UNS S40500 · W.Nr. 1.4002 · X6CrAl13 · ~13% Cr – 0.10-0.30% Al. This is a FERRITIC stainless steel: it does NOT harden by heat treatment, it gains no strength from quenching and it does NOT precipitation harden – there is NO H900 / H1025 type ageing step. ASTM S40500 (SSINA, BSSA, Penn Stainless): C 0.08% max – Mn 1.00% max – Si 1.00% max – P 0.040% max – S 0.030% max – Cr 11.5-14.5% – Ni 0.50% max (Penn Stainless; SSINA gives 0.6%) – Al 0.10-0.30% – balance Fe. EN 10088 for 1.4002 (worldstainless): C 0.08% max – Si 1.00% max – Mn 1.00% max – P 0.040% max – S 0.015% max – Cr 12.0-14.0% – Al 0.10-0.30% – balance Fe. THE TWO STANDARDS ARE NOT THE SAME: the chromium band is 11.5-14.5% in ASTM and 12.0-14.0% in EN, and the sulfur ceiling is lower in EN. The aluminium band of 0.10-0.30% is the same in four independent sources (SSINA, worldstainless, BSSA, Penn Stainless).
Bought for 12-13% chromium fabrications that are welded and then cannot be annealed. Penn Stainless describes the grade as ‘designed to be used in the as-welded condition’ and lists steam nozzles, partitions, annealing boxes and ‘fabrications that cannot be annealed after welding’.
Forms
Round bar, flat bar, plate, sheet, pipe, forging. All forms are supplied to order.
Standards
AMS: NONE. The AMS column of the Type 405 (S40500) row in the SSINA type/specification table is EMPTY. ASTM (the full list from the SSINA Type 405 row): A240 / A240M (plate, sheet, strip) · A268 (seamless and welded ferritic tubing) · A276 (bars and shapes) · A473 (forgings) · A479 / A479M (bars for boilers and pressure vessels) · A511 (seamless mechanical tubing) · A580 (wire) · A1012 (condenser tubes). ASME: SA-240 · SA-268 · SA-479. EN: 1.4002 · EN 10088-2 (flat products) · EN 10088-3 (long products). SAE type number: 51405. Military: QQ-S-763. THE AMS 5504 TRAP: AMS 5504 DOES NOT BELONG TO THIS ALLOY. In the SSINA specification table AMS 5504 appears on the Type 410 row; the AMS list for Type 410 is 5350, 5504, 5505, 5591, 5613, 5776, 5777 and 5876.
Advantage
It can be used on parts that are welded and then cannot be annealed. The aluminium band of 0.10-0.30% is the same in four independent sources (SSINA, worldstainless, BSSA, Penn Stainless).
Welding
Welding is the reason this grade exists. The SSINA welding handbook gives a columbium (niobium) stabilised filler metal for Type 405 and states that columbium additions reduce intergranular precipitation. Preheat: 150-230 °C (300-450 °F) for sections of roughly 6 mm (1/4 inch) and heavier;
Limits
1) IT DOES NOT HARDEN BY HEAT TREATMENT and its strength is the lowest in the family: ASTM minima of 170 MPa yield / 415 MPa tensile (SSINA, Penn Stainless). If strength is wanted, this is the wrong grade. 2) THE CHROMIUM IS LOW: 11.5-14.5% (ASTM) or 12.0-14.0% (EN).
Compiled from manufacturer data sheets · confirm against the current specification before ordering
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What AISI 405 IsStandards by Product FormASME Code AcceptanceProduct Forms With NO StandardChemical CompositionMechanical PropertiesPhysical PropertiesHeat Treatment and Thermal StabilityWeldingMachining and FormingCorrosionHonest ComparisonFrequently Asked QuestionsCommon Datasheet Errors and Traps
Corrosion resistance: AISI 405 stainless steel is a ferritic stainless steel with improved welding properties, formulated for primary forming into corrosion resistant wrought products. Its corrosion resistance is moderate.
Weldability: The aluminium content of the alloy reduces the tendency to harden adjacent to the weld bead, which minimises susceptibility to cracking. Its suitability for welding is good.
Machinability: It has a fairly high thermal conductivity among the wrought ferritic stainless steels. In addition it has a fairly low embodied energy and a moderately low base cost. Its properties are suited to the annealed condition. Machinability is moderate.
Heat treatment: It is a 12% chromium steel designed to be used in the as-welded condition. Unlike other 12% chromium steels it does not harden excessively on air cooling. Although AISI 405 is chosen for applications requiring greater high temperature capability and greater resistance to oxidation, it is generally more expensive than AISI 430 because of its higher cost.
Applications: Application areas are generally annealing boxes, steam nozzles, quenching racks, partitions and other fabrications. It cannot be annealed after welding.
1.4002 is an excellent choice for applications requiring high temperature capability and resistance to oxidation. It has limitations in terms of corrosion resistance, however, so austenitic steels may be preferred if the material is to be used in aggressive chemical environments.
Round bar · Flat bar · Plate · Sheet · Tube · Forgings All forms are supplied to order.
What AISI 405 Is — and Why the Aluminium Is There
AISI 405 (UNS S40500 / W.Nr. 1.4002 / DIN X6CrAl13) is a ferritic stainless steel: nominally 12–13 % chromium, low carbon, and — the entire reason the alloy exists — 0.10–0.30 % aluminium. It carries no nickel (the ASTM ceiling is ≤0.60 %), it is magnetic, and it cannot be hardened by heat treatment.
The only way to understand 405 is to understand what goes wrong with 410. A steel at about 12–13 % chromium transforms partly to austenite at high temperature. On cooling, that austenite transforms to martensite — so the part hardens and embrittles without anyone asking it to. In welding this happens exactly in the heat-affected zone: the narrow band beside the fusion line goes above 1000 °C, cools in air, and is left as hard, crack-prone martensite. That is what happens when 410 is welded, and it is why welded 410 fabrication demands preheat and post-weld annealing.
