12Cr-Mo martensitic stainless steel · Open-die forgings
AMS 5614C forgings (UNS S41025, 12Cr–0.5Mo)
Seamless rolled rings, shafts, discs, hollow bars, turbine blade blanks and valve parts, forged to drawing in Jiangyin, China.
AMS 5614C · AMS 5614 · UNS S41025 · 12.5Cr – 0.5Mo · Type 410 modified with molybdenum · AISI 410 Mod · JIS SUS410J1 (near) · GB 1Cr12Mo / 12Cr12Mo (near) · turbine blade steel
Summary
AMS 5614C is revision C of SAE AMS 5614, the material specification for a 12% chromium martensitic corrosion- and heat-resistant steel containing about 0.5% molybdenum, supplied as bars, forgings, forging stock and rings, and designated UNS S41025. It is Type 410 with molybdenum added and the residual elements held to tighter limits. The molybdenum raises tempering resistance and creep strength and improves behaviour in wet steam. The grade has been used for steam turbine blading, blade roots and valve spindles for several decades.
Jiangyin Jiangnan Metal Co., Ltd. forges AMS 5614C / UNS S41025 to customer drawings as seamless rolled rings from 200 to 2,500 mm outside diameter, forged shafts to 8 m, discs to 1,800 mm, hollow and trepanned bar, blocks, turbine wheels and blade blanks, and valve spindles, stems, bodies and bonnets, at single-piece weights up to 8,000 kg. Material is melted by EAF + LF + VOD with ESR remelting on request, annealed or hardened and tempered in-house, ultrasonically tested to EN 10228-3, SEP 1921 or ASTM A388, and certified to EN 10204 3.1 as standard or 3.2 with a third-party witness. Written quotations are issued within 24 hours from sales@steelforgepieces.com or 0086-189-2135-9659.
Chemistry as listed in the AMS 5614 grade band. Size and weight figures are the tested envelopes for this grade on our own presses and ring mills at Jiangyin, Jiangsu, China.
What AMS 5614C forgings can you buy?
UNS S41025 is a made-to-order grade. The heat is bought against your specification, so the drawing and the required condition are needed at the first enquiry. Jiangyin Jiangnan Metal produces it by four routes, chosen by geometry and order size. Open-die forging covers long shafts, blocks and heavy discs. Seamless ring rolling produces rings from 200 mm to 2,500 mm outside diameter, the usual route for diaphragm and casing rings. Closed-die forging handles repeat-volume parts such as blade blanks and valve trim. Upset forging is used for short, large-section hubs and flanges. Trepanning replaces drilling on hollow parts above about 200 mm bore, and the removed core is kept for test coupons.
Near-net dies typically remove 30–50% of the rough machining on profiled parts. This is worth more on AMS 5614C than on carbon steel, because the material costs several times as much per kilogram and the machining allowance is paid for twice, once as metal and once as cutting time.
What is AMS 5614C / UNS S41025 steel?
Plain Type 410 is the least expensive hardenable stainless steel and performs well enough at room temperature. Under load in steam at 500 °C it has two weaknesses. It continues to temper in service and loses strength, and the condensate pits it. AMS 5614C addresses both by adding 0.40–0.60% molybdenum and by holding the residual elements that embrittle 12Cr steels to tight ceilings.
Three properties matter in service:
- Tempering resistance. Molybdenum slows the coarsening of carbides, so the steel holds its hardness at temperature instead of softening over thousands of hours of service. This is what allows a blade to keep its properties over a design life measured in decades.
- Creep and fatigue strength in wet steam. The usual application is a low-pressure turbine blade, which sees high-cycle fatigue, water droplet erosion and corrosion together. The 12Cr matrix provides the fatigue strength and the molybdenum provides the resistance to condensate pitting that would otherwise start a crack.
- Full hardenability in heavy section. With 12% chromium the steel air-hardens, and even a 300 mm section transforms to martensite. This gives uniform properties through the section, but it also means a forging left to cool unattended will crack if it is not tempered promptly.
The steel is ferromagnetic in every condition because the matrix is martensite. Its pitting resistance equivalent number is around 13 to 14, which places it in steam, fresh water and mild atmospheres rather than seawater or chloride service.
Specification and chemistry are different documents
UNS S41025 is a composition number. AMS 5614C also fixes melting practice, cleanliness and quality level, delivery condition, testing and certification. Quote both on the order, as AMS 5614C (UNS S41025). If your drawing invokes a different revision letter, state it. Revision changes can affect chemistry limits and test requirements, and we buy raw material to the revision you cite.
What are the equivalents of AMS 5614C?
This steel appears under several names. They describe the same 12Cr–Mo family and we accept orders under any of them, but their limits are not interchangeable. The molybdenum-free 410 grades in particular are a different material for this application.
| Body / region | Designation | Relationship and notes |
|---|---|---|
| USA · SAE aerospace | AMS 5614 / AMS 5614C | The governing specification for bars, forgings, forging stock and rings in this chemistry. Cite the revision letter. |
| USA · UNS | UNS S41025 | The unambiguous composition number. Put it on the drawing next to the AMS number. |
| USA · descriptive | AISI 410 Mod, 12Cr–Mo, 410 + Mo | Trade descriptions of the same molybdenum-bearing 410 variant. Not a specification; do not order to these alone. |
| USA · SAE, adjacent | AMS 5613 (UNS S41000) | Plain Type 410, no molybdenum. Lower cost, lower tempering and creep resistance. Not an equivalent. |
| USA · SAE, adjacent | AMS 5616 (UNS S41800, Greek Ascoloy) | 13Cr–2Ni–3W turbine blading steel. Higher strength and higher service temperature at a higher price. Not a direct substitute. |
| Japan · JIS | SUS410J1 | Nearest stocked JIS grade. 12Cr martensitic with molybdenum, used for turbine blading. The carbon band differs, so verify before cross-certifying. |
| China · GB | 1Cr12Mo / 12Cr12Mo | Chinese turbine blade steel of the same type, covered by GB/T 1221 and the turbine blade steel standard GB/T 8732. Chemistry is close but not identical. |
| Europe · EN | X12Cr13 (1.4006), X20Cr13 (1.4021) | The stocked European 12Cr martensitic grades, with no specified molybdenum. Use only where the drawing allows plain 13Cr. |
| Europe · EN, adjacent | X20CrMoV11-1 (1.4922) | Creep-resistant 12Cr with roughly double the carbon, double the molybdenum and added vanadium. A different grade, intended for hotter steam. |
| Product-form standards | ASTM A276, A479, A182 F6a, A473 | Commercial-grade product standards for 410-family bars, forgings and flanges. They do not carry the AMS trace-element controls. |
Cross-references are for enquiry purposes. Matching a name here does not certify equivalence. Chemistry bands, trace element ceilings and test requirements differ. Always reference the standard revision in force at the contract date. Table compiled by Jiangyin Jiangnan Metal Co., Ltd.
