AISI 416 / (1.4005)

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AISI 416 / (1.4005) / UNS S41600 / AMS 5610

AISI 416
UNS S41600 · W.Nr. 1.4005 · X12CrS13. This is a MARTENSITIC stainless steel: it transforms to martensite on austenitising and quenching and is then TEMPERED. It does NOT precipitation harden; there is NO H900 / H1025 type ageing step. This grade is 410 WITH SULFUR ADDED, and sulfur is the only thing that sets the two apart. EN 10088-3 for 1.4005: C 0.06-0.15% – Si 1.00% max – Mn 1.50% max – P 0.040% max – S 0.15-0.35% – Cr 12.0-14.0% – Mo 0.60% max – balance Fe. ASTM A582 / the Carpenter type analysis: C 0.15% max (THERE IS NO FLOOR) – Mn 1.25% max – P 0.060% max – S 0.150% min – Si 1.00% max – Cr 12.00-14.00% – balance Fe; Swiss Steel adds Cu 0.50% max, and Rolled Alloys and Swiss Steel give Mo 0.60% max. THE DIFFERENCES MATTER: EN sets a carbon FLOOR (0.06%) and a sulfur CEILING (0.35%), ASTM sets neither; the ASTM phosphorus ceiling is 0.060% against 0.040% in EN; the manganese ceiling is 1.25% in ASTM and 1.50% in EN.​‌​​‌​

Not to be confused with

AISI 410

For what
Bought for volume-machined parts where machining cost governs, the environment is mild and the part is NOT WELDED: automatic screw machine parts, shafts, axles, gears, bolts and nuts, valve trim, pump shafts, lead screws, solenoid valve cores (Zapp), firearm parts and golf club heads (Carpenter).
Forms
Round bar, flat bar, plate, sheet, pipe, forging. All forms are supplied to order.
Standards
AMS: 5610 – ‘Steel, Corrosion and Heat-Resistant, Bars, Wire, and Forgings 12.5Cr – Low Carbon (SAE 51416, 51416Se) Free-Machining’. ASTM: A582 / A582M (free-machining stainless bars). EN: 1.4005 · EN 10088-3 (bars, wire, sections; +A and +QT650 conditions). Welding procedure: ASME Section IX P-No 6 (although this grade is not welded in practice).
THE AMS 5610 TRAP: this number DOES NOT BELONG TO A SINGLE ALLOY. Its title names both SAE 51416 (the sulfur-bearing 416) and SAE 51416Se (the selenium-bearing 416Se), and the specification separates them as TYPES.
Advantage
THE BEST MACHINABILITY OF ANY STAINLESS STEEL sits in this grade, and it comes together with the ability to be hardened by heat treatment. In numbers: AZoM gives a machinability rating of 85% and calls it the highest of all stainless steels;
Welding
IT IS NOT SUITABLE FOR WELDING. Five independent sources say the same thing: Carpenter states it is ‘not recommended for welding’; Rolled Alloys states that ‘typically free-machining grades are not welded due to problems stemming from the free-machining additives’;
Limits
1) IT IS NOT WELDED (five sources above). 2) ITS CORROSION RESISTANCE IS LOWER THAN THAT OF 410. The cause is the same sulfur: MnS inclusions act as pit initiation sites in the passive layer.
Compiled from manufacturer data sheets · confirm against the current specification before ordering

On this page · click to jump
What AISI 416 IsStandards by Product FormProduct Forms With NO StandardChemical CompositionMechanical PropertiesPhysical PropertiesHeat TreatmentWeldingMachiningCorrosionFrequently Asked Questions



Corrosion resistance: The corrosion resistance and surface quality of AISI 416 are lower than those of 1.4006 because of the sulphur addition. It is not suitable for severe corrosive conditions. With corrosion resistance that is not very good, this grade should not be used in corrosive environments.​‌​​‌​

Weldability: Welding is not recommended for this grade, which is both high in chromium and high in sulphur, and welding this material is quite difficult.

Machinability: Thanks to the high sulphur content it contains, this grade is very easy to machine. Grade 416 stainless steel in the annealed condition has very good machinability.​‌​​‌​

Heat treatment: The most important property of this stainless grade is that it can be hardened by heat treatment, and that it machines very easily and quickly in the annealed condition. After heat treatment, however, machinability falls to a certain extent in this grade, so machining is recommended before heat treatment. Among the martensitic steels, AISI 416 offers better properties in terms of weldability, although there are some factors to observe during welding, such as overheating.

Applications: AISI 416 stainless steel is frequently used in the machinery industry, in defence industry components, in automotive parts and in valves. It is suitable for producing screws, nuts, shafts, fittings and similar parts. Carbide or ceramic tooling is recommended for machining.​‌​​‌​

AISI 416 is a martensitic stainless steel that provides high machinability, wear resistance and mechanical strength. Its sulphur content gives very good machinability, but its corrosion resistance is limited. These properties make the steel ideal for applications such as cutting tools, mechanical parts and industrial equipment, while its use in aggressive chemical environments or areas carrying a high corrosion risk is limited.

Chemical Composition

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CMin. 0.06 · Max. 0.15​‌​​‌​
MnMax. 1.50​‌​​‌​
SiMax. 1.00​‌​​‌​
PMax. 0.04​‌​​‌​
SMin. 0.15 · Max. 0.35​‌​​‌​
CrMin. 12 · Max. 14​‌​​‌​
MoMax. 0.60​‌​​‌​
Mechanical Properties

Tensile Strength (MPa)​‌​​‌​650-850
Proof Stress (MPa)​‌​​‌​450
Elongation A50 mm​‌​​‌​–
Hardness Brinell​‌​​‌​≤207 Max HB
Density​‌​​‌​7.75 g/cm3
Melting Point​‌​​‌​1480-1530 °C
Modulus of Elasticity​‌​​‌​200 kN/mm²
Electrical Resistivity​‌​​‌​0.57 x 10-6 Ω.m
Thermal Conductivity​‌​​‌​24.9 W/m.K
Thermal Expansion​‌​​‌​9.9 x 10-6/K
Standards and Equivalents · AISI 416
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Trade nameAISI 416​‌​​‌​
UNSS41600​‌​​‌​
W.Nr (DIN/EN)1.4005 · 1.4006​‌​​‌​
AMS5610​‌​​‌​
ASTMA484 · A582​‌​​‌​
Available formsRound bar · Flat bar · Plate · Sheet · Tube · Forgings
All forms are supplied to order.​‌​​‌​

What AISI 416 Is — a Steel Designed as a Trade-off​‌​​‌​

AISI 416 (UNS S41600 / W.Nr. 1.4005 / DIN X12CrS13) is the sulphurised, free-machining derivative of 410. Its chemistry is the same as 410 — 12–14 % Cr, C ≤0.15 % — with one addition: a minimum of 0.15 % sulphur. That single addition makes it the easiest-machining stainless grade there is and at the same time permanently degrades its corrosion resistance, weldability and formability. 416 is not a performance alloy; it is a deliberate trade-off.

The mechanism is simple and is exactly the logic of 303. Sulphur combines with the manganese in the steel to form manganese sulphide (MnS) inclusions. These are soft, friable islands dispersed through the matrix, and they do three jobs: (1) they break the chip — short controlled chips instead of long stringy ones; (2) they act as a solid lubricant in the cutting zone, lowering tool–chip friction; (3) they lower cutting force and heat — tool life goes up, surface finish improves. On a screw machine running unattended overnight, the combined value of those three effects is large.​‌​​‌​

The price comes from the very same inclusions. MnS particles are discontinuities in the passive film. In chloride environments that is precisely where pitting starts; in the weld pool sulphur forms low-melting-point films that cause hot cracking; in cold forming the inclusions act as crack initiators. These are not defects that can be fixed — they are the unavoidable consequence of what the steel was designed to do.