The 405 solution is to shift the chemistry so that austenite cannot form at all.Aluminium is a strong ferrite former — like chromium, silicon and molybdenum it widens the ferrite field. A small addition of 0.10–0.30 % effectively closes the austenite field in a steel of about 12–13 % chromium. No austenite on heating means no martensite on cooling. The result, in the producer’s own words: “Unlike other grades in the 12 % chromium category, 405 is not susceptible to extensive hardening through air cooling from high temperature.” That is the commercial reason 405 exists, in one sentence: it is the 12Cr stainless made for parts that cannot be annealed after welding.
Where 405 Sits in the Family · Honest Positioning (from the ASTM A240 table)
DEFENCE METAL
405 (S40500 / 1.4002)
Ferritic. C ≤0.08 % · Cr 11.5–14.5 % · Ni ≤0.60 % · Al 0.10–0.30 %. A240 minima: tensile ≥415 MPa, yield ≥170 MPa, elongation ≥20 %, hardness ≤179 HBW / ≤88 HRB. Not hardenable. Weldable without mandatory post-weld heat treatment. The aluminium does not pay for this in toughness or corrosion resistance — that price comes from being a 12Cr ferritic in the first place
410 (S41000)
Martensitic. C 0.08–0.15 % · Cr 11.5–13.5 % · Ni ≤0.75 %. Annealed A240 minima: tensile ≥450 MPa, yield ≥205 MPa, elongation ≥20 %, ≤217 HBW / ≤96 HRB. Hardenable — that is its entire purpose. The price: martensite in the weld, mandatory preheat and post-weld annealing. See our 410 page
409 (S40910)
Ferritic, titanium-stabilised. C ≤0.030 % · Cr 10.5–11.7 % · Ni ≤0.50 % · N ≤0.030 % · Ti: 6×(C+N) min, 0.50 % max · Cb ≤0.17 %. A240 minima: tensile ≥380 MPa, yield ≥170 MPa, elongation ≥20 %, ≤179 HBW. It solves the same problem a different way: it defeats martensite not with aluminium but by dropping the carbon and tying it up with titanium. It is the standard automotive exhaust material; its chromium is lower than 405’s
430 (S43000)
Ferritic, higher chromium. C ≤0.12 % · Cr 16.0–18.0 % · Ni ≤0.75 %. A240 minima: tensile ≥450 MPa, yield ≥205 MPa, elongation ≥22 %, ≤183 HBW / ≤89 HRB. Its corrosion resistance is markedly better than 405’s (four more points of chromium), but it is unstabilised: it carries a risk of HAZ martensite and intergranular attack when welded. See our 430 page
How to read that table: the difference between 405 and 410 is not only aluminium — the carbon differs too. The carbon of 410 is a BAND, 0.08–0.15 %: 410 must contain carbon, because it needs it to harden. In 405 carbon is only a ceiling (≤0.08 %). Aluminium and low carbon work together: one narrows the austenite field, the other lowers the hardenability of whatever little austenite does form.
Standards by Product Form
STANDARDS BY PRODUCT FORM
DEFENCE METAL
Product form
Standards
Plate, sheet, strip (THE MAIN ROUTE)
THERE IS NO AMS. ASTM A240 / A240M · ASME SA-240 · EN 10088-2 (1.4002)
Round bar, flat bar (sections)
THERE IS NO AMS. ASTM A276 (bars and shapes) · ASTM A479 / A479M (bars for boilers and pressure vessels) · ASME SA-479 · EN 10088-3 (1.4002)
Pipe and tubing
THERE IS NO AMS. ASTM A268 (seamless and welded ferritic tubing) · ASTM A511 (seamless mechanical tubing) · ASTM A1012 (condenser tubes) · ASME SA-268. These numbers come from the SSINA Type 405 row; no second independent source was found.
Forgings
THERE IS NO AMS. ASTM A473 (forgings). SSINA is the single source.
Wire
THERE IS NO AMS. ASTM A580 (wire). SSINA is the single source.
AMS numbers come FIRST and ASTM numbers after them; this grade has no AMS number, so the ASTM numbers are given directly. The whole ASTM list comes from a single source (the Type 405 row of the SSINA specification handbook). The buyer should verify the relevant ASTM text before an order is written. That AMS 5504 belongs to 410 was read from the AMS list on the Type 410 row of the SSINA table (5350 5504 5505 5591 5613 5776 5777 5876).
Next to the austenitics, 405 has narrow specification coverage. Plate, bar and tube are covered solidly; on the pipe, fitting, flange and fastener side there are real gaps, and quoting without knowing them is risky.
Standards by Product Form · AISI 405 (S40500 / 1.4002)
DEFENCE METAL
Plate · sheet · strip (pressure vessel)
ASTM A240 / ASME SA-240 Type 405 — the strongest verified coverage
Bar · shapes · wire
ASTM A276 (bars and shapes) · ASTM A580 (wire)
Tube (seamless and welded)
ASTM A268 / ASME SA-268 Gr. TP405 — the general service specification for ferritic and martensitic stainless tubing
Forgings
ASTM A473
Single-source additional specifications
Publisher pages also cite A176 (general flat product), A314 (billets and bars for forging), A479 (bars for boilers and pressure vessels) and A511 (seamless mechanical tubing). Their coverage of S40500 could not be independently verified in this study — confirm before ordering
ASME Section IX
Base metal P-No. 7 (ferritic stainless). The same group holds SA-240 Types 405, 409 and 410S and SA-240 Type 430
Europe
EN 10088-2 · 1.4002 X6CrAl13
Other national
JIS SUS405 (JIS G3463) · BS 405S17 · SAE 51405 · QQ-S-763 — from single-source lists, verification limited
ASME Code Acceptance
The code status of 405 is not published as clearly as that of the austenitics, and this section has to be honest about it.