Designation lookup
Enter a designation such as AMS 5614, S41025, 410, SUS410J1, 1Cr12Mo or Greek Ascoloy.
A match here is a cross-reference, not a certificate of equivalence. Chemistry bands differ. See Table 1 and Table 2.
What is the chemical composition of AMS 5614C?
This is the band we buy raw material against unless a drawing calls for something tighter. Chromium provides the corrosion resistance, carbon sets the attainable hardness, molybdenum is what separates this grade from plain 410, and the trace element ceilings at the foot of the table are what allow the steel to last in a steam path.
| Element | Min | Max | Why it is controlled |
|---|---|---|---|
| Carbon (C) | 0.07 | 0.12 | Sets martensite hardness. Held low enough to keep chromium in solution and the steel weldable and tough |
| Manganese (Mn) | 0.30 | 0.60 | Deoxidiser and sulphur getter; a narrow band keeps hardenability consistent heat to heat |
| Silicon (Si) | – | 0.35 | Deoxidiser. Capped because silicon promotes delta ferrite and temper embrittlement |
| Phosphorus (P) | – | 0.040 | Residual. Segregates to prior-austenite grain boundaries and drives temper embrittlement |
| Sulphur (S) | – | 0.030 | Residual. Manganese sulphide stringers start pits and cut transverse toughness |
| Chromium (Cr) | 11.50 | 12.50 | The passive film. Below about 10.5% the steel is not stainless at all |
| Molybdenum (Mo) | 0.40 | 0.60 | The addition that distinguishes this grade. Tempering resistance, creep strength, pitting resistance in condensate |
| Nickel (Ni) | – | 0.60 | Austenite stabiliser that suppresses delta ferrite; capped so the martensite finish stays above room temperature |
| Copper (Cu) | – | 0.50 | Residual from scrap. High copper causes hot shortness during forging |
| Aluminium (Al) | – | 0.05 | Deoxidation residual. Capped to limit alumina inclusions that fail ultrasonic examination |
| Tin (Sn) | – | 0.05 | Tramp element. With phosphorus and antimony it is a primary cause of temper embrittlement |
| Nitrogen (N) | – | 0.08 | Raises strength but coarsens nitrides and reduces toughness above the ceiling |
| Iron (Fe) | Balance | Matrix | |
Source: AMS 5614C grade band as published by Jiangyin Jiangnan Metal Co., Ltd. Every heat ships with a ladle analysis on the mill certificate; product analysis on the finished forging is added on request. Where your purchase order states a tighter band, the order governs.
Trace element limits
Most 12Cr datasheets stop at chromium and molybdenum. The 0.05% ceilings on tin and aluminium and the 0.08% ceiling on nitrogen are what separate turbine quality AMS 5614C from a commercial 410 bar that happens to contain molybdenum. Tin and phosphorus segregate to prior-austenite grain boundaries during slow cooling and raise the ductile-to-brittle transition temperature by tens of degrees. A commercial bar can meet every chromium, carbon and hardness requirement on a drawing and still be unsuitable for a blade root.
Melting route
The standard route is EAF + LF + VOD: electric arc melting, ladle refining, then vacuum oxygen decarburisation to remove carbon and gases while retaining the chromium. ESR remelting is added where the specification calls for consumable electrode quality, tighter cleanliness or higher transverse properties in heavy sections. State which route your drawing requires at enquiry stage, because it affects both price and mill lead time.
| Element | AMS 5614C S41025 | AMS 5613 / Type 410 S41000 | Type 416 S41600 | Greek Ascoloy S41800 |
|---|---|---|---|---|
| Carbon | 0.07–0.12 | 0.08–0.15 | 0.15 | 0.15–0.20 |
| Chromium | 11.50–12.50 | 11.50–13.50 | 12.00–14.00 | 12.00–14.00 |
| Molybdenum | 0.40–0.60 | not specified | 0.60 (optional) | not specified |
| Nickel | 0.60 | 0.75 | – | 1.80–2.20 |
| Tungsten | – | – | – | 2.50–3.50 |
| Sulphur | 0.030 | 0.030 | 0.15 min | 0.030 |
| Trace controls | Al, Sn, N, Cu capped | none | none | per specification |
| Typical duty | Turbine blading, valve spindles, hot steam parts | General hardenable stainless | Free-machining parts only | High-strength blading, hotter service |
Values are the nominal grade bands used for comparison. Type 416 is included because it is sometimes offered as a free-machining substitute. Its sulphur addition makes it unsuitable for any part exposed to steam, condensate or fatigue loading.
What are the mechanical properties of AMS 5614C?
The tempering temperature controls the delivered properties. The hardening step is the same in every case; the temper decides whether the part ends up hard and strong or softer and tougher. A higher tempering temperature gives lower strength, higher elongation, higher impact energy and better resistance to stress-corrosion cracking.
