Weld Trincas — Tipos, Causas & D1.1:2025 Zero Tolerance
Cracks are the only Soldagem Descontinuidade with absolute zero tolerance under D1.1:2025. Table 8.1 item (1) states that any Trinca shall be unacceptable regardless of Tamanho or location — no Mínimo length, no depth threshold, no exceptions for static or cyclic loading.
The Zero-Tolerance Rule
D1.1:2025 Table 8.1 organizes Visual Critérios de aceitação into eight discontinuity categories. Seven of those categories have quantitative Limites — a Máximo depth, a maximum length, a percentage of weld length. Cracks are different. Item (1) Crack Prohibition reads: “Any crack shall be unacceptable, regardless of size or location.”
The “X” in both the statically carregado and cyclically loaded columns means this criterion applies to every structural connection type covered by D1.1. There is no connection type, no loading condition, and no Tamanho da solda for which a crack is acceptable. A hairline crack visible only under magnification is held to the same Norma as a full-penetration crack through the weld cross-section.
This absolute standard reflects the fracture mechanics reality: under cyclic loading, even a very small crack is a stress concentration that will propagate. Under static loading, a crack indicates a failure in the Processo de Soldagem that may signal other quality problems. The zero-tolerance rule eliminates any judgment call about whether a crack is “small enough.”
Crack Types in Structural Welds
- Hot Cracks (Solidification Cracks)
- Form during solidification of the Metal de Solda while it is still at elevated Temperatura. Low-melting-point impurities — primarily sulfur and phosphorus — segregate to grain boundaries as the metal solidifies. When the surrounding weld metal contracts on cooling, these weakened grain boundaries tear apart. Hot cracks typically run longitudinally along the weld centerline or through the crater at the weld termination. They are visible immediately after Soldagem.
- Cold Cracks (Hydrogen-Induced Cracking)
- Form after the weld has cooled to below approximately 300°F, driven by three factors acting together: Hidrogênio Difusível in the weld metal, a susceptible Microestrutura (hard Zona Afetada pelo Calor), and residual tensile stress. Cold cracks may not appear until hours or days after welding — which is why D1.1 Table 8.1 item (5) requires delaying Inspeção Visual of A514, A517, and A709 HPS 100W welds for 48 hours. Using Baixo Hidrogênio electrodes (H8, H4) and adequate Pré-aquecimento are the primary Prevenção methods.
- Crater Cracks
- Form at unfilled craters at weld terminations. When the arc is extinguished without filling the crater, the small weld pool solidifies rapidly under high restraint, creating a star-shaped crack pattern. D1.1 Table 8.1 item (3) requires all craters to be filled to the specified weld size. Crater cracks are one of the most preventable crack types — proper arc termination technique eliminates them.
- Lamellar Tearing
- A Metal de Base cracking mode, not a weld metal crack. Occurs in rolled plate when through-Espessura tensile stresses (from weld shrinkage in Junta em T and Junta de canto configurations) separate the low-ductility sulfide Inclusão planes parallel to the plate surface. Appears as a step-like crack beneath the weld. More common in older steels with high sulfur content. Modern steels with controlled sulfur content (Z-grade steels per ASTM A770) are significantly more resistant.
- Toe Cracks
- Initiate at the Margem da solda — the junction between the weld face and the base metal surface. The weld toe is a geometric stress concentration and a site where hydrogen from the weld metal can diffuse into the HAZ. Toe cracks are a form of hydrogen-induced cracking and are prevented by the same methods: low-hydrogen process, adequate preheat, and avoiding excessive restraint.
- Root Cracks
- Initiate at the Raiz da solda in groove welds, typically in the first pass where the cross-section is smallest and restraint is highest. Fusão incompleta at the root combined with hydrogen and residual stress creates the conditions for root cracking. Back-gouging and re-welding from the second side eliminates any root crack before it is enclosed in the completed weld.
