Guide
What causes chloride stress corrosion cracking in stainless parts, and what grade or stress relief prevents it?
Chloride stress corrosion cracking is the sudden, branching cracking of a stainless steel part that happens only when three things meet at once: a susceptible alloy (above all the common 304 and 316 austenitic grades), a tensile stress in the metal, and a warm, wet environment carrying chlorides. Remove any one of the three and the cracking stops, which is why the fix is always a choice between changing the grade, lowering the stress, or keeping chlorides and heat off the surface.
By Saola Manufacturing engineering team · Published · Updated
The situation that brings most engineers to this question is specific. A 304 or 316 fitting, housing, sensor body or connector has been in warm, salty or chlorinated service for months, sometimes years, and it has started to weep or has split, with almost no visible general corrosion. Someone now has to decide whether the part was bad, the environment was worse than assumed, or the design asked the wrong grade to do the job. This guide shows how to recognize the failure, how to confirm it at the lab, which of the three conditions to attack first, and what to write on the drawing and RFQ so the replacement part does not crack the same way.
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How do you recognize chloride stress corrosion cracking on a stainless part?
Look for fine, tight cracks with little or no rust around them, often at a weld, a bend, a threaded or swaged section or a press fit, on a part that otherwise still looks clean. Under the microscope the cracks branch like tree roots and usually run through the grains rather than around them.
The Specialty Steel Industry of North America describes chloride stress corrosion cracks in stainless steel as branched and transgranular (SSINA, chloride stress corrosion cracking). Because the attack is concentrated in narrow cracks, the surrounding surface can stay bright, and that contrast is the main field clue. Pitting leaves visible pits; crevice corrosion leaves stained, attacked metal under a gasket or washer; general corrosion thins the whole surface. Stress corrosion cracking leaves the part looking serviceable until it leaks.
The location of the cracks is the second clue, because cracks follow stress. Typical sites on machined and fabricated parts are the toe of a weld, the outside of a bent or flared tube, a swaged or crimped ring under hoop stress, the root of a thread in a fitting that was tightened hard, and the bore of a housing with an interference-fit bushing. In 2015 the UK Health and Safety Executive warned that 316/316L pipe connectors in marine and coastal service had cracked in the swaged driver ring, the section under tensile hoop stress, and that some cracks were internal and found only by radiography (HSE Safety Alert ED 01-2015). A part that cracks along its most stressed feature and nowhere else is pointing at this mechanism.
What causes chloride stress corrosion cracking, ranked by how often each factor decides the outcome?
Temperature and chloride concentration at the metal surface decide most cases, followed by tensile stress, which is usually residual stress from welding, forming or assembly rather than the design load. Grade choice sets how much of each the part can tolerate.
- Temperature. SSINA notes that cracking is rare in fully immersed stainless steel below about 60 °C, but that severe evaporative conditions can crack parts well below that level (SSINA). Treat that figure as a screening line, not a guarantee. The British Stainless Steel Association warns that cracking can occur at 25 °C where chloride levels are very high, as on surfaces wetted by condensed swimming pool air (BSSA, stainless steel in swimming pool buildings).
- Chloride concentration where the metal is wet. The bulk water chemistry often looks harmless. SSINA notes that failures have been reported in environments with as little as 10 ppm chlorides, and explains that at wet and dry interfaces or on heat-rejecting surfaces a few ppm in the bulk can concentrate to hundreds of ppm. Drips, splash zones, condensate, evaporating cooling water and wet thermal insulation are the usual concentrators.
- Tensile stress, mostly residual. Welding shrinkage, cold forming, swaging, straightening, interference fits, hard-tightened threads and machining with dull tools all leave tension in the surface. Design loads are often low; it is the stress nobody wrote down that cracks the part.
- Oxygen and pH. SSINA notes that chlorides and dissolved oxygen act together, and that lower pH and higher stress also raise susceptibility. Aerated, slightly acidic chloride water is worse than the same water deaerated.