Annealed condition, as normally shipped for machining
| Property | Typical value | Note |
|---|---|---|
| Anneal | 840–870 °C, slow furnace cool | Cool at 25 °C/h or slower to 600 °C, then air |
| Tensile strength | ≤ 690 MPa (100 ksi) | Soft enough for deep machining and cold straightening |
| Yield strength, 0.2% | ≈ 380–450 MPa | Indicative |
| Elongation | ≥ 20% | 4D or 2 in |
| Hardness | ≤ 235 HB (≈ 22 HRC) | This is a maximum, not a target |
Hardened and tempered: strength against tempering temperature
The table below is the indicative production band for AMS 5614C forgings in sections up to about 200 mm, hardened from 950–1010 °C and tempered for a minimum of two hours. Use it to choose a tempering temperature. It is not a set of specification minima.
| Temper | Tensile | Yield 0.2% | Elong. | RA | Hardness | Charpy V, RT |
|---|---|---|---|---|---|---|
| 620 °C | 900–1000 MPa · 131–145 ksi | 750–850 MPa | 15% | 50% | 28–32 HRC | ≈ 40 J |
| 660 °C | 830–930 MPa · 120–135 ksi | 690–780 MPa | 17% | 55% | 25–28 HRC | ≈ 55 J |
| 700 °C | 760–860 MPa · 110–125 ksi | 620–700 MPa | 18% | 60% | 22–26 HRC | ≈ 70 J |
| 740 °C | 690–790 MPa · 100–115 ksi | 550–620 MPa | 20% | 62% | 18–22 HRC | ≈ 90 J |
| 400–550 °C | Do not use this range. Hardness stays high and Charpy energy collapses; see the temper embrittlement note below | |||||
Indicative bands from Jiangyin Jiangnan Metal production experience on AMS 5614C / UNS S41025 forgings, longitudinal tests, sections to 200 mm. These are not acceptance values. The values that must appear on your certificate are those in the AMS revision, drawing or purchase specification you order to. Ask us to confirm them in writing before the drawing is released. Heavy sections, transverse test direction and sub-zero impact requirements all reduce the values that can be relied on.
Transverse properties in heavy sections
Above roughly 150 mm section, state whether tensile and impact tests are longitudinal or transverse. Transverse elongation and impact energy in a forging typically run 20–40% below longitudinal, because inclusions and grain flow are aligned with the forging axis. A certificate can pass or fail on that one word, and it is the most common source of dispute on turbine and valve forgings.
Tempering dial
Drag from 400 °C to 760 °C to see strength trade against toughness. The embrittlement trough is included in the range.
Indicative values for hardened AMS 5614C, sections to 200 mm, longitudinal. Qualify on coupons from the same heat before releasing production parts.
How is AMS 5614C heat treated?
Four operations, of which two are compulsory and two are used where required. Section thickness sets every hold time. Allow roughly 30 minutes per 25 mm at temperature, with a one hour minimum.
1. Annealing
Full anneal at 840–870 °C, then furnace cool at 25 °C per hour or slower to 600 °C before air cooling. This gives ferrite plus spheroidised carbides at 235 HB maximum, soft enough for deep machining. A subcritical anneal at 730–790 °C followed by air cooling is quicker and sufficient when the part only needs stress relieving between machining passes.
2. Hardening
Austenitise at 950–1010 °C and quench in oil for heavy sections, or in forced or still air for thin ones. Because the steel air-hardens, air quenching still gives a fully martensitic structure and produces much less distortion than oil, so it is preferred for blades, thin rings and parts with abrupt section changes. Soaking above about 1030 °C coarsens the grain and dissolves enough carbon to leave retained austenite. Soaking below 950 °C leaves undissolved carbides and the part will not reach strength.
3. Tempering
Temper immediately after the quench, for at least two hours at temperature, then cool in air. Do not leave hardened parts overnight before tempering. Fresh martensite in a 12Cr steel cracks under its own residual stress, particularly at section changes and drilled holes.
Do not temper between 400 and 550 °C
Never temper or stress-relieve AMS 5614C between about 400 °C and 550 °C, and do not let a heavy forging cool slowly through that band after tempering. Fine carbides precipitate on the martensite lath boundaries and tramp elements segregate to the prior-austenite grain boundaries. Hardness barely moves, so a hardness check will not detect it. The damage appears as a large drop in Charpy energy, or as a brittle fracture in service. Temper above 620 °C, and on sections above about 150 mm accelerate the cool from the tempering temperature with forced air.
4. Stress relief after machining
Where heavy machining follows tempering, stress-relieve at 600–650 °C, always at least 25–30 °C below the last tempering temperature, so the mechanical properties on the certificate are not disturbed.
| Operation or point | Temperature | Practice |
|---|---|---|
| Forging range | 1150–1200 °C start | Finish above 900 °C; reheat rather than finish cold |
| Full anneal | 840–870 °C | Furnace cool ≤ 25 °C/h to 600 °C, then air |
| Subcritical anneal | 730–790 °C | Air cool |
| Hardening | 950–1010 °C | 30 min per 25 mm; oil or air quench |
| Tempering | 620–760 °C | 2 h minimum, air cool; avoid 400–550 °C |
| Stress relief | 600–650 °C | At least 25–30 °C below the temper |
| Ac1 (approx.) | ≈ 800 °C | Lower critical point; hard ceiling on tempering |
| Ac3 (approx.) | ≈ 870 °C | Fully austenitic above this |
| Ms (approx.) | ≈ 320 °C | Martensite start; transformation completes near room temperature |
Approximate values for the AMS 5614C chemistry band; exact critical points shift with the actual heat analysis and should be confirmed by dilatometry where a specification demands it. Compiled by Jiangyin Jiangnan Metal Co., Ltd.
ESR on request
Heat number traced
Finish > 900 °C
Reduction ≥ 4:1
Slow cool
Structure reset
Annealed
UT after
30 min per 25 mm
Oil or air quench
2 h minimum
Air cool
UT EN 10228-3
PT / MT surface
3.2 on request
Marked and packed
Heat-treatment recipe generator
Select a target hardness or strength and a section thickness for a cycle you can pass to your heat treatment shop.
Cycles follow normal practice for 12Cr–Mo martensitic steel. Qualify on coupons from the same heat, and let the specification on your order override anything here.
What are the physical properties of AMS 5614C?
| Property | Value | Condition / note |
|---|---|---|
| Density | 7.70 g/cm³ (0.278 lb/in³) | Room temperature; used by the weight calculator below |
| Modulus of elasticity | 200 GPa (29 × 10³ ksi) | Tension, room temperature; ≈ 175 GPa at 400 °C |
| Thermal conductivity | ≈ 24.9 W/m·K | At 100 °C; ≈ 28.7 W/m·K at 500 °C |
| Specific heat | ≈ 460 J/kg·K | 0–100 °C |
| Electrical resistivity | ≈ 0.57 µΩ·m | 20 °C |
| Mean thermal expansion | 9.9 × 10⁻⁶/°C | 0–100 °C; ≈ 11.4 × 10⁻⁶/°C over 0–500 °C |
| Magnetic response | Ferromagnetic | Martensitic in every condition; magnetic particle inspection is available |
| Scaling limit in air | ≈ 650 °C continuous | Oxidation limit, not a strength limit |
Representative published values for 12Cr martensitic stainless steel, compiled by Jiangyin Jiangnan Metal Co., Ltd. for design guidance. Where a calculation is safety-critical, use values measured on the delivered heat.