Prevention: The Four Controls
Low-hydrogen electrodes. Diffusible hydrogen is the primary driver of Trinca a frio. Using electrodes with low hydrogen designations (H8 = max 8 mL/100g, H4 = max 4 mL/100g, H2 = max 2 mL/100g) and keeping them dry removes the hydrogen source. D1.1 Table 5.11 requires H8 or better for several base metal categories, and H4 for A913 Grade 80 (Categoria G).
Preheat and Temperatura Interpasse. Preheat slows the Taxa de Resfriamento, reducing the hardness of the heat-affected zone and giving hydrogen more time to diffuse out of the weld before the microstructure becomes susceptible. D1.1:2025 Cláusula 5.7 and Table 5.11 establish minimum preheat temperatures as mandatory “shall” Requisitos for Pré-qualificado WPSs — not recommendations.
Proper base metal cleanliness. Mill scale, moisture, oil, and paint introduce contaminants that increase hydrogen content and promote Trinca a quente. D1.1 Clause 7.14 requires base metal preparation before welding.
Correct arc termination. Filling craters before extinguishing the arc prevents crater cracks. A runoff tab or backstep technique at weld terminations ensures the crater is filled. D1.1 Clause 7.30 addresses the use and removal of weld tabs.
Inspector scenario: During VT on a Ligação de momento, you observe a linear Indicação along the weld centerline of a Solda de chanfro CJP. It is approximately 1/4 inch long. Under D1.1:2025 Table 8.1 item (1), this is a rejectable Defeito regardless of length. You reject the weld and initiate a Reparo per Clause 7.25. There is no measurement to take — if it is a crack, it fails.
Repair
D1.1:2025 Clause 7.25 governs repair of defective welds including cracks. The sequence: identify and mark the full extent of the crack (Ensaio por Partículas Magnéticas or dye Líquidos Penetrantes Ensaio helps define crack ends), then per Clause 7.25.1.4 remove the crack and sound metal 2 in [50 mm] beyond each confirmed crack tip by grinding or gouging. This 2-inch extension is mandatory — crack tips are often not visible and may extend further than they appear. Inspect the excavated cavity to confirm removal, then re-weld using an approved WPS with appropriate preheat. The repaired area is re-inspected by VT against Table 8.1 item (1).
For cold cracks, the repair WPS must address the root cause — typically by increasing preheat above the minimum or switching to a lower-hydrogen Eletrodo. Re-welding without addressing the hydrogen or restraint condition that caused the original crack invites recurrence.
Frequently Asked Questions
No. D1.1:2025 Table 8.1 item (1) states that any crack shall be unacceptable regardless of size or location. This applies to both statically loaded and cyclically loaded nontubular connections. There is no minimum crack length, no depth threshold, and no exception — a crack of any size in any location is a rejectable defect requiring repair.
Hot cracks form at elevated temperatures during solidification of the weld metal, typically caused by low-melting-point impurities (sulfur, phosphorus) segregating to grain boundaries as the weld cools. Cold cracks — also called hydrogen-induced cracking (HIC) or delayed cracking — form after the weld has cooled, sometimes hours or days later, driven by diffusible hydrogen, residual stress, and a susceptible microstructure. Hot cracks appear immediately after welding; cold cracks may not be visible during initial inspection.
D1.1:2025 Table 8.1 item (5) requires that visual inspection of welds in ASTM A514, A517, and A709 Grade HPS 100W steels be performed not less than 48 hours after weld completion. These high-strength, low-alloy steels are susceptible to delayed hydrogen-induced cracking, which can initiate and propagate after the weld has cooled to ambient temperature. Inspecting too early can miss cracks that have not yet formed or fully propagated.
Yes. D1.1:2025 Clause 7.25 permits repair of cracked welds. Per Clause 7.25.1.4, the crack and sound metal 2 in [50 mm] beyond each confirmed crack tip must be removed by grinding or gouging — not just the visible crack. The excavated cavity is inspected to confirm full removal, and the repair weld is made following an approved WPS. The repaired area must be re-inspected using the same acceptance criteria — visual inspection against Table 8.1 item (1). A repair weld on a cracked area must also wait the full 48-hour inspection window if the base metal is A514, A517, or HPS 100W.