- Alloy composition. The standard austenitic grades sit at the worst point. SSINA identifies austenitic grades with about 8 to 10 wt% nickel as the most susceptible, which puts 304/304L and 316/316L squarely in the risk zone, while ferritic grades are very resistant and duplex grades fall between.
One cause is easy to miss on equipment: chloride-bearing thermal insulation. The ASTM C692 test method notes that insulation systems can act as collecting media, moving corrosive ions to heated stainless steel surfaces and concentrating them there as the water evaporates. ASTM C795 covers insulation for contact with austenitic stainless steel and requires it to pass the C692 stress corrosion test. Moving from 316 to a higher grade does nothing if the jacket keeps feeding salt water onto a hot surface.
| Condition in service | Effect on 304 / 316 cracking risk | First question to ask |
|---|---|---|
| Fully immersed, below about 60 °C | Low; cracking rare | Is there any evaporation, splash or hot spot? |
| Fully immersed, above about 60 °C | Elevated; rises with temperature and chloride | What is the chloride level and is the water aerated? |
| Wet/dry cycling, drips, condensate, heat-rejecting surface | High; chlorides concentrate far above bulk | Where does water evaporate on the part? |
| Warm surface under wet thermal insulation | High unless insulation qualified for stainless contact | Does the insulation meet ASTM C795? |
| Indoor pool hall, load-bearing part | High even near 25 °C (77 °F) | Is the part safety-critical? Then change grade |
| Welded, swaged, cold-formed or interference-fit section | Raises risk at every temperature above | Can the residual stress be removed or avoided? |
How do you confirm it is chloride stress corrosion cracking and not fatigue or overload?
Section the part through a crack and look at it under a metallurgical microscope: branched, transgranular cracks starting at the wetted surface, with chlorides found in the deposits, confirm the mechanism. Fatigue cracks are usually single and unbranched, and overload fails at once rather than over months.
Work through the checks in order, cheapest first. Keep the failed part dry and unwashed until it reaches the lab, because cleaning destroys the chloride evidence on the fracture face.
- Map the cracks. Note whether they sit at welds, bends, threads, swaged sections or fits, and whether they face the wet side. Record service temperature and how the part was wetted.
- Find all of them. Liquid penetrant testing per ASTM E165/E165M shows surface cracks on the failed part and its siblings. The HSE alert above is a reminder that penetrant finds only surface-breaking cracks, so a clean penetrant result on a critical part is not proof of soundness.
- Section and etch. A metallographic cross-section shows whether the cracks are branched and transgranular (typical of chloride cracking in annealed austenitic grades) or intergranular, which points to a sensitized microstructure from welding or heat treatment and calls for a different fix.
- Analyze the deposits. Energy-dispersive X-ray analysis in a scanning electron microscope on the crack faces or surface deposits shows whether chlorine is present.
- Check the material. Compare the mill certificate and a chemistry check against the grade on the drawing. A substituted grade, or a free-machining grade where the drawing called for 304 or 316, changes the conclusion.
Accelerated laboratory tests rank alloys but do not predict service life. The boiling magnesium chloride practice in ASTM G36 is deliberately severe; the standard warns that materials which normally give acceptable resistance in hot chloride service may crack in the test, and that the solution can also pit many stainless alloys, so failed specimens need careful examination before the cause is called. U-bend specimens per ASTM G30 are a common way to load samples for these comparisons. Use them to choose between candidate grades, not to qualify a part.
Which grade change or stress relief prevents chloride stress corrosion cracking?
Changing the grade is the most reliable fix: a duplex grade such as 2205, a 6Mo super austenitic grade, or a ferritic grade such as 444 removes most of the risk in warm chloride water. Stress relief, shot peening and design changes lower the risk on 304 and 316 but do not make them immune.
SSINA states that no stainless steel grade is totally immune, but that resistance varies widely by family (SSINA). The boiling salt results it publishes, summarized in the table below, show the pattern: the standard austenitic grades crack in every solution tested, duplex and high-alloy austenitic grades survive the sodium chloride test, and ferritic grades survive all three. Each move away from 304 and 316 has a cost. Duplex grades are stronger and harder to machine and form. The 6Mo grades are expensive and not always available as bar. Ferritic grades such as 444 resist cracking but are less tough and less weldable in heavy sections. Pick the lowest grade that removes the risk for your actual temperature and wetting pattern.