ASME · What Is Known and What Is Not, for 405
DEFENCE METAL
Accepted specifications
405 is a code material under SA-240 (plate, sheet, strip) and SA-268 (tube)
ASME Section IX group
P-No. 7 — ferritic stainless steels
Maximum code temperatures
A numerical ASME maximum use temperature for 405 could not be independently verified in this study.Publish no number; read it from the current Section II Part D table for your project
Producer service limits
Published as producer guidance, not code: continuous 704 °C (1300 °F), intermittent 816 °C (1500 °F). A second publisher gives the maximum operating temperature in air as 705 °C — the two sources agree
Corrosion temperature
An independent database gives a maximum corrosion temperature of 390 °C. It is single-source, but the gap against the mechanical limit (820 °C) is meaningful: 405 stays standing when hot, but its corrosion resistance runs out far earlier
Product Forms With NO Standard — the Commercially Valuable Section
This is where the real sales knowledge for 405 lives. Buyers think of 405 as if it were an austenitic and ask for every product form; the coverage is narrow.
S40500 · Specification Gaps
DEFENCE METAL
Pipe
No dedicated ASTM pipe specification for 405 could be verified. A312 is austenitic pipe; A268 is a TUBE specification. The honest answer to a request for “405 pipe to ASTM” is: chemistry to A240/A268, dimensions and mechanicals by agreement
Fittings · flanges
Coverage of 405 by A403 (austenitic fittings) or A182 (flanges and forged fittings) could not be verified. The verified forging specification is A473, and that is a general forging specification, not a flange standard. A 405 flange is made from A473 forging to the buyer’s drawing — say so in the quotation
Bolting · fasteners
There is NO dedicated ASTM bolting specification for 405, and there is no reason for one: 405 cannot be hardened, so no high-strength fastener can be made from it. For 12Cr fasteners the right address is 410 or 416
Welding consumables
There is no such product as “405 welding wire”, and there should not be. Producer practice is explicit: 405 Cb electrodes are used — fillers containing COLUMBIUM (niobium) instead of aluminium, to control hardening. In practice austenitic fillers (309, 310, 312) are also widely used
Castings
No cast equivalent of 405 could be verified. Cast 12Cr grades sit in the martensitic CA class and do not carry the weldability advantage of 405. Do not expect a standard product called a “405 casting”
Aerospace (AMS) · NACE
An AMS specification for 405 and a NACE MR0175 / ISO 15156 listing could not be verified in this study.Make no commitments on either heading
Chemical Composition
ASTM A240 / ASME SA-240 — weight %
S40500 (Type 405): C ≤0.08 · Mn ≤1.00 · P ≤0.040 · S ≤0.030 · Si ≤1.00 · Cr 11.5–14.5 · Ni ≤0.60 · Al 0.10–0.30 · Fe balance.
What Actually Matters on the Certificate
DEFENCE METAL
Aluminium — the one distinguishing element
0.10–0.30 %.The lower limit of that band matters as much as the upper one: a heat at Al 0.08 % is not 405 and its ferrite stability is not guaranteed. When verifying in the field by PMI, ask whether aluminium is actually being measured — most handheld XRF instruments do not read light elements reliably, and an instrument that cannot see aluminium cannot tell 405 from 410
Nickel — [CONFLICT]
ASTM A240: ≤0.60 % · many publishers and the ASME SA-268 route print ≤0.50 %. Both are real — they are different product form specifications. A heat at Ni 0.55 % passes A240 and fails A268. Check the certificate against the document the customer ordered, not the grade name
Sulphur
ASTM: ≤0.030 % · EN 1.4002: ≤0.015 %. EN is tighter by exactly a factor of two. A heat at S 0.022 % passes ASTM and fails EN
EN 1.4002 chromium band
The full chromium and aluminium band for EN 1.4002 could not be independently verified in this study. The only verified divergence is the sulphur ceiling. Publish no numbers for the EN band; read them from the EN 10088-2 table
Carbon
≤0.08 %. Do not confuse this with the 0.08–0.15 % BAND of 410: in 410 carbon comes with a mandatory lower limit, in 405 it is only a ceiling. A heat at C 0.07 % can satisfy both the 405 and the 410 chemistry; what makes it 405 is the aluminium
Mechanical Properties
STRENGTH VALUES
DEFENCE METAL
Condition
Hardness
Yield MPa
Tensile MPa
Elongation
ASTM · S40500 · annealed – specification minimum
–
170
415
20%
EN 10088-2 · 1.4002 · annealed (cold rolled strip, hot rolled strip and plate)
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 table values are given in SEPARATE rows and must not be mixed. None of the mechanical figures for 405 reached four independent sources; the number of sources is stated on each row. The gap is recorded in the ‘skipped’ list. No HRC figure is given: annealed 405 sits below the Rockwell C measuring range, and the sources state hardness in HB or HRB.
The minima CHANGE WITH PRODUCT FORM — this is the most common error
There is no single “yield value” for 405. The same grade carries different minima depending on which specification it was ordered to:
405 · Minimum Mechanical Properties by Specification
Yield 170 against 205 MPa and hardness 179 against 207 HB. This is not a contradiction: tube production has a different cold-work history and the specification is written accordingly. But a datasheet that puts the two numbers side by side without saying which product form it means will mislead the reader
Typical values — three sources, three different numbers [CONFLICT]
The published typical values for 405 are inconsistent between sources, and showing that is more honest than hiding it. Three data sets in circulation for the annealed condition:
That is a 38 % spread on yield, between 200 and 276 MPa. Source C’s range approach is the honest one. Design to the SPECIFICATION MINIMUM, not to typical values (170 MPa for A240, 205 MPa for A268). Use typical values only as an expectation, never as an acceptance criterion
Toughness — the quiet limit on 405
The real weakness of ferritic stainless steels is not strength but TOUGHNESS. Unlike the austenitic structure, the ferritic structure shows a ductile-to-brittle transition temperature (DBTT): below a certain temperature the material fails in a brittle manner. Austenitic 316 still carries 88–134 J of impact energy at cryogenic temperatures, while ferritics fall far below that under their transition temperature.
