be mistaken for
Brittle fracture; creep rupture; buckling
How to distinguish it
Measure section loss and reconstruct load/temperature; distinguish plastic capacity failure from crack-controlled instability
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-091Buckling instabilityFracture & instability · Compressive/geometric instability
Structural instability, not a chemical damage mechanism

Mechanism pathway

Service conditions

None essential

Physical processes

  • Compressive loading destabilizes the original geometry
  • Post-buckling deformation may lead to yielding, tearing or collapse

Observable damage

Lateral bowing; wrinkles; ovalization; sudden loss of stiffness

Possible failure mode

Collapse or crippling

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Elastic/inelastic buckling; shell collapse
Industries / exposed sectors
Structures; pipelines; tanks; offshore; aerospace
Typically affected parts
Columns; thin shells; vacuum vessels; tubes; gusset plates
Susceptible materials
All structural metals; geometry dominates susceptibility
Required chemicals / environment
None essential
Influencing parameters
Compression/external pressure; slenderness; imperfections; restraints; eccentricity
Physical explanation (1–3 processes)
  1. Compressive loading destabilizes the original geometry
  2. Post-buckling deformation may lead to yielding, tearing or collapse
Signs and symptoms
Lateral bowing; wrinkles; ovalization; sudden loss of stiffness
Prevention / slowing the damage
Adequate stiffness/stiffening; realistic imperfection design; prevent unintended vacuum/overload
Typical failure outcome
Collapse or crippling
Possible consequences
Loss of support; containment; structural safety
Can be mistaken for
Plastic collapse without instability; creep deformation; impact damage
How to distinguish it
Compare deformation mode and compression history with stability analysis including imperfections
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
NIST’s gusset-plate studies address the 2007 I-35W bridge collapse context and demonstrate how geometry, eccentricity and restraint influence plate buckling. No single-mechanism casualty claim is inferred here.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-092Ratcheting deformationFracture & instability · Progressive cyclic plastic strain
Progressive deformation mechanism

Mechanism pathway

Service conditions

None essential

Physical processes

  • Combined mean and cyclic loading causes asymmetric plastic increments
  • Permanent strain accumulates cycle by cycle

Observable damage

Progressive bulging/ovalization; permanent strain; subsequent fatigue cracks

Possible failure mode

Excessive deformation; fatigue leak or rupture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Incremental plastic collapse; cyclic strain accumulation
Industries / exposed sectors
Pressure piping; nuclear; cyclic process equipment
Typically affected parts
Pressurized elbows; pipes; thermal discontinuities
Susceptible materials
Ductile engineering metals
Required chemicals / environment
None essential
Influencing parameters
Steady plus cyclic load; mean stress; plastic hardening; geometry; temperature
Physical explanation (1–3 processes)
  1. Combined mean and cyclic loading causes asymmetric plastic increments
  2. Permanent strain accumulates cycle by cycle
Signs and symptoms
Progressive bulging/ovalization; permanent strain; subsequent fatigue cracks
Prevention / slowing the damage
Design for shakedown; reduce mean/cyclic load combination; validated cyclic-plasticity assessment
Typical failure outcome
Excessive deformation; fatigue leak or rupture
Possible consequences
Reduced life; loss of clearance/containment
Can be mistaken for
LCF without net strain; creep; single overload
How to distinguish it
Measure accumulated residual strain per cycle and reconstruct combined loads; distinguish time-driven creep
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-093Weld solidification crackingFabrication cracking · Last-stage solidification failure
Fabrication cracking mechanism

Mechanism pathway

Service conditions

None externally essential; low-melting segregants promote susceptibility

Physical processes

  • Final interdendritic liquid films cannot carry shrinkage strain
  • Inadequate feeding/cohesion leaves a crack during solidification

Observable damage

Centreline/crater cracks; interdendritic fracture morphology

Possible failure mode

Fabrication rejection; later leak/fracture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Solidification hot cracking; weld-centreline cracking
Industries / exposed sectors
Welded fabrication; repair; additive fusion processing
Typically affected parts
Weld centreline; craters; interdendritic regions
Susceptible materials
Susceptible steels; aluminium; nickel and other weld metals
Required chemicals / environment
None externally essential; low-melting segregants promote susceptibility
Influencing parameters
Composition; restraint; bead shape; solidification pattern; travel conditions
Physical explanation (1–3 processes)
  1. Final interdendritic liquid films cannot carry shrinkage strain
  2. Inadequate feeding/cohesion leaves a crack during solidification
Signs and symptoms
Centreline/crater cracks; interdendritic fracture morphology
Prevention / slowing the damage
Qualified filler/composition and welding parameters; suitable bead shape; reduce restraint; crater control
Typical failure outcome
Fabrication rejection; later leak/fracture
Possible consequences
Rework or latent service failure
Can be mistaken for
Liquation cracking; cold hydrogen cracking; lack of fusion
How to distinguish it
Locate within solidifying weld metal; identify dendritic path and weld timing; lack of fusion follows an unfused interface
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-094Weld liquation crackingFabrication cracking · Localized grain-boundary melting
Fabrication cracking mechanism