How corrosion resistant is AMS 5614C, and how hot can it run?
General corrosion resistance is that of a 12% chromium martensitic stainless steel, improved by the molybdenum. It is better than plain Type 410 in condensate and wet steam, much better than any low-alloy steel, and well below the austenitic and duplex grades. The pitting resistance equivalent number, PREN = %Cr + 3.3 × %Mo, is roughly 13.6 for mid-band chemistry. Continuous seawater immersion requires about 32, which marks the limit of what this grade can do.
Suitable environments
Wet and dry steam, condensate and boiler feedwater; fresh water; atmospheric and mild industrial exposure; weak organic acids; most hydrocarbons and refinery streams; food and pharmaceutical process equipment where strength matters more than pitting.
Unsuitable environments
Seawater and high-chloride service; reducing acids such as hydrochloric and dilute sulphuric; hot caustic; anything requiring the part to be non-magnetic; sustained load above roughly 540 °C; unqualified sour service.
Corrosion resistance also depends on heat treatment. Material tempered in the 400–550 °C range, or left as quenched, precipitates chromium carbides that locally deplete the matrix and lower pitting resistance. The best corrosion performance comes from the hardened and tempered condition above 620 °C, with a clean, descaled and passivated surface. A forging that has been ground but not pickled will pit at the embedded iron before the base metal is attacked.
Service temperature limits
Two limits apply, and the lower one governs.
- Do not run the part within 30 °C of its own tempering temperature. Service inside that margin continues the tempering reaction and the part softens permanently. Material tempered at 620 °C is limited to about 590 °C on this basis alone.
- Creep governs above roughly 480 °C. For stressed rotating or pressure-retaining parts the practical design limit is 480–540 °C, which suits intermediate and low-pressure steam paths rather than the hottest high-pressure stages.
Oxidation is not the limiting factor. The steel resists scaling in air to about 650 °C. For sustained duty above 540 °C, move to a creep-resistant 9–12Cr grade, to Inconel 718, or to another nickel alloy.
Sour service: do not assume AMS 5614C is approved
Martensitic 12Cr steels appear in ISO 15156 / NACE MR0175 only within specific hardness, heat-treatment condition and environmental limits, and AMS 5614C is not a pre-qualified route in the way that double-aged 17-4PH is. Check the current edition of ISO 15156-2 or 15156-3 against your actual H₂S partial pressure, chloride content, pH and temperature. We will supply with a contractual hardness cap and full hardness mapping. We will not issue a compliance statement based on a hardness cap alone.
AMS 5614C against 410, 416, 431, Greek Ascoloy and 17-4PH
Type 410 costs less and is widely stocked. Greek Ascoloy is stronger and runs hotter. 17-4PH is stronger and more corrosion resistant but is limited to lower temperatures. AMS 5614C holds its properties in hot wet steam at a moderate price. Where a drawing calls for AMS 5614C and 410 is proposed to save money, the questions to answer are what temperature the part runs at and for how long.
| Property | AMS 5614C S41025 | Type 410 S41000 | Type 416 S41600 | Type 431 S43100 | Greek Ascoloy S41800 | 17-4PH S17400 |
|---|---|---|---|---|---|---|
| Chromium % | 11.5–12.5 | 11.5–13.5 | 12–14 | 15–17 | 12–14 | 15–17.5 |
| Molybdenum % | 0.4–0.6 | none | optional | none | none (3W) | not specified |
| Typical UTS | 760–1000 MPa | 690–900 MPa | 650–850 MPa | 860–1100 MPa | 900–1200 MPa | 930–1310 MPa |
| Tempering resistance | Good | Moderate | Moderate | Moderate | Very good | Not applicable |
| PREN (approx.) | 13.6 | 12.5 | 13 | 16 | 13 | 16–17 |
| Practical max service | 480–540 °C | ≈ 480 °C | ≈ 400 °C | ≈ 400 °C | ≈ 590 °C | ≈ 300 °C |
| Weldability | Preheat + PWHT | Preheat + PWHT | Not weldable | Difficult | Preheat + PWHT | Good |
| Machinability | Fair | Fair | Excellent | Fair | Fair | Good in Condition A |
| Relative cost | 1.3× | 1× baseline | 1.1× | 1.5× | 2.5× | 2× |
| Best at | Steam blading, valve spindles, hot steam parts | General hardenable stainless | Free-machining, dry service only | Higher-strength shafting | Hot, highly stressed blading | Strong, corrosion-resistant, cooler parts |
Nominal comparison values compiled by Jiangyin Jiangnan Metal Co., Ltd. from published grade data. Cost multiples are indicative of forged bar in comparable quantities and move with the nickel and molybdenum markets.
Selection checks
- How hot does it run, and for how long? Above about 450 °C for a design life in tens of thousands of hours, molybdenum is needed and plain 410 will lose hardness.
- Is there wet steam or condensate? Droplet erosion and condensate pitting are the usual causes of blade failure. AMS 5614C is specified for that duty. Type 410 and 416 are not.
- Is there a Charpy acceptance value on the drawing? If so, the trace element ceilings in AMS 5614C are what deliver it, and a commercial 410 bar containing molybdenum is not a substitute even if its chromium and molybdenum fall inside the band.
Substitution check
Select what you specify now and what you are trying to gain.
Guidance only. A substitution is final when the design authority for the equipment has signed it off.
How is AMS 5614C forged, welded and machined?
Forging
Soak and forge from 1150–1200 °C, with a workable envelope of roughly 900–1200 °C. Finish above 900 °C. Below that the steel work-hardens quickly and the risk of surface cracking rises, so reheat rather than finish cold. Aim for a forging reduction of at least 4:1 from the ingot or billet to break down the cast structure and develop grain flow along the principal axis. Heat the charge slowly through 600–850 °C. A cold 12Cr ingot placed straight into a hot furnace can crack from thermal stress.
Because the steel air-hardens, a forging left to cool in still air reaches room temperature as untempered martensite. Transfer it directly to an annealing or tempering furnace, or hold it above 550 °C until the next operation. This is the most common cause of cracked 12Cr forgings.