Let us be honest: no numerical DBTT or Charpy table for 405 could be independently verified in this study, so we publish no number. But the qualitative rule is established practice and the engineering conclusion is clear: ferritic stainless steels are used in thin sections. As the section thickens, both stress triaxiality and weld grain coarsening increase, and together they push the transition temperature up. For a thick, notched pressure part that may take impact at low temperature, 405 is the wrong material. Any thickness limit must come from the specification you order to and the customer’s impact testing requirement — do not invent a millimetre figure.
Physical Properties
The physical properties of 405 differ sharply from those of austenitic stainless, and the differences affect design directly. The ferritic structure is far closer to carbon steel than to the austenitics.
AISI 405 · Physical Properties
DEFENCE METAL
Density — [CONFLICT]
Published values: 7.70 · 7.75 · 7.80 g/cm³. The spread is 1.3 %, negligible for a weight calculation, but know that all three are in circulation
Modulus of elasticity — [CONFLICT]
200 GPa (three sources) · 190 GPa (one source). The majority is at 200 GPa
Thermal conductivity (0–100 °C)
27.0 W/(m·K) (two sources) · 30 W/(m·K) (one source). The critical comparison: the thermal conductivity of 316 is 14.6 W/(m·K). So 405 conducts heat roughly twice as well — this is the real advantage of ferritics in heat exchangers and heat transfer duty
Thermal expansion (0–100 °C)
10.8 × 10⁻⁶ /K (one source gives 11). The critical comparison: 316 runs 16.6 × 10⁻⁶ /K. 405 expands about a third less and its expansion is close to that of carbon steel — a large advantage for parts welded to, or bolted into, carbon steel structures
Specific heat
0.11 Btu/lb·°F (32–212 °F) · one source gives 480 J/(kg·K)
Melting range
1480–1530 °C (solidus 1480, liquidus 1530)
Electrical conductivity
2.9 % IACS (single source). A resistivity value could not be independently verified
Magnetic behaviour
IT IS FERRITIC — IT IS MAGNETIC. That is not a defect, it is the definition. A numerical magnetic permeability could not be verified in this study, but a magnet sticks, and 405 cannot be used in magnetic separation systems, MR environments or any equipment sensitive to magnetic fields
Service temperature (producer)
In air, continuous 704 °C · intermittent 816 °C. An independent database gives a maximum mechanical temperature of 820 °C and a maximum corrosion temperature of 390 °C
Heat Treatment and Thermal Stability
HEAT TREATMENT — SCHEMATIC
DEFENCE METAL
1 · BEFORE WELDING – PREHEAT
Step
1 · BEFORE WELDING – PREHEAT
Summary
Applied on heavy sections, undesirable on thin ones.
Temperature
150-230 °C (300-450 °F) for sections of roughly 6 mm (1/4 inch) and heavier. SSINA welding handbook, for ferritic stainless steels. SINGLE SOURCE.
Time
No source was found.
Cooling
–
Resulting hardness
SSINA: preheating is usually UNDESIRABLE for sections thinner than 6 mm in low-carbon or stabilised grades.
DEFENCE METAL
2 · WELDING – THE STAGE THAT SETS 405 APART
Step
2 · WELDING – THE STAGE THAT SETS 405 APART
Summary
The aluminium prevents hardening on air cooling from high temperature, so the part can be used as welded.
Temperature
Filler metal: columbium (niobium) stabilised (SSINA). This is not a separate temperature stage.
Time
–
Cooling
Air. Penn Stainless: ‘Unlike the other grades of 12% chromium stainless, 405 is not vulnerable to extensive hardening through air cooling from high temperatures.’
Resulting hardness
No hardness increase is expected after welding; this is why 405 is used in fabrications that cannot be annealed after welding (Penn Stainless, SSINA – 2 sources).
DEFENCE METAL
3 · POST-WELD ANNEALING (where it can be applied)
Step
3 · POST-WELD ANNEALING (where it can be applied)
Summary
Relieves embrittlement in the heat affected zone. It does NOT refine the grain. It is not mandatory for 405.
Temperature
788 °C (1450 °F) – SSINA welding handbook, for ferritics. For 1.4016 of the same family, Aalco and worldstainless give 790-815 °C and DEW gives 750-850 °C. The only figure SPECIFIC TO 405 is the SSINA one.
Time
No numerical time could be confirmed against four independent sources.
Cooling
The 566-399 °C (1050-750 °F) band must be passed QUICKLY; SSINA asks for spray quenching or rapid cooling.
Resulting hardness
worldstainless: the anneal reduces embrittlement but does not refine grain structure.
DEFENCE METAL
4 · FORBIDDEN BAND – 475 °C EMBRITTLEMENT
Step
4 · FORBIDDEN BAND – 475 °C EMBRITTLEMENT
Summary
The band is neither used as a service temperature nor passed slowly on cooling.
Temperature
Roughly 400-550 °C. Aalco 400-600 °C and 540-400 °C · worldstainless the same two bands · SSINA 566-399 °C · IMOA 300-525 °C for alpha prime. FOUR INDEPENDENT SOURCES; THE FIGURES HAVE NOT BEEN MERGED.
Time
Prolonged exposure is required (Aalco, worldstainless).
Cooling
Slow cooling through this band is FORBIDDEN.
Resulting hardness
Room temperature toughness falls. It is reversed by annealing (Aalco, worldstainless).