The One Sentence That Separates 416 From Its Siblings

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AISI 410Sulphur-free 13Cr martensitic. Hardenable, weldable, moderate corrosion resistance — but hard to machine. It is 416’s parent metal​‌​​‌​
AISI 303Sulphurised austenitic (18Cr-8Ni). Similar machinability, markedly better corrosion resistance than 416 — but it CANNOT BE HARDENED and is essentially non-magnetic. That is the real dividing line between 416 and 303​‌​​‌​
AISI 430FSulphurised ferritic (17Cr). Slightly better corrosion resistance than 416 thanks to higher chromium, but it CANNOT BE HARDENED. For magnetisable parts that do not need strength​‌​​‌​
AISI 416Se (S41623)The variant free-machined with selenium instead of sulphur. Better cold-forming and hot-working behaviour than 416, higher surface quality. Hard to source and expensive​‌​​‌​
Where 416 stands aloneIt is the only stainless grade that both machines freely AND hardens. 303 does not harden, 430F does not harden, 410 does not machine freely. If a part must be produced in high volume on a screw machine AND hardened to 30 HRC, the real number of options is one.​‌​​‌​

Standards by Product Form

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STANDARDS BY PRODUCT FORM

Product formStandards
Round bar, flat bar (sections)​‌​​‌​AMS 5610 (12.5Cr low carbon, SAE 51416 / 51416Se, free-machining – THE TYPE NUMBER IS REQUIRED) · ASTM A582 / A582M (free-machining stainless bars) · EN 10088-3 (1.4005, +A and +QT650)
Wire and wire rod​‌​​‌​AMS 5610 also covers wire. ASTM A581 (free-machining wire and wire rods) could be verified in only 2 sources and has not been written onto the card.
Forgings​‌​​‌​AMS 5610 also covers forgings. ASTM A473 (forgings) was found in 3 sources and ASTM A314 (billets and bars for forging) in 3; neither reached four sources and neither has been written onto the card.
Plate, sheet, strip​‌​​‌​ASTM A895 (free-machining plate, sheet and strip) could be verified in only 2 sources. An order for this form must be tied to a specification the buyer verifies.
Pipe and mechanical tubing​‌​​‌​No pipe specification for 416 could be verified against four sources. ASTM A511 (seamless mechanical tubing) was found in a single source. An order must be tied to a specification agreed between buyer and seller.
Welding​‌​​‌​THIS GRADE IS NOT WELDED. A filler metal list is deliberately not given. Where it cannot be avoided, AZoM recommends 410 low-hydrogen electrodes or 309 filler with a 200-300 °C preheat, and Rolled Alloys requires an anneal at about 788 °C after welding. Procedure group: ASME Section IX P-No 6.
AMS 5610 is the ONLY verified AMS number for this grade and its title covers both the sulfur and the selenium type; an order without the type number is incomplete. On the ASTM side only A582 could be verified against four sources. The other numbers are written inside their rows with how many sources they were found in and are not presented as verified. The welding row is deliberately a ‘do not’ row; welding this grade is a sign that the material selection was wrong from the start.

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Note carefully: the specification coverage of 416 is built around BAR. That is no accident — it follows directly from what the material is. 416 is a bar steel made for the screw machine, and in other product forms it is either absent or severely limited.

Standards by Product Form · S41600 / 1.4005

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Bar · rod · section (THE MAIN ROUTE)ASTM A582 — Free-Machining Stainless Steel Bars. This is the real and primary specification for 416. Cold drawn, turned, ground and hot rolled bar​‌​​‌​
Billets and bars for forgingASTM A314 — Stainless Steel Billets and Bars for Forging​‌​​‌​
Forgings (finished)ASTM A473 — stainless steel forgings​‌​​‌​
General requirementsASTM A484 — the general requirements document for bar, billet and forgings. Read together with A582​‌​​‌​
Wire (chemistry)ASTM A581 — free-machining stainless wire; chemistry and dimensions​‌​​‌​
AerospaceAMS 5610 (Type 2). Military/federal: QQ-S-763 and QQ-S-764​‌​​‌​
SAESAE J405, number 51416​‌​​‌​
Surgical instrumentsASTM F899 — single-sourced and conditional: the source page notes “not applicable in all situations, request at order placement”. Do not publish it unqualified​‌​​‌​
EuropeEN 10088-3, grade 1.4005 / X12CrS13. Semi-finished products, bar, wire and sections only — showing that the product-form limit is the same on the European side​‌​​‌​
National equivalentsBS 416S21 · old British EN56AM · JIS SUS416 · AFNOR Z11CF13 (some sources print Z13CF13)​‌​​‌​
ASME Section IXSince it is not welded there is no practical P/F number question. 13Cr martensitics are generally in the P-No. 6 group, but welding 416 is not recommended and it should not be used as the basis of a WPS​‌​​‌​

Product Forms With NO Standard — the Commercially Valuable Section

This is the section a sales engineer must memorise, and for 416 the list is long. It is exactly where customers get confused: 416 is such a common grade that it is assumed to exist in every form. It does not.​‌​​‌​

Specification Gaps for S41600

Plate · sheet · strip​‌​​‌​S41600 is NOT in the ASTM A240 grade list. A240, the main specification for stainless plate and sheet, does not cover 416. A single distributor page cites ASTM “A895” for 416 plate — A895 is genuinely a specification written for free-machining stainless flat products, but this could not be independently verified here. Do not promise a customer “416 plate to ASTM A240”. In practice 416 flat product is sold to mill specification and in limited sizes
Seamless and welded pipe / tube​‌​​‌​S41600 is not in the grade list of ASTM A268 (ferritic and martensitic stainless tubing). A312 is austenitic and does not cover it either. There is no such ASTM product as free-machining stainless pipe. The reason is metallurgical: tube making requires welding or heavy hot deformation, and sulphur sabotages both
Flanges · forged fittings​‌​​‌​There is no grade “F416” in the ASTM A182 grade list. A182’s martensitic grades revolve around F6a and F6NM. A 416 flange is machined from bar or forging and is not an ASTM flange grade
Bolts · nuts​‌​​‌​416 is not in the ASTM A193 / A194 / A320 grade lists. Martensitic stainless bolting revolves around B6 (410). 416 fasteners are made and sold — but under A582 bar plus a drawing plus separate mechanical requirements, not a bolting specification. In highly stressed fasteners, a sulphurised steel deserves a separate question
Welding wire and electrodes​‌​​‌​There is NO matching filler metal for 416, and there never will be. Making a sulphurised filler means deliberately building hot cracking into the weld metal. This is not a gap; it is a deliberate absence
Pressure-vessel service​‌​​‌​416 is not used as a pressure-boundary material. There is no ASME coverage, and the ASTM pressure-vessel bar specification (A479) does not cover it. Say so at the quotation stage
Castings​‌​​‌​416 has no standardised cast equivalent. On the cast martensitic stainless side ASTM A743 offers CA15 (the 410 counterpart) and CA6NM; no sulphurised cast grade is listed. Sulphur would produce hot tearing in a cast microstructure anyway

Chemical Composition​‌​​‌​

There are two genuine differences between ASTM and EN, and both cause trouble in the field.