Mechanism pathway

Service conditions

None externally essential

Physical processes

  • Local grain-boundary liquid forms during heating
  • Tensile weld strain separates the weakened boundary before healing

Observable damage

Intergranular cracks beside fusion boundary or reheated passes

Possible failure mode

Weld rejection; later service fracture or leak

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
HAZ hot cracking; partially melted-zone cracking
Industries / exposed sectors
Aerospace; high-alloy welding; repair; fusion processing
Typically affected parts
Partially melted HAZ; reheated prior weld metal
Susceptible materials
Susceptible nickel, aluminium and other alloys
Required chemicals / environment
None externally essential
Influencing parameters
Peak thermal cycle; segregants; precipitates; restraint; heat input
Physical explanation (1–3 processes)
  1. Local grain-boundary liquid forms during heating
  2. Tensile weld strain separates the weakened boundary before healing
Signs and symptoms
Intergranular cracks beside fusion boundary or reheated passes
Prevention / slowing the damage
Qualified thermal input/filler and material condition; control restraint and heat cycling
Typical failure outcome
Weld rejection; later service fracture or leak
Possible consequences
Rework; reduced structural integrity
Can be mistaken for
Solidification cracks; reheat cracks; LME
How to distinguish it
Locate in previously solid material affected by partial melting; examine resolidified boundary products
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-095Delayed hydrogen cracking in weldsFabrication cracking · Fabrication hydrogen-assisted cracking
Fabrication hydrogen-assisted cracking

Mechanism pathway

Service conditions

Diffusible hydrogen from moisture, consumables or contamination

Physical processes

  • Hydrogen diffuses into stressed susceptible regions during/after cooling
  • Hydrogen-assisted cracking develops, sometimes after inspection

Observable damage

Delayed weld/HAZ cracks; brittle paths; hard microstructure may be present

Possible failure mode

Fabrication rejection or later service fracture

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Cold cracking; weld hydrogen cracking; underbead cracking
Industries / exposed sectors
Steel fabrication; construction; repair
Typically affected parts
Hard HAZ; weld root/toe; weld metal
Susceptible materials
Hardenable/high-strength steels; susceptible weld deposits
Required chemicals / environment
Diffusible hydrogen from moisture, consumables or contamination
Influencing parameters
Hydrogen; susceptible microstructure; tensile restraint; cooling/preheat history
Physical explanation (1–3 processes)
  1. Hydrogen diffuses into stressed susceptible regions during/after cooling
  2. Hydrogen-assisted cracking develops, sometimes after inspection
Signs and symptoms
Delayed weld/HAZ cracks; brittle paths; hard microstructure may be present
Prevention / slowing the damage
Dry low-hydrogen process; qualified preheat/heat input; control restraint; code-appropriate delayed inspection
Typical failure outcome
Fabrication rejection or later service fracture
Possible consequences
Rework; loss of integrity
Can be mistaken for
SSC; solidification cracking; lack of fusion
How to distinguish it
Check crack timing, hardness, hydrogen-control records and location; increasing heat input is not universally beneficial
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-096Reheat and stress-relief crackingFabrication cracking · Elevated-temperature strain-relaxation failure
Fabrication or early-service cracking

Mechanism pathway

Service conditions

None essential

Physical processes

  • Grain interiors strengthen during reheating
  • Stress relaxation concentrates strain on weak grain boundaries