DEFENCE METAL
5 · THERE IS NO HARDENING STAGE
Step
5 · THERE IS NO HARDENING STAGE
Summary
This grade has NO austenitise + quench + temper cycle and NO precipitation hardening.
Temperature
–
Time
–
Cooling
–
Resulting hardness
Penn Stainless states that 405 is not vulnerable to extensive hardening on air cooling from high temperatures; BSSA describes ferritics as a non-hardenable family; SSINA describes 405 as the grade chosen when better weldability than 410 is wanted.
The diagram is schematic; the time axis is NOT TO SCALE. No curve has been drawn because no published TTT/CCT curve was used. THIS ALLOY IS FERRITIC: it does not harden by heat treatment, it gains no strength from quenching and it does NOT precipitation harden. There is NO austenitising, quenching or tempering stage. An annealing temperature SPECIFIC TO 405 could not be confirmed against four independent sources; each stage below states which figure is specific to 405 and which is given for the ferritic family. THERE IS NO AGEING in this grade. Steps such as H900, H1025, H1075 and H1150 belong to precipitation hardening alloys and do not apply to 405. No annealing temperature band SPECIFIC TO 405 could be found in four independent sources, so no separate annealing stage has been opened in the diagram and only the post-weld anneal is given. The gap is recorded in the ‘skipped’ list. The preheat and post-weld annealing temperatures come from the SSINA welding handbook and are given for the ferritic stainless family; where a stage rests on a single source, that is stated on the stage.
One real operation: annealing
405 cannot be hardened by heat treatment. The ferritic structure does not transform to martensite; preventing exactly that is the whole purpose of the aluminium. The operation applied is annealing, and its aim is not hardness but ductility and the removal of internal stress.
405 · Heat Treatment Parameters
DEFENCE METAL
Annealing — [CONFLICT]
649–760 °C (1200–1400 °F), air cool — two independent sources give this band. A third publisher writes 700–800 °C. 649–760 °C is the better supported figure; the 700–800 °C band is closer to the general post-weld annealing practice for ferritics (750–800 °C) and has probably migrated from there
Cooling
In air. The entire point of 405 is that air cooling is harmless — no quench is needed and air cooling does not harden it
Forging
Published practice: soak at 1500–1600 °F, then raise rapidly to 1900–2050 °F. The critical warning is the publisher’s own sentence: “Do not remain at this temperature as the result will be excessive grain growth.” In a ferritic structure grain coarsening is irreversible and permanently lowers toughness
Post-weld annealing
The same cycle: soak at 1500–1600 °F, then 1900–2050 °F. “Post weld annealing will maximize ductility.” — but it is NOT MANDATORY for 405, which is the reason the alloy exists
“Hardening” — [CONFLICT]
The same datasheets both say “this alloy does not respond appreciably to heat treatment” and publish a cycle of 982–1010 °C (1800–1850 °F) followed by an oil quench. That is an internal contradiction. The metallurgical reading: with aluminium at the bottom of its band and carbon at the top, some austenite can form and a little hardening can be seen — but this is not a design method. Do not sell 405 as a hardenable material
Stress relief
One publisher gives 150–300 °C — single source
The damaging phase windows — and HOW MUCH 405 is actually exposed to them
Two classic embrittlement mechanisms are published for ferritic stainless steels. Both depend on chromium, and 405 sits at the BOTTOM of the band. This is the distinction datasheets miss most often when they copy and paste.
475 °C Embrittlement and Sigma Phase · The Real Risk for 405
DEFENCE METAL
475 °C embrittlement (885 °F brittleness) — [CONFLICT]
Three different published bands: 399–566 °C (750–1050 °F) · 250–550 °C · 375–525 °C. Mechanism: precipitation of a chromium-rich phase (α’), producing a sharp drop in toughness. The common intersection of the three bands is roughly 400–525 °C, and that is what should be used in practice
Sigma phase
Published band: long holds at 550–800 °C form the hard, brittle σ intermetallic. BUT: the literature’s own statement is that “above 25 % Cr the sigma phase may appear for relatively long times at temperature“, and sigma risk is highlighted “in the higher chromium alloys such as 444 or 26-1“. 405 carries 11.5–14.5 % chromium — so sigma is NOT a primary risk for 405
The honest reading for 405
This is not a direct quotation but an engineering judgement drawn from the low chromium level: both α’ and σ formation accelerate with chromium content. In a ferritic at 12–13 % Cr, both are far weaker than in 430 at 17 % Cr or in the 26 % Cr grades. The dominant embrittlement mechanism for 405 is not either phase — it is GRAIN COARSENING IN THE WELD. Say so when you put a 475 °C warning on the datasheet
The rule nevertheless
Do not put 405 into long-term service in the 400–550 °C band, and keep the interpass temperature outside it. The risk is low, not zero
Welding
The entire commercial value of 405 lives here, so this section has to be detailed. 405 is welded by shielded fusion and resistance methods. Oxyacetylene welding is not suitable.