Chemical Composition · ASTM / AISI Route (A582 S41600), %

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Carbon (C)≤0.15 — NO lower limit. This matters: a heat at 0.06 % C conforms to the standard and will not give the expected hardness​‌​​‌​
Manganese (Mn)≤1.25 — needed to tie the sulphur up as MnS​‌​​‌​
Silicon (Si)≤1.00​‌​​‌​
Phosphorus (P)≤0.060 — looser than 410 (0.040 %)​‌​​‌​
Sulphur (S)≥0.15 — this is a MINIMUM, not a maximum. The AISI definition gives no upper limit; some manufacturer specifications apply a 0.35 % ceiling​‌​​‌​
Chromium (Cr)12.00–14.00​‌​​‌​
Molybdenum (Mo)≤0.60 — a producer option. Not mandatory; some mills add it to balance machinability and corrosion. Unless it is specified in the order, its presence cannot be guaranteed​‌​​‌​
Copper (Cu)≤0.50 — in some manufacturer specifications; in the base ASTM table this could not be independently verified​‌​​‌​
Nickel (Ni)No requirement. Residual nickel is present; do not publish a nickel band​‌​​‌​
Chemical Composition · EN 10088-3 Route (1.4005 / X12CrS13), %

Carbon (C)​‌​​‌​0.08–0.15 — NOTE: EN imposes a LOWER limit. ASTM does not. This is the single most important difference between the two standards: EN 1.4005 guarantees that it can harden, ASTM S41600 does not
Silicon (Si)​‌​​‌​≤1.00
Manganese (Mn)​‌​​‌​≤1.50 — higher than ASTM’s 1.25 %
Phosphorus (P)​‌​​‌​≤0.040 — TIGHTER than ASTM’s 0.060 %
Sulphur (S)​‌​​‌​0.15–0.35 — EN imposes both a lower AND an upper limit. ASTM sets only a minimum. A heat at 0.45 % S can be called AISI 416 and is NOT EN 1.4005
Chromium (Cr)​‌​​‌​12.0–14.0 — the two standards agree here
Molybdenum (Mo)​‌​​‌​≤0.60 — optional in EN as well
Practical consequence​‌​​‌​EN 1.4005 is the narrower, more predictable material. If you are buying a part that will be hardened, EN’s carbon minimum is in your favour; if corrosion is your concern, EN’s sulphur ceiling is in your favour. Ask for dual-certified bar (S41600 + 1.4005)

Mechanical Properties​‌​​‌​

STRENGTH VALUES
Yield (MPa)Tensile (MPa)EN 10088-3 · 1.4005 · +A (annealed bar)730EN 10088-3 · 1.4005 · +QT650 (t <= 160 mm)650450Condition T – heat treated (high temper)890760Annealed – measurement517275Hardened and tempered at 204 °C – measurement13401050Hardened and tempered at 650 °C – measurement796670Hardened and tempered at 200 °C – measurement14901210Hardened and tempered at 700 °C – measurement690500Zapp 1.4005 – solenoid valve grade, annealed and ground (C 0.02% max)350230
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ConditionHardnessYield MPaTensile MPaElongation
EN 10088-3 · 1.4005 · +A (annealed bar)–​‌​​‌​–730 max​‌​​‌​–
EN 10088-3 · 1.4005 · +QT650 (t <= 160 mm)​‌​​‌​–450​‌​​‌​650-85012% min​‌​​‌​
Condition T – heat treated (high temper)26-32 HRC (Rolled Alloys, Swiss Steel); Swiss Steel also gives 27-31 HRC​‌​​‌​760-895890-1035​‌​​‌​5% min
Annealed – measurement​‌​​‌​–275​‌​​‌​51730%​‌​​‌​
Hardened and tempered at 204 °C – measurement–​‌​​‌​10501340​‌​​‌​11%
Hardened and tempered at 650 °C – measurement​‌​​‌​–670​‌​​‌​79617.5%​‌​​‌​
Hardened and tempered at 200 °C – measurement–​‌​​‌​12101490​‌​​‌​10.8%
Hardened and tempered at 700 °C – measurement​‌​​‌​–500​‌​​‌​69021.5%​‌​​‌​
Zapp 1.4005 – solenoid valve grade, annealed and ground (C 0.02% max)–​‌​​‌​230350-550​‌​​‌​30% min
Hardness attainable by heat treatment (general)​‌​​‌​26-32 HRC–​‌​​‌​––​‌​​‌​
In the chart, a value given as a range is drawn at its lower bound; the full range is in the table. SPECIFICATION MINIMA and TYPICAL MEASUREMENTS are given on separate rows and must not be mixed. The elongation floor of Condition T is 5%. That is a third of the ASTM A276 Condition T floor for 410 in the same family (15%), and it is the direct price of the sulfur. The Zapp row is NOT standard 416: under the same W.Nr. it is a separate grade whose carbon has been cut to 0.02% for magnetic applications. It is here for comparison and to show the trap. The low-temper rows from AZoM and Lucefin do not give the same number (1340 MPa at 204 °C against 1490 MPa at 200 °C). Both are written with their source named, and NO AVERAGE HAS BEEN TAKEN.

The mechanical properties of 416 cannot be given in one table, because the material is sold in three different conditions: annealed, cold drawn, and hardened-and-tempered. Under the same bar designation you are buying three different steels.​‌​​‌​

Annealed and Cold-Drawn Conditions · ASTM A582 and Producer Data

Annealed (ASTM A582 typical)​‌​​‌​Rm 517 MPa · Rp0.2 275 MPa · A 30 % · Hardness ≤262 HB. [Conflict] In that row the hardness is a CEILING while the tensile is a TYPICAL value — 262 HB corresponds to roughly 900 MPa tensile. Do not read them as a description of one and the same material condition
Cold-drawn bar, ≤25 mm​‌​​‌​Rm 620–830 MPa · Rp0.2 550–725 MPa · A ≥10 % · Z ≥40 % · Hardness 190–240 HB
Turned bar, >25 mm​‌​​‌​Rm 650–750 MPa · Rp0.2 510–580 MPa · A ≥20 % · Z ≥60 % · Hardness 190–210 HB
The section effect is serious​‌​​‌​Between ≤25 mm and >25 mm, elongation goes from 10 % to 20 % and yield falls from 725 to 580 MPa. The cold-draw effect disappears in heavy bar. Re-check the properties whenever the diameter changes
EN 1.4005 annealed​‌​​‌​Rm ≤730 N/mm² · Hardness ≤220 HB (annealed 745–825 °C, furnace cooled)
EN 1.4005 +QT650​‌​​‌​Rp0.2 ≥450 N/mm² (typical 480) · Rm 650–850 N/mm² (typical 710) · A ≥12 % (typical 14 %). Hardened 950–1000 °C, tempered 680–780 °C
Hardened Condition · “Condition T” and the Tempering Curve

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Maximum as-quenched hardness41–43 HRC. That is the ceiling 416 can reach, and it does not approach 420 or 440C — its carbon is lower​‌​​‌​
Condition T (ASTM A582 typical)Rm 758 MPa · Rp0.2 586 MPa · A 18 % · Hardness 248–302 HB​‌​​‌​
Condition T (producer band)Rm 890–1035 MPa · Rp0.2 760–895 MPa · A ≥5 % · Z ≥40 % · Hardness 27–31 HRC (264–294 HB). [Conflict] There is a serious gap between the ASTM typical values and the producer band — state in the purchase order which numbers you are buying​‌​​‌​
Tempered at 204 °CRm 1340 MPa · Rp0.2 1050 MPa · A 11 % · 388 HB​‌​​‌​
Tempered at 316 °CRm 1350 MPa · Rp0.2 1060 MPa · A 12 % · 388 HB​‌​​‌​
Tempered at 427 °CRm 1405 MPa · Rp0.2 1110 MPa · A 11 % · 401 HB — the peak of the curve. BUT NOBODY TEMPERS AT THIS TEMPERATURE, for the reason given below​‌​​‌​
Tempered at 538 °CRm 1000 MPa · Rp0.2 795 MPa · A 13 % · 321 HB​‌​​‌​
Tempered at 593 °CRm 840 MPa · Rp0.2 705 MPa · A 19 % · 248 HB​‌​​‌​
Tempered at 650 °CRm 796 MPa · Rp0.2 670 MPa · A 17.5 % · 253 HB​‌​​‌​
How to read the curveThe hardness and strength peak at 427 °C is a trap. 416 tempered in that region loses both impact resistance and corrosion resistance. There are two usable windows: low tempering at roughly 150–400 °C (high hardness, low toughness) or high tempering above 580 °C (moderate hardness, acceptable toughness). The band in between is forbidden​‌​​‌​

Physical Properties

Published physical data for 416 scatters by roughly 20 % between sources. The scatter itself is shown below.​‌​​‌​