Stress relief is the fix when the grade must stay. It is a trade-off on austenitic stainless, because the temperatures that remove the most residual stress overlap the range where standard-carbon grades precipitate chromium carbides and lose corrosion resistance at the grain boundaries, as the 316 vs 316L guide explains. Practical options are, from most to least effective: a full solution anneal and quench after welding and forming; a stress relief on a low-carbon L grade or a stabilized grade such as 321 or 347 chosen for that purpose; and shot peening of the stressed surface, commonly specified per SAE AMS2430, which puts the surface in compression. The heat treatment cycle should be chosen by a materials engineer for the grade and section, not copied from a carbon steel note.
Design and environment changes are often cheaper than either. Remove crevices and water traps, make parts free-draining, keep insulation dry and qualified, avoid interference fits and swaged joints on stainless in warm chloride service, and set a tightening torque for threaded fittings instead of “tighten until it stops leaking.” In a closed water loop, oxygen control is a lever too: SSINA states that with dissolved oxygen held at 0.01 to 0.1 ppm, solutions with low to moderate chloride levels are not likely to crack 304L and 316L.
While replacements are on order, contain the risk on the parts still in service. Pull the siblings of the failed part that see the same temperature and wetting, starting with the hottest and wettest locations, and inspect them; on safety-critical parts add volumetric inspection such as radiography, because penetrant misses internal cracks. In the HSE alert, all the cracked connectors found had been unpainted, though HSE cautioned that painting may not fully prevent the problem, so treat a coating as a temporary barrier, not a cure.
| Grade (UNS) | Family | Boiling 26% NaCl U-bend | Boiling 42% MgCl2 U-bend | Trade-off to check |
|---|---|---|---|---|
| 304L (S30403) | Austenitic | Cracked | Cracked | Baseline; very susceptible |
| 316L (S31603) | Austenitic | Cracked | Cracked | Better pitting resistance than 304L, not better cracking resistance |
| 904L (N08904) | High-alloy austenitic | No cracking | Cracked | Cost and bar availability |
| 6Mo, e.g. N08367 | Super austenitic | No cracking | Cracked | Cost and bar availability |
| 2205 (S32205 / S31803) | Duplex | No cracking | Cracked | Harder to machine; weld procedure must control ferrite balance |
| 2507 (S32750) | Super duplex | No cracking | Cracked | Cost; harder still to machine |
| 444 (S44400) | Ferritic | No cracking | No cracking | Lower toughness; limited in heavy welded sections |
What should the drawing and RFQ say so a replacement part does not crack the same way?
State the service environment, name the grade by UNS number and product specification, and name any stress relief, anneal or peening step together with where in the routing it happens. A note that says only “316 stainless” leaves every one of those choices to the supplier.
- Service environment. Write the maximum metal temperature, the chloride source (seawater, pool air, chlorinated process water, de-icing salt, insulation) and whether the surface dries out. The supplier cannot flag a grade risk it does not know about.
- Grade. “Material: UNS S31603 bar per ASTM A276” or “UNS S32205 plate per ASTM A240”, with the product specification matched to the stock form, not “duplex” or “316”. Add “no substitution without written approval” so a free-machining or lower grade does not slip in.
- Stress control. Name the step and its sequence, for example “solution anneal after welding and forming, before final machining” or “shot peen weld toes per SAE AMS2430”. If the part must not be swaged, press-fit or straightened, say so.
- Surface condition. Call out deburring and, where it applies, passivation per ASTM A967 or A380 as covered in the passivation guide. Passivation helps against pitting and rust staining; it does not stop stress corrosion cracking on its own.
- Assembly. Give a torque for threaded fittings and forbid interference fits on the wetted stainless body unless the design was checked for them.