Observable damage

Intergranular coarse-HAZ cracks, often at stress raisers

Possible failure mode

Fabrication rejection; leak/fracture in service

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Reheat cracking; stress-relaxation cracking
Industries / exposed sectors
Power; pressure-vessel fabrication; high-alloy welding
Typically affected parts
Coarse-grained HAZ; weld metal during PWHT or hot service
Susceptible materials
Susceptible Cr-Mo/low-alloy steels; some precipitation-strengthened alloys
Required chemicals / environment
None essential
Influencing parameters
Residual stress; grain size; precipitates; impurity segregation; thermal cycle
Physical explanation (1–3 processes)
  1. Grain interiors strengthen during reheating
  2. Stress relaxation concentrates strain on weak grain boundaries
Signs and symptoms
Intergranular coarse-HAZ cracks, often at stress raisers
Prevention / slowing the damage
Qualified alloy/welding/PWHT procedure; avoid severe coarse grains and notches; inspect after heat treatment
Typical failure outcome
Fabrication rejection; leak/fracture in service
Possible consequences
Rework; high-temperature integrity loss
Can be mistaken for
Type IV creep; liquation cracking; temper embrittlement
How to distinguish it
Locate coarse-grain damage and relate timing to reheating/relaxation; Type IV targets fine/intercritical HAZ
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-097Lamellar tearingFabrication cracking · Inclusion-assisted weld-shrinkage tearing
Fabrication tearing mechanism

Mechanism pathway

Service conditions

None essential

Physical processes

  • Weld shrinkage strains the plate through thickness
  • Inclusion decohesion and plastic tearing link step-like cracks

Observable damage

Stepped cracks roughly parallel to plate surface; woody fracture

Possible failure mode

Weld rejection; later joint separation

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Through-thickness tearing; lamellar cracks
Industries / exposed sectors
Heavy plate fabrication; offshore; structural welding
Typically affected parts
Restrained T/corner/cruciform joints in rolled plate
Susceptible materials
Rolled steels with poor through-thickness ductility/inclusion stringers
Required chemicals / environment
None essential
Influencing parameters
Through-thickness shrinkage strain; restraint; inclusion morphology; joint orientation
Physical explanation (1–3 processes)
  1. Weld shrinkage strains the plate through thickness
  2. Inclusion decohesion and plastic tearing link step-like cracks
Signs and symptoms
Stepped cracks roughly parallel to plate surface; woody fracture
Prevention / slowing the damage
Through-thickness-quality plate; improved joint/load direction; reduce restraint; qualified buttering where suitable
Typical failure outcome
Weld rejection; later joint separation
Possible consequences
Rework; structural integrity loss
Can be mistaken for
HIC; laminations; weld H cracking
How to distinguish it
Show stepped inclusion-linked tearing in parent plate and Z-direction shrinkage loading; HIC requires hydrogen charging evidence
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-098Quench crackingHeat treatment & thermal shock · Thermal/transformation-stress cracking
Heat-treatment cracking mechanism

Mechanism pathway

Service conditions

No corrosive chemical essential; quench medium controls heat transfer

Physical processes

  • Uneven cooling and phase transformation create incompatible strains
  • Local tensile stress exceeds the low-temperature fracture resistance

Observable damage

Cracks after hardening; sharp-corner initiation; brittle fracture features

Possible failure mode

Manufacturing rejection or later break

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Hardening cracks; quench-induced fracture
Industries / exposed sectors
Heat treatment; automotive; tools; manufacturing
Typically affected parts
Hardened gears; shafts; dies; tube/cylinder parts
Susceptible materials
Hardenable steels and susceptible heat-treated metals
Required chemicals / environment
No corrosive chemical essential; quench medium controls heat transfer
Influencing parameters
Cooling rate/distribution; section changes; hardenability; residual stress; inclusions
Physical explanation (1–3 processes)
  1. Uneven cooling and phase transformation create incompatible strains
  2. Local tensile stress exceeds the low-temperature fracture resistance
Signs and symptoms
Cracks after hardening; sharp-corner initiation; brittle fracture features
Prevention / slowing the damage
Qualified heat-treatment/quench process; sound geometry; clean steel; timely specified tempering; NDT
Typical failure outcome
Manufacturing rejection or later break
Possible consequences
Scrap; latent component fracture
Can be mistaken for
Grinding cracks; hydrogen cracks; pre-existing forging laps
How to distinguish it
Trace heat-treatment timing; metallography and oxide/temper evidence; assess transformation and thermal stresses
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
ASM documents 4140 seamless hydraulic-cylinder tubing rejected for quench cracks associated with inclusions and excessive severity for the geometry; not reported as a catastrophic public accident.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-099Grinding burn and grinding crackingHeat treatment & thermal shock · Machining-induced thermal damage
Manufacturing property degradation/cracking

Mechanism pathway

Service conditions

None essential; inadequate cooling/process control may contribute

Physical processes

  • Grinding heat locally tempers or rehardens the surface
  • Thermal strain produces harmful residual stress and sometimes cracks

Observable damage

Hardness gradients; tensile subsurface stress; burns/cracks; discoloration may be absent