Physical Properties · S41600 / 1.4005

Density​‌​​‌​7.7 g/cm³ (0.276 lb/in³) — three sources agree. One secondary database gives 7.8
Melting point​‌​​‌​~1490 °C (2714 °F). One secondary database gives the range 1480–1530 °C
Elastic modulus [conflict]​‌​​‌​200 GPa (secondary database) · 205 GPa (producer) · 215 GPa (a second producer). Three different numbers. For a precise deflection calculation, ask the mill for heat data
Thermal conductivity [conflict]​‌​​‌​25.1 W/m·K (20 °C, producer) · 24.9–28.7 W/m·K (secondary database) · 30 W/m·K (two European producers). There is a genuine split between 25 and 30
Specific heat​‌​​‌​460 J/kg·K (20 °C) — two European sources give the same value. One secondary database gives a 460–570 band
Mean thermal expansion​‌​​‌​10.8 × 10⁻⁶ /K (20–200 °C, producer) · 11.5 × 10⁻⁶ /K (20–200 °C, second producer) · 10.5–12.0 × 10⁻⁶ /K across the 20–400 °C range
Electrical resistivity​‌​​‌​0.55 Ω·mm²/m (producer, 20 °C) · 0.60 Ω·mm²/m (two European sources) · 0.57 Ω·mm²/m (secondary database). Three sources in a narrow band
Magnetic response​‌​​‌​Magnetic in every condition — the producer’s own wording. Annealed, cold drawn, hardened: ferromagnetic in all of them. This can be an advantage (parts sitting on magnetic fixtures, sensor targets) or an exclusion criterion (MR-compatible medical devices, field-sensitive instrumentation). No numerical relative permeability value could be found — do not publish a µr figure
Scaling resistance​‌​​‌​675 °C continuous · 760 °C intermittent. But those figures are misleading: 416 cannot be used above its tempering temperature — so the real limit is not oxidation but the loss of mechanical properties

Heat Treatment​‌​​‌​

HEAT TREATMENT — SCHEMATIC
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1 · ANNEALING – two purposes, two bands
Step1 · ANNEALING – two purposes, two bands​‌​​‌​
SummarySoftening for machinability. The sources give two separate bands: a process anneal that stays below the critical temperature and a full anneal that goes above it.​‌​​‌​
TemperaturePROCESS (SUB-CRITICAL) ANNEAL 650-825 °C: Carpenter 650-760 °C · Lucefin 750-780 °C · Rodacciai 745-825 °C. FULL ANNEAL 815-900 °C: Carpenter 815-899 °C · AZoM 815-900 °C · Swiss Steel 900 °C. The two bands are given separately and have not been merged.​‌​​‌​
TimeNo numerical time could be confirmed across four independent sources. Named value: AZoM gives half an hour for the full anneal.​‌​​‌​
CoolingIN AIR FOR THE PROCESS ANNEAL (Carpenter, Lucefin, Rodacciai). SLOW FURNACE COOLING FOR THE FULL ANNEAL (Carpenter; Swiss Steel ‘slow cooling in the furnace’; AZoM ‘controlled cooling’).​‌​​‌​
Resulting hardnessEN 10088-3 +A ceiling: 220 HB max and 730 MPa tensile max. Carpenter gives about 187 HB after the process anneal and about 155 HB after the full anneal. AZoM measures 517 MPa tensile, 275 MPa yield, 30% elongation and 262 HB in the annealed condition.​‌​​‌​

2 · AUSTENITISING + QUENCH (hardening)
Step​‌​​‌​2 · AUSTENITISING + QUENCH (hardening)
Summary​‌​​‌​The step that produces the hardness. Carbon goes into solid solution and transforms to martensite on quenching. The sulfide inclusions do not dissolve at this step; they stay where they are.
Temperature​‌​​‌​925-1010 °C. Carpenter 927-1010 °C · AZoM 925-1010 °C · Rodacciai 950-1000 °C · Lucefin 980-1010 °C. A SOURCE THAT DIVERGES: Swiss Steel gives a single value of 950 °C. NO AVERAGE HAS BEEN TAKEN.
Time​‌​​‌​No numerical time could be confirmed across four independent sources.
Cooling​‌​​‌​OIL or AIR. Carpenter and AZoM say OIL; Swiss Steel ‘air or oil’; Rodacciai ‘air or oil’; Lucefin ‘oil / polymer / air’. No source recommends a water quench.
Resulting hardness​‌​​‌​No as-quenched hardness figure could be found across four independent sources. The nearest data point is the Lucefin measurement of 1490 MPa tensile after tempering at 200 °C.
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3 · TEMPERING – LOW BAND (150-400 °C), the highest strength
Step3 · TEMPERING – LOW BAND (150-400 °C), the highest strength​‌​​‌​
SummaryThe service condition in which strength and hardness are kept. It stays BELOW the forbidden band.​‌​​‌​
TemperatureAbout 150-400 °C. Named measurements: Lucefin gives rows at 200, 250, 300, 350 and 400 °C; AZoM gives a row at 204 °C. Carpenter gives no figure for this band and only says the material is tempered to secure the hardness and mechanical properties desired.​‌​​‌​
TimeNo numerical time could be confirmed across four independent sources.​‌​​‌​
CoolingAir.​‌​​‌​
Resulting hardnessAZoM measures 1340 MPa tensile, 1050 MPa yield, 11% elongation and 388 HB at 204 °C. Lucefin measures 1490 MPa tensile and 1210 MPa yield at 200 °C. The two measurements do not give the same number; both are written with their source named.​‌​​‌​

4 · TEMPERING – HIGH BAND (600-780 °C), Condition T and +QT650
Step​‌​​‌​4 · TEMPERING – HIGH BAND (600-780 °C), Condition T and +QT650
Summary​‌​​‌​For toughness and dimensional stability. This band lies ABOVE the forbidden band and is therefore usable.
Temperature​‌​​‌​680-780 °C (Rodacciai, for the +QT650 condition). Lucefin and AZoM give measured rows at 600, 650 and 700 °C.
Time​‌​​‌​No numerical time could be confirmed across four independent sources.
Cooling​‌​​‌​Air.
Resulting hardness​‌​​‌​EN 10088-3 +QT650 (t <= 160 mm): 450 MPa yield min, 650-850 MPa tensile, 12% elongation min. Rodacciai gives 220-280 HB for +QT650 depending on section. Rolled Alloys and Swiss Steel give Condition T as 26-32 HRC; Swiss Steel writes 890-1035 MPa tensile, 760-895 MPa yield, 5% elongation minimum and 27-31 HRC for that condition. AZoM measures 796 MPa tensile, 670 MPa yield, 17.5% elongation and 253 HB at 650 °C.
​‌​​‌​

FORBIDDEN TEMPERING BAND – 400-580 °C (the upper end is 566-600 °C depending on the source)
StepFORBIDDEN TEMPERING BAND – 400-580 °C (the upper end is 566-600 °C depending on the source)​‌​​‌​
What happensIn this band the impact toughness drops and the corrosion resistance falls. In 416 the second effect weighs more, because the corrosion resistance of the grade already sits below that of 410 on account of the sulfur.​‌​​‌​
As named in the sourceCarpenter for 416, 399-566 °C (750-1050 °F): ‘results in decreased impact strength and also reduced corrosion resistance’ · Swiss Steel for 416, 400-600 °C (750-1110 °F): ‘results in reduced corrosion resistance and decreased impact strength’ · AZoM for 416, 400-580 °C: ‘tempering temperatures ranging from 400 to 580 °C should be avoided’ because of poor ductility. On the 410 side of the same family Carpenter gives 399-566 °C, Rolled Alloys 750-1050 °F and West Yorkshire Steel 400-580 °C. Because the sources diverge at the ends, no single figure has been written and the 400-580 °C envelope is used.​‌​​‌​
Mechanism warningThis is NOT the 475 °C EMBRITTLEMENT of ferritic stainless steels. In martensitic 12-14Cr steels the mechanism is temper embrittlement together with chromium carbide precipitation at the grain boundaries. NUMERICAL EVIDENCE (Lucefin, dia. 10 mm, oil quenched from 980 °C): the impact energy falls from 30 J at 250 °C to 19 J at 350 °C, 18 J at 400 °C, 17 J at 450 °C and 18 J at 500 °C, then rises to 31 J at 600 °C and 90 J at 700 °C. The toughness trough sits exactly inside the forbidden band. A SECOND PIECE OF NUMERICAL EVIDENCE FROM THE SAME TABLE: the tensile strength does NOT fall in this band and even rises slightly (1410 MPa at 350 °C against 1450 MPa at 450 °C). That is the trap: a part tempered inside the band measures well for hardness and strength, and what has been lost is toughness and corrosion resistance.​‌​​‌​

