Grade summary
UNS S42200, written on older drawings as SAE 51422 and known elsewhere as AISI 422, AISI 616, JIS SUH 616 and EN 1.4935 (X20CrMoWV12-1), is a hardenable martensitic stainless steel with roughly 11 to 13 per cent chromium plus molybdenum, tungsten and vanadium. Those three additions form stable carbides and are the reason the steel holds its strength under load at red heat, which is why it has stayed in use for turbine blading since the 1950s. Alloy 422 is rated for service to 1200 F (649 C) and has good resistance to scaling and oxidation.
Jiangyin Jiangnan Metal Co., Ltd. is an open-die forging factory in Jiangyin City, Jiangsu Province, China. We forge UNS S42200 into round bars, seamless rolled rings, discs, blocks, hollow bars, sleeves, turbine blade stock, valve spindles and double end studs, and supply them hardened and tempered with an EN 10204 3.1 certificate. Telephone 0086-189-2135-9659, email sales@steelforgepieces.com.
Page reviewed 9 October 2026. Figures taken from ASTM A565, AMS 5655, EN 10088-3 and EN 10302, and from published mill datasheets.
1. Designations and equivalent grades
This steel travels under a lot of names, and buyers often quote two or three of them on the same enquiry. The table below lists the ones we see most often on drawings and purchase orders.
| System | Designation |
|---|---|
| UNS | S42200 |
| AISI / SAE, USA | AISI 422, AISI 616, SAE 51422 |
| ASTM | ASTM A565 Grade 616, bars, forgings and forging stock |
| Aerospace | AMS 5655, bars, wire and forgings, hardened and tempered |
| EN, Europe | 1.4935, X20CrMoWV12-1 (also published as X22CrMoWV12-1) |
| JIS, Japan | SUH 616 |
| BS, UK | BS 970 442S19, EN61 |
| Military and OEM | DOD F 24669/7, MIL S 861, B50A125, B50A951A1, 20VNiWMoCr120, HWMoV3, T502 |
One point worth checking before you place an order. The EN and ASTM chemistry windows overlap but do not match. EN 1.4935 allows tungsten 0.4 to 0.6 per cent and vanadium 0.25 to 0.35 per cent, while the ASTM window for S42200 is tungsten 0.75 to 1.25 and vanadium 0.15 to 0.30. On a rotating part that difference can matter to the end user, so name one standard on the order and we certify to that one rather than treating them as the same material.
2. Chemical composition
ASTM limits for Grade 616 / UNS S42200 are given below, with iron making up the balance at around 82 per cent.
| Element | Content | Why it is there |
|---|---|---|
| Carbon, C | 0.20 to 0.25 | Hardenability and carbide formation |
| Chromium, Cr | 11.00 to 12.50 | Scaling and oxidation resistance |
| Nickel, Ni | 0.50 to 1.00 | Toughness, holds back delta ferrite |
| Molybdenum, Mo | 0.90 to 1.25 | Creep strength, temper resistance |
| Tungsten, W | 0.90 to 1.25 | Creep strength at temperature |
| Vanadium, V | 0.20 to 0.30 | Fine carbide dispersion, grain refinement |
| Manganese, Mn | 0.50 to 1.00 | Deoxidation and hardenability |
| Silicon, Si | 0.50 max | Deoxidation |
| Phosphorus, P | 0.025 max | Residual, held down for toughness |
| Sulfur, S | 0.025 max | Residual, held down for toughness |
| Iron, Fe | balance, about 82 | Base |
Published ASTM ranges vary slightly between sources, with some datasheets quoting Mo and W from 0.75 and Si up to 0.75. For rotating turbine parts we normally melt AOD and then remelt by ESR. The remelt tightens the inclusion rating and lifts transverse toughness, which shows up where it counts, on blade roots and disc rims. Say so in the enquiry if ESR is mandatory for you.
3. Physical properties
| Property | Metric | Imperial | Note |
|---|---|---|---|
| Density | 7.7 to 7.8 g/cm3 | 0.278 to 0.282 lb/in3 | EN 7.7, other datasheets 7.8 |
| Thermal conductivity | 24 W/m·K | about 14 BTU/h·ft·F | At 100 C |
| Thermal expansion | 10.5 to 12.5 x 10-6 /K | 5.8 to 6.9 x 10-6 /F | EN range; 11.2 quoted for 0 to 100 C |
| Specific heat | 460 J/kg·K | 0.11 BTU/lb·F | |
| Electrical resistivity | 0.6 micro-ohm·m | ||
| Modulus of elasticity | 190 to 216 GPa | 27,600 to 31,300 ksi | EN gives 216, other sources 190 to 210 |
| Poisson's ratio | 0.27 to 0.30 | 0.27 to 0.30 | |
| Magnetic response | Magnetic in every condition, the structure is martensitic | ||
4. Mechanical properties
Strength in this grade is set almost entirely by the tempering temperature, so the figures below are kept separate by the standard they come from instead of being merged into one set.