Possible failure mode

Premature fatigue fracture or contact-surface failure

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Grinding thermal damage; retempering/rehardening burn
Industries / exposed sectors
Gear/bearing manufacture; aerospace; precision engineering
Typically affected parts
Ground gear teeth; bearing races; shafts; ball screws
Susceptible materials
Hardened ferromagnetic steels; other metals can suffer grinding damage
Required chemicals / environment
None essential; inadequate cooling/process control may contribute
Influencing parameters
Grinding heat input; wheel condition; removal rate; coolant; initial hardness
Physical explanation (1–3 processes)
  1. Grinding heat locally tempers or rehardens the surface
  2. Thermal strain produces harmful residual stress and sometimes cracks
Signs and symptoms
Hardness gradients; tensile subsurface stress; burns/cracks; discoloration may be absent
Prevention / slowing the damage
Control grinding energy/cooling and wheel condition; qualified inspection; reject/remediate damage
Typical failure outcome
Premature fatigue fracture or contact-surface failure
Possible consequences
Reduced life; precision-system failure
Can be mistaken for
Quench cracking; adhesive scuffing; normal grinding marks
How to distinguish it
Calibrated Barkhausen/etch/hardness or metallographic checks; surface appearance alone misses subsurface damage
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

DM-100Thermal-shock fractureHeat treatment & thermal shock · Single/severe-transient thermal fracture
Transient thermomechanical fracture

Mechanism pathway

Service conditions

None chemically essential; coolant can impose the thermal step

Physical processes

  • Rapid unequal thermal expansion/contraction creates transient stress
  • A severe excursion drives a crack beyond material resistance

Observable damage

Cracks after a sudden transient; surface-origin fracture; limited prior cycling

Possible failure mode

Fracture; possible through-wall leak or complete break

Original conceptual map. Processes may act together or be alternative explanations; not a ranked sequence, no scale, no remaining-life prediction.
Other names
Thermal shock cracking; acute thermal-gradient fracture
Industries / exposed sectors
Foundries; heat treatment; boilers; high-temperature equipment
Typically affected parts
Castings; hot components hit by cold fluid; thick-section interfaces
Susceptible materials
Metals with insufficient toughness/ductility for the gradient and restraint
Required chemicals / environment
None chemically essential; coolant can impose the thermal step
Influencing parameters
Temperature step; heat-transfer rate; thickness; restraint; toughness
Physical explanation (1–3 processes)
  1. Rapid unequal thermal expansion/contraction creates transient stress
  2. A severe excursion drives a crack beyond material resistance
Signs and symptoms
Cracks after a sudden transient; surface-origin fracture; limited prior cycling
Prevention / slowing the damage
Avoid abrupt incompatible transients; controlled heating/cooling; appropriate geometry/toughness
Typical failure outcome
Fracture; possible through-wall leak or complete break
Possible consequences
Hot-fluid release; loss of component function
Can be mistaken for
Thermal fatigue; quench cracking; cold brittle fracture
How to distinguish it
Establish acute thermal transient; distinguish repeated-cycle growth and transformation-related quench stresses
How often is it seen?
No representative subtype-specific incidence was identified in the reviewed sources. This is a data gap, not evidence of rarity.
Historical case / verification status
No mechanism-attributed catastrophe was verified in the sources reviewed; this does not mean none has occurred.

Photographs — 5 needed (real-life, not diagrams)

SLOT 1
Macro / field view
Macro / field view. the damage as an inspector first meets it on the component, in context; identify part and material.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 2
Close-up or micrograph
Close-up or micrograph. morphology at magnification: attack front, pit shape, product, phase; scale bar if a micrograph.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 3
Cross-section
Cross-section. metallographic section through the damage: depth, sub-surface extent, affected microstructure.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 4
In-service failure
In-service failure. the consequence: perforation, leak or weep trail, fracture face, or the replaced component.Not yet sourced — being collected with source, licence, date and a credibility tier.
SLOT 5
Distinguishing feature
Distinguishing feature. the single visual that separates this mechanism from its look-alikes.Not yet sourced — being collected with source, licence, date and a credibility tier.

Sources

Educational synthesis, not a diagnosis or repair instruction. Confirm the actual alloy, environment, loading and damage before selecting mitigation. Generic signs are not unique proof of a mechanism.

Version 1.1-review, generated 2026-09-08. Sources carry a credibility tier: 80 = TWI / ASNT / ASME / ASTM / API / EPRI / peer-reviewed papers and recognised failure-analysis standards; 70 = Wikipedia / Wikimedia; 50 = other inspection and case sources; 20 = general web. Questions or corrections: inquiry@matertec.com.