Lucefin measurement – 1.4005 / X12CrS13, dia. 10 mm round, oil quenched from 980 °C, then tempered
Title​‌​​‌​Lucefin measurement – 1.4005 / X12CrS13, dia. 10 mm round, oil quenched from 980 °C, then tempered
Reading​‌​​‌​The table is a single measurement series (Lucefin) and is labelled as such; figures from different sources have not been mixed into it. Two things can be read from it. FIRST: the strength barely falls between 200 and 500 °C (1490 down to 1420 MPa); the real drop starts after 550 °C. SECOND: the impact energy falls from 30 J at 250 °C to 17 J at 450 °C and only recovers above 600 °C. Anyone choosing a tempering temperature by hardness alone will read the 400-500 °C band as ‘good’; the table shows the opposite. A CHECK AGAINST ANOTHER SOURCE: the independent AZoM measurement gives 1340 MPa tensile / 1050 MPa yield / 388 HB at 204 °C and 796 MPa tensile / 670 MPa yield / 253 HB at 650 °C. The trend is the same, the numbers are not identical, and NO AVERAGE HAS BEEN TAKEN.
The diagram is schematic; the time axis is NOT to scale. No published TTT/CCT curve was used, so no curve is drawn. THIS ALLOY IS MARTENSITIC: it hardens by quenching and tempering, it does NOT precipitation harden. There is NO ageing step of the H900 / H1025 / H1075 / H1150 type. The cycle has the same shape as that of 410; the sulfur does not change the heat treatment temperatures, it changes the ductility and the corrosion resistance of the result. The heat treatment temperatures are the same as those of 410. The sulfur DOES NOT CHANGE the austenitising or tempering temperature; the sulfide inclusions do not dissolve during heat treatment and remain as they are. There are two separate annealing bands and the sources mix them up: a 650-825 °C process (sub-critical) anneal and an 815-900 °C full anneal. The results differ – Carpenter gives about 187 HB for the first and about 155 HB for the second. Condition T (the condition Rolled Alloys and Swiss Steel give as 26-32 HRC) and the low tempering rows of the Lucefin table ARE NOT THE SAME CONDITION. Condition T is a high temper; the Lucefin 200 °C row is a low temper and gives a far harder material. No source recommends WATER as the quench medium; oil, air and polymer appear. No published TTT/CCT curve could be verified against four sources, so NO CURVE IS DRAWN in this diagram.

​‌​​‌​

The only real advantage of 416 over 410 is machinability; its only real advantage over 303 is THAT IT HARDENS. That is why the heat-treatment section sits at the centre of any decision to buy 416.

Heat Treatment Recipes · 416

​‌​​‌​

Full annealing815–900 °C for half an hour, then cool at 30 °C per hour, followed by air cooling. The European route is lower: 745–825 °C or 750–820 °C, slow furnace cooling. [Conflict] There is a real 75–80 °C split at the UPPER end​‌​​‌​
Sub-critical annealing650–760 °C, air cool. This is the condition in which 416 machines best — the producer’s own statement​‌​​‌​
Hardening (austenitising)925–1010 °C (secondary database) · 950 °C (producer) · 950–1000 °C (two European sources). Three sources converge on the 950–1000 °C band​‌​​‌​
Quench mediumOil preferred, especially in heavy section. Air cooling is possible but costs 1–2 HRC points. DO NOT WATER QUENCH — quench cracking in a martensitic stainless is a real risk​‌​​‌​
Tempering — the usable windowsLow: about 150–400 °C → hardness 388–401 HB, tensile 1340–1405 MPa, low toughness. High: 580–680 °C → hardness 248–321 HB, tensile 796–1000 MPa, acceptable toughness and corrosion resistance. The European route gives 660–780 °C​‌​​‌​
THE FORBIDDEN BAND [conflict]Three sources give three different bands, and all point the same way: 400–580 °C (“low impact resistance”) · 400–600 °C (“corrosion resistance and impact strength are reduced”) · 425–525 °C. Publish the conservative envelope: DO NOT TEMPER between 400 and 600 °C. The intersection of all three (425–525 °C) is absolutely forbidden; at the edges the sources diverge​‌​​‌​
Stress relief — hardened part30–55 °C below the tempering temperature actually used, 4–7 hours, slow cool​‌​​‌​
Stress relief — annealed part595 °C, 4–7 hours, slow cool​‌​​‌​

The term “475 °C embrittlement” is being misused here

One European producer page, writing that 416 must not be tempered between 425 and 525 °C, calls the effect “475 °C embrittlement”. That terminology is wrong and it creates confusion. 475 °C embrittlement is a phenomenon of high-chromium FERRITIC and duplex stainless steels, caused by the demixing of a chromium-rich α′ phase — it is the problem of grades such as 430 and 434. 416 is martensitic, and the effect there is classical TEMPER EMBRITTLEMENT: carbides and impurities segregating to the grain boundaries of tempered martensite. The practical outcome is the same (do not temper in that band) but the mechanism differs, and the name confusion puts a ferritic grade and 416 in the same category. And in 416 that band has a second cost that ferritics do not have: loss of corrosion resistance. Chromium carbide precipitation depletes chromium at the grain boundaries, and in a sulphurised steel the already limited passivity weakens further.​‌​​‌​

Welding — 416 IS NOT WELDED

The heading of this section is not a warning but a conclusion. 416 was not designed to be welded and welding it is not recommended. The producer’s own statement is unambiguous: “similar to any sulphur bearing stainless steel, the welding of 416 should be avoided since the high sulphur content can result in cracking”. A second European producer says the same: “welding is discouraged, especially autogenous methods”.​‌​​‌​

Why — two separate mechanisms operating at once

1. Sulphur-driven hot cracking (solidification cracking). Sulphur concentrates in the last liquid to solidify in the weld pool and forms low-melting sulphide films at the grain boundaries. As the bead contracts those films are still liquid and separate under tensile stress. The result is a longitudinal crack running down the centre of the bead. This cannot be cured by filler selection — the sulphur comes from the base metal.
2. Martensitic hardening and hydrogen cracking. 416 is an air-hardening 13Cr martensitic. The heat-affected zone transforms to hard, brittle, untempered martensite. That is the classic 410 problem, and in 416 it is superimposed on the sulphur embrittlement.
These two mechanisms do not cancel; they multiply. Welding 416 means combining the two worst weldability characteristics in a single material.​‌​​‌​

If Welding Is Unavoidable — Damage Limitation, Not a Solution

Filler metal​‌​​‌​AWS E309 / ER309 (austenitic, high Cr-Ni) — three independent sources give the same recommendation. The European equivalent is 1.4833 (309S). Some sources also mention 410-type low-hydrogen electrodes. The purpose of 309 is to dilute the sulphur and give a ductile austenitic weld metal
Preheat​‌​​‌​200–300 °C, to slow the cooling rate in the heat-affected zone and reduce untempered martensite
Post-weld treatment​‌​​‌​Stress relief at 650–675 °C (secondary database) or tempering at 650 °C (two producers). A third source suggests a more aggressive route: full annealing at about 790 °C, to recover ductility and corrosion resistance
Shielding gas​‌​​‌​Do not use gas containing hydrogen or nitrogen. Hydrogen feeds delayed cracking; nitrogen raises hardness in the heat-affected zone
Post-weld surface​‌​​‌​The weld zone must be mechanically cleaned and passivated. Otherwise it will sit below even the already-limited corrosion resistance of the base metal
The honest advice​‌​​‌​If the part is going to be welded, do not choose 416. The right answers: make the welded part from 410 or 415 and keep 416 for unwelded machined parts; or solve the assembly mechanically (screws, interference fits, brazing). Welding a free-machining steel cancels the reason you chose it

Machining — the Reason 416 Exists​‌​​‌​

There is a very common confusion here, and it has to be cleared up first. Two different “machinability” numbers circulate for 416, and both are correct, because they measure different things.