405 Welding · Rules and Parameters
DEFENCE METAL
The difference from 410 — one sentence
“Unlike other grades in the 12 % chromium category, 405 is not susceptible to extensive hardening through air cooling from high temperature.” When 410 is welded, the HAZ forms hard martensite and preheat plus post-weld annealing are required. In 405 the aluminium prevents that transformation from the start — post-weld annealing improves ductility but is not mandatory
Filler metal — critical
405 Cb electrodes: in the producer’s own words, “405 Cb electrodes that contain columbium rather than aluminum to control hardening” are used. Why: aluminium oxidises readily under the arc and does not survive reliably in the weld pool; columbium (niobium) is both a ferrite former and a carbide former and it is not lost in arc transfer. Do not look for an “aluminium-bearing 405 filler”
The austenitic filler alternative
For ferritics, 309, 310 and 312 austenitic fillers are common. The gain: a ductile, tough weld metal with low cracking risk. The price: the weld metal and the parent metal now differ in corrosion behaviour and thermal expansion — the austenitic deposit expands about 1.5× as much as the parent metal and accumulates stress at the bead under cyclic thermal loading. Decide by whether the application can tolerate that
The real problem: grain coarsening
405 does not form martensite in welding, but it DOES coarsen the grain in the HAZ, and that is irreversible. The rule: low heat input, narrow beads, fast travel. In heavy sections, multi-pass welding reheats the HAZ repeatedly and grows the grain — that is the true reason 405 is a thin-section material
Preheat
The general published practice for ferritic stainless steels: preheat of 150–230 °C (300–450 °F) is recommended when thickness exceeds about 6 mm (¼ in). This was not verified as MANDATORY for 405 — since 405 does not form martensite, the justification is weaker than for 410; but it is reasonable in heavy sections and restrained joints
Interpass temperature
Do not let it run high. Two reasons: grain coarsening, and time spent in the 475 °C embrittlement band (roughly 400–525 °C)
Post-weld heat treatment
NOT MANDATORY for 405 — that is the reason the alloy exists. If it is wanted: for low-chromium ferritics, post-weld heating at 788–843 °C (1450–1550 °F)assures a wholly ferritic structure, and cooling down to no lower than 593 °C (1100 °F) is recommended to minimise distortion
Welding to carbon steel
The thermal expansion of 405 is close to that of carbon steel — a real, measurable advantage over the austenitics in dissimilar joints: less stress accumulates at the bead under cyclic thermal loading
Machining and Forming
Unlike the austenitics, 405 is an easy material to machine. The reason is directly microstructural: the ferritic structure does not work-harden as the austenitic structure does, its thermal conductivity is roughly twice as high (heat does not build up in the tool), and the chip breaks more readily.
405 · Machining and Forming
DEFENCE METAL
General behaviour
The producer’s own words: “Soft and ductile, 405 can be easily machined” and it “machines similarly to 4130 alloy steel“. That second sentence is directly usable for a machine shop: if you have 4130 parameters, that is your starting point
Cutting speed · feed
No verified numerical cutting speed / feed table for 405 was found in this study.Do not publish invented numbers. Practical approach: start from 4130 parameters and do not use austenitic stainless parameters — they are needlessly slow for 405
Forming
“405 can be easily spun, drawn and formed using common forming procedures.” Compared with the austenitics there is less springback and lower forming force — the work-hardening exponent of ferritics is low
Caution in forming
The ferritic structure has limited elongation (A240 minimum 20 %; austenitic 316 gives 40 %). Do not expect austenitic behaviour from 405 in deep drawing; reduce the draw ratio accordingly
Surface finish
12Cr ferritic surfaces do not take or hold the bright finish of the austenitics; decorative work is not the job of 405. For a decorative ferritic, 430 is the right address
Corrosion — Where It Works, Where It FAILS
COMPARISON
One consistent set of standards: the ASTM composition bands come from the SSINA and BSSA type tables, the EN 10088 bands from the worldstainless table and the producer data sheets (Rodacciai, Lucefin, DEW, thyssenkrupp, Aalco); hardening behaviour, weldability and machinability come from the producers’ own data sheets. ALL FOUR GRADES BELONG TO THE FERRITIC FAMILY: none of them precipitation hardens and none has an H900 / H1025 type ageing step. The single exception is 1.4104, written as the EN counterpart of 430F; that number is classed martensitic in EN 10088-3 and can be quenched and tempered.
DEFENCE METAL
Grade
UNS
W.-Nr.
EN designation
Carbon
Chromium
Molybdenum
Aluminium
Sulphur
Sertlesme
Weldability
Note
AISI 405
S40500
1.4002
X6CrAl13
ASTM: 0.08% max · EN: 0.08% max
ASTM: 11.5-14.5% · EN: 12.0-14.0% – THE LOWEST CHROMIUM IN THE FAMILY
–
0.10-0.30% – THE ONLY GRADE IN THIS FAMILY THAT CARRIES ALUMINIUM
ASTM: 0.030% max · EN: 0.015% max
Does not harden by heat treatment. The aluminium prevents hardening on air cooling from high temperature (Penn Stainless).
THE GRADE OF THIS FAMILY DESIGNED FOR WELDING. It is used in the as-welded condition in fabrications that cannot be annealed after welding (Penn Stainless, SSINA).
ASTM minimum 170 MPa yield / 415 MPa tensile (SSINA, Penn Stainless) – the lowest strength floor in the family.
AISI 430
S43000
1.4016
X6Cr17
ASTM: 0.12% max · EN: 0.08% max – THE TWO STANDARDS DIFFER
16.0-18.0%
ASTM: not specified (Ulbrich type analysis 0.50% max) · EN: not specified
–
ASTM: 0.030% max · EN 10088-3: 0.030% max · EN 10088-2: 0.015% max
Does not harden by heat treatment (Ulbrich ‘Heat Treatable: No’; Penn Stainless ‘non-hardenable grade’; worldstainless ‘not thermally hardenable’).
Conditional. Preheat 150-200 °C and post-weld annealing at 790-815 °C are recommended (Aalco, worldstainless); DEW does not recommend arc welding and asks for heat input below 1 kJ/mm.
The reference grade of the family and the only member with AMS numbers (AMS 5503 sheet/strip/plate, AMS 5627 bar/wire/forgings).