Welding
Weldable, provided normal martensitic steel practice is followed:
- Preheat to 200–300 °C and hold the interpass temperature in the same band.
- Use a matching 12Cr filler where the joint must have parent metal strength and corrosion resistance, or an austenitic (309/310) or nickel-base filler where a softer weld metal is acceptable and post-weld heat treatment is not possible.
- Post-weld temper at 700–760 °C, and do not let the joint fall to room temperature first. Cool to about 100–150 °C to complete transformation, then transfer directly to the tempering furnace.
- Use low-hydrogen consumables, dried and stored correctly. Hard martensite and hydrogen together produce delayed cracking, sometimes days after welding.
Machining
Machine in the annealed condition wherever the tolerance stack allows. At 235 HB it cuts like a tough medium-carbon alloy steel. At 32 HRC tool life falls away quickly. Use positive rake, rigid setups, sharp edges and flood coolant, and do not let a tool dwell. 12Cr steels work-harden under a rubbing edge and glaze the surface, and the next pass then rubs instead of cutting. Chips are stringy, so pecking and chip-breaking geometry are important on deep holes.
Machining starting values
Enter the condition, operation and tooling for a starting cutting speed and feed.
Starting values for a rigid setup with flood coolant. Adjust for machine stiffness, tool overhang and the finish you need.
How does AMS 5614C fail, and how do you prevent it?
Temper embrittlement
Cause: tempering in, or cooling slowly through, 400–550 °C, with tin, phosphorus and antimony segregating to grain boundaries. Prevention: temper above 620 °C, accelerate the cool on heavy sections, and hold the trace-element ceilings in Table 2 when buying the heat.
Delayed cracking after quench
Cause: a hardened forging left untempered overnight. Residual stress in fresh martensite concentrates at a section change or a drilled hole. Prevention: temper immediately, or hold above 550 °C until the furnace is free. Do not leave a heavy 12Cr forging to air-cool unattended.
Hydrogen embrittlement
Cause: pickling, electroplating, cathodic over-protection or wet welding consumables charging hydrogen into hard martensite. Prevention: bake 4–24 h at 190–220 °C after plating or pickling, use dried low-hydrogen consumables, and prefer the softer tempers for plated parts.
Delta ferrite stringers
Cause: chromium at the top of the band with carbon and nickel at the bottom, leaving free ferrite that survives austenitising. Prevention: buy the heat to a balanced chromium equivalent, check the microstructure, and set a ferrite ceiling on the order where transverse toughness is critical.
Condensate pitting and corrosion fatigue
Cause: chlorides concentrating in the wet steam phase, pitting the surface, and a pit becoming a fatigue initiation site. Prevention: temper above 620 °C, passivate, hold surface finish on aerofoils and roots, and control steam chemistry.
Forging bursts and laps
Cause: finishing below 900 °C, excessive reduction per blow, or a cold ingot heated too fast. Prevention: control the finish temperature, work in incremental passes, soak slowly through 600–850 °C, and accept the part on ultrasonic examination to EN 10228-3 or ASTM A388 with a stated class.
What can Jiangyin Jiangnan Metal forge in AMS 5614C?
Jiangyin Jiangnan Metal Co., Ltd. is an open-die forging factory at No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China, operating since 2008 with 460 employees, including 9 senior and 32 intermediate engineers. The envelopes below are what we have run in this grade, not carbon-steel limits.
Forging
1 t, 3 t, 5 t and 9 t open-die hammers; 4,500 t and 5,000 t hydraulic presses; radial-axial ring rolling mills to 2,500 mm outside diameter on a 6 m ring line; trepanning and boring for hollow parts.
Heat treatment
Bogie-hearth furnaces to 1,100 °C with ±5 °C uniformity; dedicated tempering furnaces 200–800 °C with ±3 °C uniformity and chart recording; oil, water and forced-air quench; part thermocouples on request.
Machining
CNC vertical and horizontal lathes, boring mills and machining centres for rough, semi-finish and finish machining, so a ring or shaft can leave the plant ready to install rather than as a black forging.
Inspection
Optical emission spectrometer, universal tensile machine, Charpy impact machine with sub-zero bath, Brinell and Rockwell testers, ultrasonic flaw detection, magnetic particle and penetrant lines, metallographic microscope for grain size and delta ferrite.
Which standards and certificates apply to AMS 5614C forgings?
Material and product
- SAE AMS 5614 / AMS 5614C, bars, forgings, forging stock and rings
- UNS S41025 chemistry
- ASTM A276, A479, A473 and A182 F6a for 410-family product forms
- EN 10250-4 for open-die stainless forgings, where cross-certification is required
- EN 10204 3.1 as standard; 3.2 with third-party witness
Testing and examination
- Ultrasonic: EN 10228-3, SEP 1921 or ASTM A388, to a stated quality class
- Magnetic particle: ASTM E1444 or ISO 9934
- Penetrant: ASTM E165 or ISO 3452
- Tensile ASTM E8/E8M or ISO 6892; impact ASTM E23 or ISO 148
- Hardness ASTM E10 / E18; grain size ASTM E112; macroetch ASTM E381
- Delta ferrite count and microstructure on request
Quality management is certified to ISO 9001:2015. Third-party witness certificates are issued through the inspection body you nominate: Lloyd’s Register, DNV, Bureau Veritas, ABS, TÜV or SGS. Customers keep an unrestricted right to witness any production stage, including chemistry, forging, heat treatment and mechanical testing.
How do you specify an AMS 5614C forging order?
- Name the specification and the revision. Write
AMS 5614C (UNS S41025). A purchase order that says only “12Cr stainless” or “410 with moly” leaves the trace-element ceilings and the melting route open. - State the delivery condition. Annealed for customer machining, or hardened and tempered. If tempered, give either the tempering temperature or the hardness band. “Supplied annealed” and “supplied at 25–28 HRC” are different parts, with different prices and lead times.
- Give the mechanical acceptance values. Tensile, yield, elongation, reduction of area, impact energy and impact test temperature. State the test direction: longitudinal or transverse to grain flow.
- Send the drawing with grain flow and machining stock. Mark the principal axis, the required grain direction, and the stock left on each surface for finish machining.
- Define NDE and the acceptance class. For example “UT per EN 10228-3, quality class 3” or “UT per ASTM A388 with acceptance to the purchase order”. An unqualified “ultrasonic test” is not a specification.