[Conflict] Two Different Machinability Indices — Do Not Mix Them

​‌​​‌​

AISI relative machinability rating416 = 85 %, the highest among stainless steels. The reference is B1112 free-machining steel = 100 %. This index weighs tool life, chip breaking and achievable surface finish together. It is the figure most often quoted for 416​‌​​‌​
Cutting-speed indexA distributor table comparing cutting SPEED against the same B1112 = 100 % reference: 416 annealed 95 SFM = 54 % · 303 150 SFM = 75 % · 430F 150 SFM = 75 % · 430 110 SFM = 66 % · 420 85 SFM = 50 % · 410 60 SFM = 36 % · 304 70 SFM = 40 % · 316 60 SFM = 36 % · 440C 65 SFM = 40 %​‌​​‌​
Is the conflict real?Yes, and it is explicable. A relative rating of 85 % and a speed index of 54 % are published for the same material. The difference: a martensitic stainless is HARDER than an austenitic grade, so it runs at a lower cutting speed — but it breaks the CHIP far better and wears the tool less. In other words 416 machines more slowly but more predictably than 303. Use the speed index when programming the machine and the relative rating when comparing suppliers​‌​​‌​
416’s constant advantageOn both indices 416 is far above its sulphur-free sibling 410 (54 % against 36 % — roughly 1.5×). That is the real comparison and it is not in dispute​‌​​‌​
Cutting Parameters · 416 (producer data, SFM against B1112)

Turning — cold drawn​‌​​‌​Depth of cut 1 mm · HSS 120–160 SFM (M2–M3) · Carbide 460–900 SFM (C7) · Feed 0.003–0.008 in/rev
Turning — annealed​‌​​‌​Depth of cut 1 mm · HSS 130–170 SFM (M2–M3) · Carbide 505–950 SFM (C7) · Feed 0.003–0.008 in/rev
Form turning / grooving​‌​​‌​Width 2 mm · HSS 120–160 SFM · Carbide 390–550 SFM (C6) · Feed 0.002–0.004 in/rev
Drilling​‌​​‌​Ø1.6 mm · HSS 30–115 SFM (M2) · Carbide 50–250 SFM (C5–C6 / C1–C2) · Feed 0.002–0.005 in/rev
Reaming​‌​​‌​Ø1.6 mm · HSS 30–115 SFM (M2) · Carbide 50–250 SFM (C5–C3) · Feed 0.002–0.005 in/rev
Tapping​‌​​‌​All sizes 20–80 SFM · Tooling M2–M7 or TiN coated
Correction for hardened 416 (HT)​‌​​‌​With HSS, REDUCE speed by 20 % · With carbide, INCREASE speed by 20 %. That opposing correction is surprising but correct: the hardened material is too abrasive for HSS, while for carbide it gives better chip breaking. Drilling speeds are unchanged
Tool coating​‌​​‌​Coated tooling allows a 10–15 % speed increase
Drill point angle​‌​​‌​130–140° points run 10–20 % faster than 118° points
Deep holes​‌​​‌​Beyond 3 diameters deep, reduce speed and feed by 20–40 %
Preferred carbide grade​‌​​‌​C6 or better
In which condition to machine​‌​​‌​The producer states: “416 HT (hardened and tempered) is the optimum condition for machinability” — better alloy distribution and chip control. A secondary source says the sub-critically annealed condition is best. [Conflict] Two sources recommend different conditions — trial it on your own part

Corrosion — Where It Is Good, Where It FAILS​‌​​‌​

COMPARISON
One standard set: the chemistry bands come from EN 10088-3:2005 Table 9 and from the ASTM specifications; the attainable hardness and the weldability come from the manufacturers’ own data sheets. All five grades are MARTENSITIC and none of them precipitation hardens.
​‌​​‌​

GradeUNSW.-Nr.EN designationCarbonChromiumNickelMolybdenumSulphurMaximum hardnessWeldabilityNote
AISI 410S41000​‌​​‌​1.4006X12Cr13​‌​​‌​0.08-0.15%11.5-13.5%​‌​​‌​0.75% max–​‌​​‌​0.030% max38-47 HRC tempered; practical working ceiling about 43-45 HRC​‌​​‌​Conditional – a preheat of 177-204 °C is MANDATORY and a postweld anneal is requiredThe reference grade of the family. Carbon ceiling 0.15%.​‌​​‌​
AISI 415S41500​‌​​‌​1.4313X3CrNiMo13-4​‌​​‌​EN: 0.05% max · ASTM: 0.05% maxEN: 12.0-14.0% · ASTM: 11.5-14.0%​‌​​‌​EN: 3.5-4.5% · ASTM: 3.5-5.5%EN: 0.30-0.70% · ASTM: 0.50-1.00%​‌​​‌​EN: 0.015% max · ASTM: 0.030% max+QT900: 285-346 HB, about 30-37 HRC. THE LOWEST ATTAINABLE HARDNESS IN THE FAMILY.​‌​​‌​GOOD – 100-160 °C preheat, 580-620 °C postweld temper, ER410NiMo filler. THE ONLY GENUINELY WELDABLE GRADE IN THE FAMILY.Soft martensitic. Bought for toughness and welding, not for hardness. The only grade with a specification impact floor.​‌​​‌​
AISI 416S41600​‌​​‌​1.4005X12CrS13​‌​​‌​EN: 0.06-0.15% · ASTM: 0.15% max12.0-14.0%​‌​​‌​–0.60% max​‌​​‌​0.15-0.35% (EN 10088-3) – ADDED ON PURPOSE26-32 HRC in Condition T (Rolled Alloys, Swiss Steel); at a low temper Lucefin measures 1490 MPa tensile at 200 °C​‌​​‌​NOT SUITABLE – the sulfur forms MnS inclusions and causes hot cracking410 plus sulfur. Corrosion resistance and weldability have been given up for machinability.​‌​​‌​
AISI 431S43100​‌​​‌​1.4057X17CrNi16-2​‌​​‌​EN: 0.12-0.22% · ASTM: 0.20% max15.0-17.0% – THE HIGHEST CHROMIUM IN THE FAMILY​‌​​‌​EN: 1.50-2.50% · ASTM: 1.25-2.50%–​‌​​‌​0.030% maxWorking hardness 32-47 HRC (Abrams); 1345 MPa tensile / 388 HB tempered at 204 °C (AZoM), 1580 MPa at 200 °C (Lucefin)​‌​​‌​Difficult – needs a 200-300 °C preheat and a postweld treatment at about 650 °C; corrosion resistance falls after weldingThe highest corrosion resistance among the hardenable martensitics. The nickel is what stops 16% chromium making the structure ferritic.​‌​​‌​
AISI 440CS44004​‌​​‌​1.4125X105CrMo17​‌​​‌​0.95-1.20% – THE HIGHEST CARBON IN THE FAMILY16.0-18.0%​‌​​‌​–EN: 0.40-0.80% (THERE IS A FLOOR) · ASTM: 0.75% max (NO FLOOR)​‌​​‌​0.030% max (EN 10088-3) / 0.015% max (Lucefin, Abrams)59-62 HRC as quenched; 60 HRC tempered at 150-175 °C; 61-62 HRC with refrigeration at -73 °C (Carpenter). THE HIGHEST IN THE FAMILY AND AMONG STANDARD STAINLESS STEELS.​‌​​‌​Not welded in practice – it needs a 260 °C preheat and a 6-8 hour anneal at 732-760 °CA bearing and cutting grade. The 1% carbon ties chromium up as carbide; not all of the 16-18% Cr on paper works for corrosion resistance.​‌​​‌​