AISI 430F
S43020
1.4104 (X14CrMoS17) and 1.4105 (X6CrMoS17) – BOTH ARE QUOTED, THEY ARE NOT THE SAME
X14CrMoS17 / X6CrMoS17
ASTM S43020: 0.12% max (no floor) · EN 1.4104: 0.10-0.17% (THERE IS A FLOOR) · EN 1.4105: 0.08% max
ASTM: 16.0-18.0% · EN 1.4104: 15.5-17.5%
ASTM: 0.60% max · EN 1.4104: 0.20-0.60%
–
ASTM: 0.15% min · EN 1.4104: 0.15-0.35% – ADDED DELIBERATELY
ASTM 430F (S43020) is ferritic and does not harden by heat treatment. EN 1.4104 sits in the martensitic class: 950-1070 °C quench plus 550-650 °C temper (DEW, Lucefin, Rodacciai, ABRAMS).
NOT SUITABLE. DEW states it is ‘not welded except by resistance or friction welding’; ABRAMS states welding is ‘generally not recommended’; Lucefin rates weldability ‘difficult’; BSSA describes the weldability of free-machining grades as ‘more limited’.
430 with sulfur. Weldability and chloride resistance were given up for machinability.
AISI 434
S43400
1.4113
X6CrMo17-1
ASTM: 0.12% max · EN: 0.08% max
16.0-18.0% – THE SAME AS 430
ASTM: 0.75-1.25% · EN: 0.90-1.40% – THE ONLY GRADE IN THIS FAMILY WITH A MOLYBDENUM FLOOR
–
ASTM: 0.030% max · EN 10088-3: 0.030% max · EN 10088-2: 0.015% max
Does not harden by heat treatment (Ulbrich).
The same limits as 430. Filler metal and preheat figures specific to 434 could not be confirmed against four sources; the SSINA welding handbook states that austenitic filler metal is used for 434.
Molybdenum is the only thing that separates it from 430. Ulbrich states the molybdenum addition ‘enhances corrosion resistance and resistance to deicing chemicals’; SSINA describes 434 as the grade specified ‘when better corrosion resistance is required’.
The table compares only the bands taken from standard texts and producer data sheets; NO laboratory corrosion test comparison has been made. No corrosion diagram has been produced because data from more than one independent laboratory for the same medium and the same exposure time could not be found. Molybdenum is the only compositional difference between 430 and 434; sulfur is the one thing that decides the difference between 430 and 430F; what separates 405 from the rest of the family is both its lower chromium and its aluminium. The ASTM and EN carbon ceilings are not the same for these grades. Confusing the ASTM 0.12% ceiling with the EN 0.08% ceiling makes an order bring the wrong material.
Realistic positioning
The honest sentence is this: 405 is a marginal stainless steel. In the publisher’s own words, “AISI Type 405 / 1.4002 stainless steel has marginal stainless steel corrosion resistance” and it is “resistant only to mild atmospheric and fresh water“. The reason is simple: corrosion resistance comes from chromium, and in 405 the chromium is only 11.5–14.5 % — below the 16–18 % of 316 and below the 16–18 % of 430. Aluminium contributes nothing to corrosion resistance; its role is metallurgical.
405 · Where It Works
DEFENCE METAL
Nitric acid
Resistant. A ferritic structure with no molybdenum behaves well in oxidising acids. This is precisely the inverse of the weakness that molybdenum-bearing austenitics (316) show in nitric acid
Organic acids
Resistant (published general statement)
Alkalis
Resistant
Mild atmosphere · fresh water
It works. This is the real service envelope of 405
High-temperature oxidation
In air, continuous 704 °C, intermittent 816 °C. A 12Cr ferritic shows reasonable resistance to scaling
CHLORIDE STRESS CORROSION CRACKING (SCC)
This is the strongest card 405 holds, and it is usually under-emphasised.Ferritic stainless steels show very strong resistance to SCC compared with the austenitics, despite carrying no nickel — or more precisely, because they carry none. Austenitic 316 cracks in 4–24 hours in the boiling 42 % MgCl₂ test, while the ferritic structure is structurally closed to that mechanism. If you are looking for a replacement material for a 304/316 item that has failed by SCC in hot chloride service, the ferritic class is a serious candidate
WHERE IT FAILS
Do Not Specify 405 For
DEFENCE METAL
Sulphuric acid
It does not hold. It is explicitly among the media listed as attacking it
Hydrochloric acid
It does not hold. No concentration is suitable
Hydrofluoric acid
It does not hold
Phosphoric acid
It does not hold. Note the contrast: in the same medium 316L runs <0.01 mm/yr in boiling 20 % phosphoric — the gap is enormous
Seawater
It does not hold. There is nothing to discuss for 405; chloride immersion is impossible at 12 % Cr
General chloride (pitting)
Weak. 405 resists chloride SCC but does NOT resist PITTING and CREVICE corrosion. Do not confuse the two mechanisms — the ferritic advantage exists only in SCC
Heavy section · low-temperature impact
Toughness is limited. The ductile-to-brittle transition and weld grain coarsening work together. 405 is a thin-section material
Anywhere high strength is needed
It cannot be hardened. The A240 yield minimum is 170 MPa. For high-strength 12Cr, use 410 or the martensitic grades
Decorative surfaces
It does not give the surface quality of the austenitics
Magnetic-field sensitivity
405 is magnetic. If a non-magnetic material is required, the ferritic class is eliminated at the outset
Honest Comparison — 405, 410, 409 or 430
Four 400-Series Grades · Whose Job Is Whose
DEFENCE METAL
Choose 405
A thin-section 12Cr part that will be welded, cannot be annealed afterwards, and has modest corrosion demands. The classic examples as published: annealing boxes, steam nozzles, quenching racks, partitions and fabrications that cannot be annealed after welding. 12Cr internals and linings are common in refineries and process plants; a specific standard reference for the share 405 takes in that duty could not be verified in this study, but the rationale is the same: no opportunity to anneal after welding
Choose 410
When strength and hardness are needed. It is martensitic and hardenable; even annealed, its yield minimum beats 405 (205 against 170 MPa). The price is welding: HAZ martensite, preheat and post-weld annealing. If you specify 410 for welded fabrication, budget for the heat treatment
Choose 409
When a titanium-stabilised ferritic is what you need — especially automotive exhaust and similar welded, thermally cycled applications. Its carbon at ≤0.030 % is far below 405’s and titanium ties it up. But its chromium is lower (10.5–11.7 %), so its corrosion resistance is below even 405’s. Its tensile minimum is also lower (380 MPa)
Choose 430
When you want to stay ferritic but need more corrosion resistance. Cr 16.0–18.0 % — four to five points above 405. It is also mechanically superior: tensile ≥450 MPa, yield ≥205 MPa, elongation ≥22 %. The price: it is unstabilised and its carbon is higher (≤0.12 %), so you lose the welding advantage of 405. The higher chromium also raises the 475 °C embrittlement and sigma risk relative to 405. See our 430 page
If none of them fits
If the corrosion demand is beyond a 12–18 Cr ferritic, move to an austenitic: 304 (no chloride), 316 (chloride present). But if there is a chloride SCC risk, moving to an austenitic is a STEP BACKWARD — in that case either stay ferritic or look at duplex: F53 · F55
Frequently Asked Questions
What exactly is the difference between 405 and 410?