- Choose the certificate. EN 10204 3.1 as standard, 3.2 with a named witness where the project demands it. Say if you need cross-certification to a national standard.
- Give quantity, date, Incoterm and destination. Below roughly 500 kg we consolidate onto a larger heat, which changes both price and schedule.
Drawing callout you can copy
MATERIAL: AMS 5614C / UNS S41025 (12.5Cr - 0.5Mo)
MELTING: EAF + LF + VOD (add "+ ESR" if consumable-electrode quality required)
CONDITION: Harden 950-1010 °C, oil or forced-air quench;
temper 700 °C min 2 h, air cool. Tempering below 620 °C not permitted.
HARDNESS: 22-26 HRC, verified at locations A, B and C
TENSILE: 760 MPa UTS min, 620 MPa YS min, 18% elongation, 60% RA (longitudinal)
IMPACT: Charpy V, 3 specimens, 55 J average min at +20 °C
GRAIN FLOW: Longitudinal, parallel to the principal axis; verify per ASTM E381
NDE: UT per EN 10228-3 quality class 3
MT per ASTM E1444 on all machined surfaces
CERTIFICATE: EN 10204 3.1 (3.2 with third-party witness if stated on the PO)
SURFACE: Descaled and passivated; Ra ≤ 1.6 µm on sealing faces
MARKING: Heat number, condition and drawing number, low-stress stamped
Seven common ordering errors
- Substituting plain 410 because the chromium matches. Without molybdenum the part softens in service and pits in condensate.
- Leaving the revision letter off the order. Revisions change chemistry limits and test requirements. Cite AMS 5614C, or whichever revision your drawing invokes.
- Specifying a tempering temperature in the 400–550 °C band to reach a hardness number. The hardness is met and the toughness is lost.
- Giving a hardness band but no impact requirement on a part that will see shock loading or sub-zero start-up. A hardness test will not detect embrittlement.
- Omitting the test direction on a heavy forging. Transverse values run well below longitudinal, and the certificate can pass or fail on that word alone.
- Ordering “ultrasonic tested” with no standard or class. Each shop then applies its own acceptance level and quotations cannot be compared.
- Treating a hardness cap as sour service compliance. It is not. See the ISO 15156 note above.
Forging weight calculator
Select a shape and enter dimensions for the net weight at 7.70 g/cm³ and a rough billet allowance.
Net finished weight at 7.70 g/cm³. Add 20–35% machining stock for the rough forging, more on profiled geometries. Our single-piece limit in this grade is 8,000 kg.
RFQ writer
Complete the fields for a full enquiry that can be copied into email or WhatsApp.
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Ask for an AMS 5614C / UNS S41025 quotation
Send the drawing and the condition you need. We answer within 24 hours with price, lead time and the standards we will certify to. If a form is not convenient, write to sales@steelforgepieces.com, call 0086-189-2135-9659, or message us on WhatsApp.
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Jiangyin Jiangnan Metal Co., Ltd. · No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China · open-die forging factory since 2008 · ISO 9001:2015.
Where is AMS 5614C used?
Steam turbines
The main application. Blades and vanes, blade roots, diaphragms, shroud and lacing components, and blade attachment hardware in the intermediate and low-pressure paths, where wet steam, droplet erosion and high-cycle fatigue occur together.
Turbine rotating parts
Turbine wheels, discs and impeller blanks, forged as discs or contoured rings, where property uniformity through a heavy section and a clean ultrasonic response both have to be demonstrated.
Valves for steam and power service
Valve spindles, stems and rods, bodies, bonnets and seat rings. Spindles are a typical application: hot, cycled, in contact with packing, and required to stay dimensionally stable over a long service life.
Pumps and rotating equipment
Shafts, sleeves and wear rings in feedwater and condensate service, where the fluid is hot and mildly corrosive and a low-alloy steel shaft would rust in the packing box.
Compressors and gas turbines
Compressor blades and vanes, stator rings and casing hardware, in the cooler stages, where the strength to cost ratio is better than a nickel alloy.
Boiler and process plant
Internals, fasteners, tube-sheet hardware and structural parts in hot, wet, mildly corrosive service, generally where a hardenable stainless steel has to hold its properties at temperature.
Worked examples
Example 1: choosing a tempering temperature for a valve spindle
Given. A ø90 mm forged valve spindle in AMS 5614C, superheated steam at 480 °C, drawing requires 620 MPa minimum yield and a Charpy V of 50 J average at room temperature.
Method. Work from the service temperature first. The tempering temperature must be at least 30 °C above the service temperature, so 480 + 30 = 510 °C is the lower limit on that basis. 510 °C is inside the embrittlement band, so the effective lower limit is 620 °C. From Table 5: 620 °C gives 750–850 MPa yield but only about 40 J; 660 °C gives 690–780 MPa and about 55 J; 700 °C gives 620–700 MPa and about 70 J.
Result. Specify a temper at 700 °C. It clears the yield requirement with a margin, meets the 50 J impact requirement, and leaves 220 °C between service and tempering temperature so the spindle does not soften in service. Tempering at 620 °C would meet the yield requirement easily and fail the impact requirement, which is how this part is most often specified incorrectly.
Example 2: sizing and weighing a turbine diaphragm ring
Given. A ring, 1,400 mm outside diameter × 1,150 mm inside diameter × 260 mm high, in AMS 5614C, ultrasonic acceptance to EN 10228-3 class 3.
Method. Net volume = π/4 × (1.400² − 1.150²) m² × 0.260 m = 0.1302 m³. At 7,700 kg/m³ that is 1,003 kg net. Add 25% for machining stock and ring-rolling allowance and the rough forging is about 1,254 kg, inside both the 8,000 kg single-piece limit and the 2,500 mm ring mill envelope.
Points to settle first. A 125 mm radial wall at class 3 acceptance means the ultrasonic examination has to resolve small indications through a thick, air-hardening section. That favours ESR remelted material rather than the standard VOD route, and ultrasonic examination in the annealed condition before hardening, when attenuation is lowest. Both decisions have to be taken before the heat is bought.