Additional information
Inverse relationship​‌​​‌​As the carbon rises the attainable hardness rises and the toughness and weldability fall. The ladder is plain: 415 (0.05% C) is welded and stops at 30-37 HRC; 410 (0.15% C) is welded conditionally and reaches 43-45 HRC; 431 (0.12-0.22% C) is welded with difficulty and reaches 47 HRC; 440C (0.95-1.20% C) is not welded and reaches 60 HRC. 416 sits outside that ladder: its carbon is the same as 410’s and what separates it is the sulfur.
Nikelin isi​‌​​‌​410, 416 and 440C carry no nickel; 415 carries 3.5-5.5% and 431 carries 1.25-2.50%. In those two grades the nickel does two different jobs. In 415 it makes the structure transform to martensite even though the carbon is very low (it would otherwise stay ferritic). In 431 it stops 16% chromium making the structure ferritic. The same element, for two different reasons.
Kukurdun isi​‌​​‌​Sulfur is present ON PURPOSE only in 416: EN 10088-3 specifies a band of 0.15-0.35%. In the other four grades sulfur is an IMPURITY and is capped (0.015-0.030% max). The same element is a product feature in one grade and a defect in the others.
Cokelme uyarisi​‌​​‌​NONE OF THE FIVE GRADES PRECIPITATION HARDENS. Ageing steps such as H900, H1025, H1075 and H1150 belong to PRECIPITATION HARDENING grades such as 17-4 PH, 15-5 PH, 13-8 PH and Custom 455, and have no counterpart in any of these five. Here the condition names are +QT650, +QT780, +QT900 or, on the ASTM side, Condition A / T / H.
The comparison rests on the EN 10088-3 and ASTM texts for the chemistry bands and on manufacturers’ data sheets for the hardness; figures from different test methods have not been gathered into one row. Because the ASTM and EN bands for 415 differ, both are written out separately in that row; the same applies to the carbon and molybdenum rows of 416, 431 and 440C. The molybdenum row for 440C is the most important trap in this table: EN 1.4125 specifies a FLOOR for molybdenum (0.40%), while ASTM S44004 gives only a CEILING (0.75%). A 440C bought against ASTM may contain almost no molybdenum. The carbon row for 431 is the second trap: EN 1.4057 sets a carbon FLOOR (0.12%), ASTM S43100 does not (only the 0.20% ceiling).

​‌​​‌​

The honest opening sentence: a European producer’s own datasheet for 1.4005 says that it is “probably the least resistant to corrosion of all of the stainless steel grades”. That was not written by a competitor; it was written by the company that makes the material. Opening a 416 sale with that sentence prevents most of the complaints that come later.

The mechanism: why an MnS inclusion starts a pit​‌​​‌​

The protection of a stainless steel is the chromium oxide passive film on the surface. That film only works while it is continuous. MnS inclusions break that continuity in three separate ways:
1. Physical discontinuity. Over an inclusion the passive film is either absent or very weak. For a chloride ion that is a direct point of entry.
2. The inclusion itself dissolves. MnS dissolves at a lower potential than the surrounding matrix. When it does, it leaves a micro pit — that is, a crevice. Inside that crevice chloride concentrates and pH falls.
3. The dissolution products acidify the local environment. Sulphur species (sulphide, thiosulphate) go into solution and prevent repassivation. Once a pit opens it feeds itself and does not close.
The result: the pitting resistance of 416 is measurably lower than sulphur-free 410 at the same chromium level, and the difference does not show up in the chemical analysis table. Sulphur is a corrosion variable, not just a manufacturing variable.

Where 416 IS good​‌​​‌​

Fresh water, steam, dry air. Indoor atmospheric conditions including high humidity.
Many petroleum products. Oil, fuel, hydraulic fluid — as long as they carry no chloride and no water.
Soaps, solvents, mould atmospheres, many organic acids.
Weak alkalis.
In which condition is corrosion resistance best? The producer states that the 416 HT condition (27–31 HRC) is the optimum for both machinability and corrosion resistance. The reason is that in the correct tempering window carbides precipitate finely and dispersed rather than at grain boundaries.
Surface treatment is decisive. For 416 passivation is not optional but effectively mandatory: per ASTM A380, 20–50 % nitric acid plus 2–6 wt % sodium dichromate, 25–40 minutes at 20–50 °C. Free iron smeared onto the surface during machining and exposed sulphides are removed by this step. Unpassivated 416 behaves markedly worse than passivated 416.

Where 416 FAILS — read this list before quoting​‌​​‌​

1. Chlorides and seawater. An absolute exclusion. Salt spray, marine atmosphere, chlorinated water, road salt. Producer pages put “NaCl saline mist” and “seawater” on the restricted list — which in practice means “do not use”. For marine service there are 316, F53 and F55.
2. Crevice geometries. The producer warns explicitly: “avoid crevice designs”. Under gaskets, threaded joints, interference fits, under deposits. 416 already has microscopic crevices (dissolved MnS voids); adding a macroscopic one compounds the problem.
3. Acids. Nitric, phosphoric, sulphuric and acetic acid are all on the restricted list.
4. Welding. See the welding section above. A welded 416 part carries both cracking and corrosion risk.
5. Parts tempered between 400 and 600 °C. That band lowers both impact resistance and corrosion resistance. Here the heat-treatment records matter as much as the material certificate.
6. Roughly machined, unpassivated surfaces. A rough surface, exposed MnS and free iron all accelerate corrosion. The producer’s advice: “maintain smooth, contamination-free surfaces”.
7. Food and pharmaceutical contact surfaces. A sulphurised steel pits quickly against cleaning chemicals — especially chlorinated disinfectants — and a pit is a bacterial refuge that cannot be cleaned. Those applications use 316L.
8. Sour service (H₂S). 416 is not accepted for sour service under NACE MR0175. For sulphide stress cracking, a sulphurised and hardened martensitic is the worst possible combination. If you need a sour-service 13Cr, that is 415.
9. Deep drawing and heavy cold forming. Not corrosion but a mechanical limit: MnS inclusions initiate cracks. 416 can be bent but not deep drawn.
10. Cryogenic and low-temperature impact service. No verified low-temperature toughness data could be found for a sulphurised martensitic, and the microstructure is not suited to it. If there is a low-temperature impact requirement, do not quote 416.

Frequently Asked Questions​‌​​‌​

We make our parts from 303 but they need to be a bit harder. Can we switch to 416?

Technically yes — and this is exactly the reason 416 exists. But you lose three things, and none of them comes back.
What you gain is clear: 303 is austenitic and cannot be hardened by heat treatment — outside of cold work there is no way to raise its strength. 416 is martensitic: quenched it reaches 41–43 HRC and tempering sets it wherever you want. The typical working point is Condition T, 27–31 HRC, tensile 890–1035 MPa. Far above cold-drawn 303.
The first thing you lose is corrosion resistance. 303 is an 18Cr-8Ni austenitic; 416 is a 13Cr martensitic. Five points less chromium and no nickel at all. A producer writes on its own 1.4005 datasheet that it is “probably the least resistant to corrosion of all of the stainless steel grades“. If your part sits in a damp environment, gets washed with cleaning chemicals, or occasionally meets salt water, this switch will be visible in the field.
The second is magnetic response. 303 is effectively non-magnetic (it picks some up from cold work). 416 is ferromagnetic in every condition. If the part sits near a sensor, passes through a magnetic separator, or needs MR compatibility, that alone is grounds for exclusion. Conversely, if you run magnetic fixturing on the assembly line, it may be an advantage.
The third is cutting speed. Published speed tables give 303 about 150 SFM and 416 about 95 SFM — so your cycle time goes up. Even though 416’s relative machinability rating (85 %) is higher than 303’s (78 %), that rating also measures tool life and chip breaking; in raw speed, 303 is faster. Cost the machine hours in.
And a fourth point that gets forgotten: switching to 416 means you are also buying a heat treatment step. Hardening, tempering, probably straightening, and certainly passivation. Add those to the part price; the price per kilo of the material is misleading.​‌​​‌​

Our datasheet says 416 is “the most machinable stainless” but 303 runs faster on our machines. Which is right?