4.1 AMS 5655, hardened and tempered
| Property | Value |
|---|---|
| Ultimate tensile strength | 140 ksi (965 MPa) |
| 0.2 per cent yield strength | 115 ksi (793 MPa) |
| Elongation in 2 in. | 13 per cent |
| Reduction of area | 25 per cent |
| Hardness | 293 to 341 HB |
Some circulated copies of this table print the tensile and yield figures the other way round, which cannot be right since yield always sits below ultimate. The order above is the physically correct one. Other suppliers publish a lower minimum set for general bar, around 897 MPa tensile with 15 per cent elongation and 290 HB maximum, so always work to the acceptance values written into your own order.
4.2 EN 1.4935 delivery classes
| Class | Yield Re min | Tensile Rm | Elongation A min |
|---|---|---|---|
| +QT700 | 500 MPa | 700 to 850 MPa | 15 per cent |
| +QT800 | 600 MPa | 800 to 950 MPa | 14 per cent |
4.3 Yield strength at temperature
This is the data that actually sizes a turbine part, and it shows what the molybdenum, tungsten and vanadium are buying.
| Test temperature | +QT700 | +QT800 |
|---|---|---|
| 50 C | 465 MPa | 585 MPa |
| 100 C | 460 MPa | 560 MPa |
| 150 C | 445 MPa | 545 MPa |
| 200 C | 430 MPa | 530 MPa |
| 250 C | 415 MPa | 505 MPa |
| 300 C | 390 MPa | 480 MPa |
| 350 C | 380 MPa | 450 MPa |
| 400 C | 360 MPa | 420 MPa |
| 450 C | 330 MPa | 380 MPa |
| 500 C | 290 MPa | 335 MPa |
| 550 C | 250 MPa | 280 MPa |
Creep rupture strength for 1.4935 is quoted above 275 MPa for 100,000 hours at 500 C. Note the gap between the two temperature limits you will see in print. The 1200 F (649 C) figure applies to short term and oxidation limited duty, while EN sets 580 C as the ceiling for continuous creep loaded operation. Both are correct in their own context, and the lower one is the number to design long life rotating parts against.
5. Forging and heat treatment
Section size drives quench response, so we set the heat treatment route against the actual forging envelope instead of running one recipe for everything. On heavy discs and rings we take test prolongations from the forging itself, which means the certified properties come from the part rather than from a separate coupon.
Machining
Machinability is close to 18-8 austenitic stainless and a little easier. Sharply ground tools and a steady speed and feed keep galling down. Published starting points for cobalt high speed tooling are 90 to 120 sfpm turning, 40 to 75 sfpm drilling, 70 to 120 sfpm milling and 20 to 60 sfpm reaming, with 8 to 14 degrees side rake on turning tools, a 140 degree drill point, and 10 to 15 degrees back rake for threading.
Welding
Hard. EN assigns 1.4935 to welding group 7.2 under ISO/TR 20172. Any weld calls for preheat, interpass temperature control and post weld heat treatment, and most turbine specifications rule out weld repair on finished parts. Where the geometry allows it, a one piece forging is the cheaper and safer route than a fabrication.
6. Forged product forms in UNS S42200
7. Where the grade is used
UNS S42200 gets specified where a part has to hold load and resist scaling in hot, mildly corrosive service without paying for an austenitic or nickel alloy. Published application lists cover steam and gas turbine components, turbine blades, compressors, rotors, aircraft parts, valves and high temperature bolting. Corrosion resistance extends to atmosphere, fresh water, steam and the milder acids and alkalies, so it is the wrong pick for aggressive chloride service or strong acids.
8. Testing and documents
Every UNS S42200 forging ships with an EN 10204 3.1 certificate covering melt analysis, heat treatment records and mechanical results, with product analysis added on request. Depending on the specification we also run ultrasonic testing to ASTM A388 or SEP 1921, magnetic particle inspection to ASTM E709, grain size and inclusion rating, hardness survey, Charpy V notch impacts at the stated temperature, and intergranular corrosion testing. Witness inspection by TUV, SGS, BV, Lloyd's or your own engineer is routine here and welcome.
9. Common questions
What is UNS S42200 stainless steel?
Is AISI 422 the same as EN 1.4935?
How is UNS S42200 heat treated?
What is the maximum service temperature of 422 stainless steel?
Is UNS S42200 weldable?
What sizes are forged, and is there a minimum order?
Who supplies UNS S42200 open-die forgings?
10. Request a quotation
Quoting takes very little from you. We need the grade and standard, for instance UNS S42200 to ASTM A565 Grade 616, the forged shape with finished dimensions or a drawing, the quantity, the delivery condition you want (+QT700, +QT800 or a hardness band), and any NDT or third party inspection that applies. Drawings in PDF, DWG or STEP all work.
Jiangyin City, Jiangsu Province, China
Data sources
Figures on this page come from ASTM A565 / A565M, AMS 5655, EN 10088-3:2014 and EN 10302, together with published datasheets for the grade. Where sources disagree, both are shown rather than averaged, which is the case for density at 7.7 to 7.8 g/cm3 and for modulus at 190 to 216 GPa. Everything here is indicative. The governing numbers for any order are the ones on the mill certificate that ships with the goods.