Glossary
| Term | Meaning |
|---|---|
| AMS 5614C | Revision C of SAE aerospace material specification AMS 5614, covering 12.5Cr–0.5Mo corrosion- and heat-resistant steel bars, forgings, forging stock and rings. |
| UNS S41025 | The Unified Numbering System composition number for the same steel. A chemistry, not a full specification. |
| Martensitic stainless steel | A stainless steel that transforms to hard martensite on cooling from the austenitising temperature, and is therefore hardenable by heat treatment and always magnetic. |
| Tempering | Reheating hardened martensite to precipitate carbides and relieve stress. On this grade it sets the mechanical properties that appear on the certificate. |
| Temper embrittlement | Loss of impact toughness caused by tempering in, or cooling slowly through, roughly 400–550 °C. Hardness is barely affected, so only a Charpy test will detect it. |
| Delta ferrite | High-temperature ferrite retained at room temperature when the chromium equivalent is too high. It lowers transverse toughness and can affect ultrasonic response. |
| PREN | Pitting resistance equivalent number, %Cr + 3.3 × %Mo (+ 16 × %N). Roughly 13.6 for AMS 5614C, against about 32 needed for seawater. |
| Ac1 / Ms | The temperature at which austenite starts to form on heating (≈ 800 °C) and at which martensite starts to form on cooling (≈ 320 °C). |
| VOD / ESR | Vacuum oxygen decarburisation, the standard refining route for stainless steel; electroslag remelting, an additional step that improves cleanliness and transverse properties. |
| EN 10204 3.1 / 3.2 | Inspection certificate types. 3.1 is issued by the manufacturer’s own independent inspection function; 3.2 is countersigned by a third party or the buyer’s representative. |
| EN 10228-3 quality class | The ultrasonic acceptance level for ferritic and martensitic steel forgings, from class 1 (loosest) to class 4 (tightest). Always state a class. |
| Grain flow | The direction in which the forging process aligns the structure. Properties measured along the flow (longitudinal) are higher than across it (transverse). |
AMS 5614C frequently asked questions
What is AMS 5614C?
AMS 5614C is revision C of SAE aerospace material specification AMS 5614, which covers a corrosion- and heat-resistant 12% chromium martensitic steel containing roughly 0.5% molybdenum, supplied as bars, forgings, forging stock and rings. The grade is designated UNS S41025 and is a molybdenum-bearing modification of Type 410. It is used where a hardenable stainless steel has to keep its strength in hot, wet steam, and it is a common steam turbine blading and valve spindle material. Jiangyin Jiangnan Metal Co., Ltd. forges it to customer drawings in Jiangyin, Jiangsu Province, China.
What is the difference between AMS 5614 and AMS 5613?
Both cover 12% chromium martensitic stainless steel, but AMS 5613 is plain Type 410 (UNS S41000) while AMS 5614 adds 0.40–0.60% molybdenum and tightens the residual elements, giving UNS S41025. The molybdenum raises tempering resistance, creep strength and pitting resistance in condensate, which is why AMS 5614 is specified for steam-path components and AMS 5613 for general hardenable stainless parts. The two are not interchangeable on a drawing.
What is the chemical composition of AMS 5614C?
In weight percent: carbon 0.07–0.12, manganese 0.30–0.60, silicon 0.35 max, phosphorus 0.040 max, sulphur 0.030 max, chromium 11.50–12.50, molybdenum 0.40–0.60, nickel 0.60 max, copper 0.50 max, aluminium 0.05 max, tin 0.05 max, nitrogen 0.08 max, balance iron. The aluminium, tin and nitrogen ceilings are trace-element controls that protect toughness and steam-side behaviour; and they are why ordinary Type 410 cannot be substituted for it.
Is AMS 5614C the same as UNS S41025?
They describe the same steel, but they are different kinds of document. UNS S41025 is only a composition number. AMS 5614C is a full material specification: it also fixes the melting practice, the quality and cleanliness level, the delivery condition, the testing and the certification. Order to AMS 5614C when the aerospace or turbine quality level matters, and quote UNS S41025 alongside it so the chemistry is unambiguous.
What are the European, Japanese and Chinese equivalents of AMS 5614C?
There is no exact one-for-one equivalent. The closest grades are JIS SUS410J1 and Chinese 1Cr12Mo (12Cr12Mo), both 12Cr martensitic steels with 0.3–0.6% molybdenum used for turbine blading. In Europe the nearest stocked grades are X12Cr13 (1.4006) and X20Cr13 (1.4021), which contain no molybdenum, or X20CrMoV11-1 (1.4922), which has much higher carbon, molybdenum and vanadium. Treat all of these as cross-references for enquiry purposes only. Jiangyin Jiangnan Metal buys raw material to the specification named on your order rather than cross-certifying a near grade.
How is AMS 5614C heat treated?
Anneal at 840–870 °C with a slow furnace cool for machining. Harden by austenitising at 950–1010 °C, holding about 30 minutes per 25 mm of section, then quenching in oil or forced air. Temper for at least two hours at 620–760 °C and cool in air. Never temper or stress relieve between about 400 and 550 °C, because Charpy toughness collapses in that range.
What tensile strength does AMS 5614C reach?
It depends on the tempering temperature. Tempered near 620 °C, forgings typically reach 900–1,000 MPa tensile with 750–850 MPa yield and 28–32 HRC. Tempered near 700 °C they typically give 760–860 MPa tensile with 620–700 MPa yield, 22–26 HRC and much better impact energy. Annealed material is under about 690 MPa at 235 HB maximum. These are indicative production bands; the acceptance values on your certificate are the ones stated in the specification revision and drawing you order to.
Why must AMS 5614C never be tempered between 400 and 550 °C?
Twelve percent chromium martensitic steels lose impact toughness sharply when they are tempered in that band, because fine carbides precipitate on the lath boundaries and locally deplete chromium. Hardness barely changes, so a hardness check will not detect the problem. It appears in a Charpy test, or as a service failure. Temper above 620 °C, and on heavy sections cool briskly through 550–400 °C after tempering rather than letting the part cool slowly in the furnace.
Is AMS 5614C magnetic?
Yes. The structure is martensite in every delivery condition, so the steel is ferromagnetic and no heat treatment will make it non-magnetic. That also means magnetic particle inspection can be used on it, unlike the austenitic stainless grades.
What is the maximum service temperature of AMS 5614C?
For stressed components the practical ceiling is roughly 480–540 °C, set by creep and by the need to stay at least 30 °C below the tempering temperature so the part does not soften in service. Scaling resistance in air extends to about 650 °C, but that is an oxidation limit, not a strength limit. Above this range use a creep-resistant grade or a nickel alloy such as Inconel 718.