- Verification. Ask for mill certificates, and for welded or critical parts, liquid penetrant inspection per ASTM E165 of the stressed areas.
Who does what when a stainless part for chloride service is ordered through Saola?
Machining runs at our lead CNC plant in Vietnam; annealing, stress relief, peening and finishing go to partner plants we manage. The quote states the production site and country of origin for each step.
Turned and milled stainless parts, including bodies, fittings and housings, are cut on the CNC turning and CNC milling equipment at our lead CNC plant, T.K Viet Nam Precision Company Limited. Stainless bar is not on the published bar lists today, so name the exact grade on the RFQ and ask before assuming it can be sourced with certificates. Passivation, stress relief, solution annealing and shot peening are not on the fixed surface finishing menu either; when the drawing calls for them, they are arranged with a partner plant we manage, which is not named, and the quote says where each step runs. Material certification is available on request, and ISO 9001 certification is in progress, not held. The grade decision stays with the design owner; putting the temperature and chloride source on the RFQ lets the manufacturability note that comes with the quote point out a grade or stress step worth a second look. Send the drawing and the service notes through the quote form.
Frequently asked
Is 316 more resistant to stress corrosion cracking than 304?
Not in any useful way. The molybdenum in 316 improves pitting and crevice resistance, but SSINA lists both 304/304L and 316/316L as very susceptible to chloride stress corrosion cracking. If cracking is the failure, moving from 304 to 316 is not the fix.
Does stress corrosion cracking happen at room temperature?
It is uncommon in fully immersed parts at room temperature, but it does happen where chlorides concentrate. The BSSA notes cracking of standard grades in indoor pool halls, where condensate carries high chloride levels, which is why load-bearing parts there need grades with proven resistance.
Can a cracked stainless fitting be weld-repaired?
Usually not reliably. The surrounding metal often holds more cracks than penetrant shows, and the repair weld adds fresh residual stress in the same environment. Replace the part and change at least one of the three conditions: grade, stress or environment.
Does passivation or electropolishing prevent stress corrosion cracking?
No. Both improve the passive film and resistance to pitting and staining, which can help indirectly by removing initiation sites, but neither removes tensile stress or changes the alloy. Treat them as surface hygiene, not as the fix.
Is 17-4 PH stainless a safe choice for chloride service?
It depends on the aged condition. 17-4 PH is most prone to stress corrosion cracking at its highest strength and more resistant in the overaged conditions, as the 17-4 PH condition guide explains. Specify the condition, not just the alloy.
Sources
- Chloride Stress Corrosion Cracking, Specialty Steel Industry of North America, accessed October 2026
- Stainless steel in swimming pool buildings, British Stainless Steel Association, accessed October 2026
- Safety Alert ED 01-2015: External chloride stress corrosion cracking of stainless steel pipe connectors, UK Health and Safety Executive, 2015 (refers to HSE Research Report RR902, 2011)
- ASTM G36-24, Standard Practice for Evaluating Stress-Corrosion-Cracking Resistance of Metals and Alloys in a Boiling Magnesium Chloride Solution (scope and significance), ASTM International, 2024
- ASTM G30-22, Standard Practice for Making and Using U-Bend Stress-Corrosion Test Specimens (scope), ASTM International, 2022
- ASTM C795-08(2023), Standard Specification for Thermal Insulation for Use in Contact with Austenitic Stainless Steel (scope), ASTM International, 2023
- ASTM C692-13(2023), Standard Test Method for Evaluating the Influence of Thermal Insulations on External Stress Corrosion Cracking Tendency of Austenitic Stainless Steel (scope and significance), ASTM International, 2023
- ASTM E165/E165M-23, Standard Practice for Liquid Penetrant Testing for General Industry (scope), ASTM International, 2023
- ASTM A240/A240M-24a, Standard Specification for Chromium and Chromium-Nickel Stainless Steel Plate, Sheet, and Strip for Pressure Vessels and for General Applications (scope), ASTM International, 2024
- SAE AMS2430U, Shot Peening, SAE International, 2018