Both are right, and the confusion comes from two different indices being published with the same percent sign.
Index one: the AISI relative machinability rating. Reference B1112 free-machining steel = 100 %. This rating weighs tool life, chip-breaking behaviour and achievable surface finish together. On that scale 416 = 85 % is first among stainless steels and 303 = 78 % is second.
Index two: the cutting-speed index. Same B1112 = 100 % reference, but it measures only the applicable cutting speed. On that scale 416 annealed is 95 SFM (54 %) and 303 is 150 SFM (75 %). 303 is clearly faster.
Not a contradiction — physics. 416 is martensitic and harder; hard material is cut at lower speed. But 416 breaks the chip far better, galls less, wears the tool less and is more dimensionally stable. 303 is austenitic: it runs fast but work hardens, produces stringy chips and builds up edge on the tool.
Practical consequence: on short, simple parts 303 gives the faster cycle. On long, multi-operation, tight-tolerance, unattended work, 416 is more predictable and cheaper overall — because there are fewer tool changes, fewer chip jams and less dimensional drift. The right comparison is not parts per hour but good parts per shift.
And remember: on both indices 416 is roughly 1.5× better than its sulphur-free sibling 410. 416’s true benchmark is not 303 but 410.​‌​​‌​

The customer wants us to weld a 416 part. “Just a small tack weld,” he says. Should we?

No — and put the reason in writing, because the liability comes back to you later.
The welding problem in 416 is not a skill problem; it is a metallurgy problem. Two mechanisms operate simultaneously.
The first is sulphur-driven hot cracking. Sulphur concentrates in the last liquid to solidify in the weld pool and leaves low-melting sulphide films at the grain boundaries. The bead contracts as it cools; those films are still liquid and separate under tensile stress. This cannot be fixed by filler metal — the sulphur comes from the base metal and mixes into the pool. A tack weld does not remove the problem; it merely makes the crack smaller and invisible.
The second is martensitic hardening. 416 is an air-hardening 13Cr steel. The narrow band around the tack transforms to untempered, hard and brittle martensite. If hydrogen is present (damp electrode, oily surface, moisture in the shielding gas) delayed cracking arrives days later.
The third is corrosion, and it is usually overlooked. The weld and the heat-affected zone lose what passivity they had. Even if the part looks sound right after welding, the first corrosion will start in that band.
If you are forced into it, damage limitation: filler E309 / ER309 (European equivalent 1.4833), preheat 200–300 °C, shielding gas free of hydrogen and nitrogen, post-weld stress relief at 650–675 °C or full annealing at about 790 °C, followed by mechanical cleaning and passivation of the weld zone. But that is damage control, not a procedure.
The right engineering answer: do not make a welded part from 416. Either solve the assembly mechanically (screws, pins, interference fits, brazing), or make the component that gets welded from 410 or 415, or look for a sulphur-free free-machining alternative. Welding a free-machining steel cancels every reason you had for choosing it.​‌​​‌​

Our 416 parts started rusting six months after assembly. Did we get the wrong material?

Most likely the material was right and a step in the process was skipped. There are four things to check, in order.
1. Were the parts passivated? For 416, passivation is not optional. During machining, free iron is transferred onto the surface from tooling, machine ways and chip conveyors, and the cut also exposes MnS inclusions at the surface. Both start rusting when they meet moisture. The correct treatment is 20–50 % nitric acid plus 2–6 wt % sodium dichromate, 25–40 minutes at 20–50 °C, per ASTM A380. Unpassivated 416 rusts within six months — that is expected behaviour, not a defect.
2. What is the surface roughness? A roughly machined surface means more exposed inclusions and more micro-crevices. The producer’s advice is explicit: “maintain smooth, contamination-free surfaces, avoid crevice designs”.
3. What was the tempering temperature? If the part was tempered between 400 and 600 °C, its corrosion resistance has been reduced, even if nobody intended it. That band damages both impact resistance and passivity. Ask your heat treater for the furnace record. It can be more informative than the material certificate.
4. Is the environment actually the one you expected? 416 is fine in fresh water, steam, dry air and most petroleum products. If chloride is present — salt spray, road salt, chlorinated cleaner, perspiration — 416 was the wrong grade from the start. Six months is a realistic life for 416 in a chloride environment.
What to do: in the short term, re-passivate the parts and reduce the surface roughness. In the long term, if there is chloride in the environment, change grade: 303 if there is no hardness requirement, 415 or 17-4 PH if there is. You cannot make 416 chloride-resistant by passivating it; passivation only lets the material reach its own limit.​‌​​‌​

Common datasheet errors — check these before you place an order

1. The EN equivalent is printed as 1.4401 — WRONG. A widely mirrored producer datasheet lists the specification as “ISO/EN 10088-3 (1.4401/1.4005)”. 1.4401 is 316, an entirely different material (austenitic, 17Cr-11Ni-2Mo). The only EN counterpart of 416 is 1.4005 / X12CrS13.
2. Thermal conductivity is given in impossible units. One distributor page prints “171.8 Btu·ft/ft²·hr·°F” for 416. That is above the conductivity of silver and is impossible. The unit was most likely meant to be Btu·in/ft²·hr·°F. The correct magnitude is 25–30 W/m·K.
3. The annealed row pairs 517 MPa tensile with 262 HB hardness. 262 HB corresponds to roughly 900 MPa tensile, not 517 MPa. In that row the hardness is a CEILING and the tensile is a TYPICAL value. Do not read them as one material condition.
4. Sulphur is written as an upper limit. In the ASTM/AISI definition S ≥0.15 % is a MINIMUM — a guaranteed floor. Some pages write it as “S max 0.15”. That inverts what the material is. EN 1.4005 by contrast gives both limits: 0.15–0.35 %.
5. The carbon minimum is forgotten. ASTM S41600 has NO carbon minimum (only ≤0.15 %); EN 1.4005 HAS one (0.08–0.15 %). For a part that will be hardened this difference is decisive: a heat of S41600 at 0.06 % C conforms and will not reach the expected hardness. For hardened work, ask for dual certification to 1.4005.
6. The term “475 °C embrittlement” is used for 416. A European producer page names the 425–525 °C forbidden band that way. 475 °C embrittlement is a phenomenon of FERRITIC and duplex stainless steels (α′ demixing). The effect in 416 is TEMPER EMBRITTLEMENT. Same practical outcome (do not temper in that band), different mechanism.
7. The forbidden tempering band is given three different ways. 400–580 °C, 400–600 °C and 425–525 °C. Publish the conservative envelope: 400–600 °C. The intersection of all three, 425–525 °C, is absolutely forbidden.
8. “Highest machinability” is confused with cutting speed. On the relative rating scale 416 = 85 % (first among stainless steels). On the cutting-speed scale 416 = 54 % and 303 = 75 %. They measure different things and both are correct. Use the speed index when programming the machine.
9. Molybdenum is shown as if it were part of the composition. Mo ≤0.60 % is a PRODUCER OPTION, not a mandatory alloying element. Unless it is explicitly required in the order, its presence cannot be guaranteed — and do not base a corrosion calculation on it.
10. “416 plate to ASTM A240” gets quoted. S41600 is not in the A240 grade list. A single source cites ASTM A895 for free-machining stainless flat product, but that could not be independently verified. In practice 416 flat product is sold to mill specification in limited sizes.
11. Two different property sets circulate for the hardened condition. ASTM A582 typical: 758/586 MPa, 248–302 HB; producer band: 890–1035 / 760–895 MPa, 27–31 HRC. The gap is not small. State in the purchase order which set you are buying.
12. 416 and 416Se are treated as the same thing. 416Se (S41623) is selenium-bearing and differs from sulphurised 416: better cold forming and hot working, higher surface quality, higher price and harder to source. Do not order them under the same part number.​‌​​‌​

Related grades​‌​​‌​

AISI 420  ·  AISI 420B  ·  AISI 420C  ·  AISI 431  ·  Martensitic steels →

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