How corrosion resistant is AMS 5614C?
It resists atmospheric exposure, fresh water, wet and dry steam, mild organic acids and many hydrocarbons, and the molybdenum makes it better than plain Type 410 in condensate. Its pitting resistance equivalent number is only about 13–14, so it is not a chloride or seawater alloy. Corrosion resistance is best when the part is hardened and tempered above 620 °C with a clean, descaled surface.
Can AMS 5614C be welded?
Yes, provided normal martensitic steel practice is followed. Preheat to 200–300 °C, keep the interpass temperature in that range, use a matching 12Cr filler or an austenitic or nickel-base filler where a softer weld is acceptable, and post-weld temper at 700–760 °C. Do not let the joint cool to room temperature before post-weld heat treatment, because untempered martensite in the heat-affected zone cracks readily under hydrogen.
Is AMS 5614C acceptable for sour service under NACE MR0175 / ISO 15156?
Do not assume it is. Martensitic 12Cr steels are only acceptable in sour service within specific hardness, condition and environmental limits, and AMS 5614C is not a pre-qualified route. Check the current edition of ISO 15156-2 or 15156-3 against your actual hydrogen sulphide partial pressure, chloride content, pH and temperature. Jiangyin Jiangnan Metal will supply with a contractual hardness cap and hardness mapping, but a hardness cap on its own is not a statement of compliance.
What AMS 5614C forgings can Jiangyin Jiangnan Metal supply, and in what sizes?
Seamless rolled rings from 200 mm to 2,500 mm outside diameter with a 30 mm minimum wall, discs to 1,800 mm diameter, shafts to 8 m long, round, square and flat bar from 25 mm to 500 mm, hollow and trepanned bar, sleeves, bushings, cylinders, hubs, housings, blocks, blanks, turbine wheels and blade blanks, and valve spindles, stems, bodies and bonnets, at single-piece weights up to 8,000 kg. Everything is made to drawing at the plant at No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China.
What certificates and non-destructive testing come with AMS 5614C forgings?
EN 10204 3.1 certification is standard and EN 10204 3.2 with a third-party witness is available on request through Lloyd’s Register, DNV, Bureau Veritas, ABS, TÜV or SGS. Ultrasonic examination is carried out to EN 10228-3, SEP 1921 or ASTM A388 to the quality class stated on the order, with penetrant, magnetic particle, hardness mapping, grain size and macroetch testing added where the specification calls for them.
What is the density of AMS 5614C?
About 7.70 g/cm³, or 0.278 lb/in³, at room temperature, which is the figure used by the forging weight calculator on this page. It is slightly lower than austenitic stainless steels such as 304 because the structure is martensite rather than austenite.
What is the lead time and minimum order for AMS 5614C forgings?
Eight to twelve weeks is typical, because the heat is bought against your specification rather than pulled from stock, and third-party witnessed release adds one to two weeks. Below roughly 500 kg the order is consolidated onto a larger heat, which affects both price and schedule, so state the quantity in the enquiry. Written quotations are issued within 24 hours of receiving a drawing at sales@steelforgepieces.com or +86-189-2135-9659.
References
- SAE International, AMS 5614, Steel, Corrosion and Heat Resistant, Bars, Forgings, Forging Stock, and Rings, 12.5Cr – 0.5Mo. The governing specification for this grade; cite the revision letter in force at your contract date.
- SAE International, AMS 2759/5, Heat Treatment of Martensitic Corrosion-Resistant Steel Parts.
- SAE International, AMS 2300 / AMS 2301, Aircraft Quality and Premium Aircraft Quality Steel Cleanliness, referenced where a cleanliness class is invoked.
- SAE International, AMS 2241 (bar tolerances) and AMS 2248 (chemical check analysis limits), referenced by the AMS corrosion-resistant steel family.
- ASTM International, ASTM A276 / A479 / A473 / A182, product standards for Type 410 family bars, forgings and flanges.
- ASTM International, ASTM A388/A388M, Standard Practice for Ultrasonic Examination of Steel Forgings.
- CEN, EN 10228-3, Non-destructive testing of steel forgings — Ultrasonic testing of ferritic or martensitic steel forgings, and SEP 1921.
- CEN, EN 10250-4, Open die steel forgings for general engineering purposes — Part 4: Stainless steels.
- CEN, EN 10204, Metallic products — Types of inspection documents.
- ISO / NACE, ISO 15156-2 and 15156-3 (NACE MR0175), Materials for use in H₂S-containing environments in oil and gas production.
- ASM International, ASM Handbook Volume 1: Properties and Selection: Irons, Steels and High-Performance Alloys, martensitic stainless steels.
- ASM International, ASM Handbook Volume 4D: Heat Treating of Irons and Steels, heat treating of martensitic stainless steels.
- GB/T 1221 and GB/T 8732, Chinese standards for heat-resisting steel and steam turbine blade steel, covering 1Cr12Mo.
Standards are cited by number. Always work to the revision in force at your contract date. Test results on our certificates are independent and traceable to calibrated equipment.
About the manufacturer, and how to cite this page
Jiangyin Jiangnan Metal Co., Ltd. is an open-die forging factory at No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China, operating since 2008 with 460 employees, including 9 senior engineers and 32 intermediate engineers. The plant runs 1 t to 9 t open-die hammers, 4,500 t and 5,000 t hydraulic presses and radial-axial ring mills to 2,500 mm outside diameter, with heat treatment, machining, mechanical testing and non-destructive examination in house. Alongside AMS 5614C / UNS S41025 we forge carbon, alloy and tool steels, the martensitic and precipitation-hardening stainless families, duplex grades and nickel alloys. Quality management is certified to ISO 9001:2015, and material is supplied with EN 10204 3.1 certification as standard, 3.2 with third-party witness on request.
Suggested citation
Jiangyin Jiangnan Metal Co., Ltd. (2026). AMS 5614C / UNS S41025 forgings: chemical composition, heat treatment, mechanical properties and ordering guide. Updated 3 September 2026. Retrieved from https://www.steelforgepieces.com/Alloy-Steel/AMS-5614C.html
Contact for technical questions or a quotation: Jiangyin Jiangnan Metal Co., Ltd., No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China · 0086-189-2135-9659 · sales@steelforgepieces.com · WhatsApp