There are two differences, and both serve the same purpose: avoiding martensite.The first is aluminium. 405 contains 0.10–0.30 % Al; 410 contains none. Aluminium is a ferrite former: it suppresses austenite formation at high temperature, and if no austenite forms, no martensite forms on cooling. The second is carbon. The carbon of 410 is a mandatory BAND of 0.08–0.15 % — 410 has to want carbon, because its hardenability comes from it. In 405 carbon is only a ceiling (≤0.08 %) and lower is preferred. The practical consequence: 410 hardens when air-cooled from high temperature and leaves hard, crack-prone martensite in the weld HAZ, which is why welded 410 fabrication demands preheat and post-weld annealing. 405 does not — in the producer’s words, “unlike other grades in the 12 % chromium category, 405 is not susceptible to extensive hardening through air cooling from high temperature“. The price is strength: 410 can be hardened, 405 cannot, and its annealed yield minimum is 170 MPa instead of 205 MPa. Decision rule: if the part needs hardness, 410; if the part will be welded and cannot be annealed, 405.
Is 405 magnetic? Was stainless steel not supposed to be non-magnetic?
405 is magnetic, and that is not a defect but the definition of its class. The sentence “stainless steel is non-magnetic” applies only to the austenitic stainless steels and only in the annealed condition. Stainless steel splits into four main families and three of them are magnetic: ferritic (405, 409, 430), martensitic (410, 420, 440C) and duplex. Only the austenitic family (304, 316, 321) is practically non-magnetic when annealed — and even that is conditional, because cold deformation and the delta ferrite in weld metal raise permeability. Magnetism is a consequence of CRYSTAL STRUCTURE, not of chromium or of stainlessness: the body-centred cubic structure of ferrite is ferromagnetic, the face-centred cubic structure of austenite is not. So the test “a magnet stuck to it, therefore it is not stainless” is metallurgically wrong, and on ferritic grades such as 405 it is completely misleading. But the converse warning is also needed: in any application sensitive to magnetic fields, 405 is eliminated from the start.
Do I have to anneal 405 after welding?
No — and that is the entire reason the alloy exists. 405 was developed for “fabrications that cannot be annealed after welding”, and the published application list says exactly that. Because aluminium prevents HAZ martensite, the mandatory justification that exists for 410 does not exist for 405. But there are two nuances.(1) Post-weld annealing maximises ductility — so while it is not mandatory, calling it useless would also be wrong. It can be worth considering after forming or on heavily restrained joints. The published cycle is soak at 1500–1600 °F, then raise rapidly to 1900–2050 °F; for low-chromium ferritics it is separately published that heating at 788–843 °C (1450–1550 °F)assures a wholly ferritic structure and that cooling should stop no lower than 593 °C to control distortion. (2) The real welding problem in 405 is not martensite but grain coarsening in the HAZ, and annealing does not reverse it. The only defence against grain coarsening is procedural: low heat input, narrow beads, fast travel, single pass where possible. That is the one thing post-weld annealing cannot fix.
How good is the corrosion resistance of 405, really?
Low. The publisher’s own words are “marginal stainless steel corrosion resistance” and “resistant only to mild atmospheric and fresh water“. Even so, many distributor pages claim “good corrosion resistance” for 405 — because it is easy to copy a 12Cr page from a 304 page. The truth: corrosion resistance comes from chromium, and in 405 chromium is 11.5–14.5 %. Where it works: nitric acid, organic acids, alkalis, mild atmosphere, fresh water and oxidation in air up to 704 °C. Where it ends: sulphuric, hydrochloric, hydrofluoric and phosphoric acid, and seawater. But in one area 405 beats the austenitics outright:chloride stress corrosion cracking. The ferritic structure is structurally closed to that mechanism, whereas austenitic 316 cracks in 4–24 hours in boiling magnesium chloride. So writing 405 off as a “bad stainless” is also wrong: it has a narrow but real envelope, and inside that envelope it is cheap, weldable and immune to SCC.
Common Datasheet Errors and Traps
1) Classifying 405 as “martensitic”. There are supplier pages in the market whose product title reads “Martensitic Stainless Steel Tube S40500”. 405 IS FERRITIC; the sole purpose of the aluminium is to prevent martensite from forming. This error comes from mistaking 405 for 410 and it sets up the welding procedure wrongly from the start.
2) Publishing a hardening cycle. The same datasheets both say “this alloy does not respond appreciably to heat treatment” and print a cycle of 982–1010 °C plus an oil quench. That is an internal contradiction and it leads buyers to expect hardness from 405. 405 cannot be hardened.
3) Misstating the role of aluminium. One widely circulated page gives the role of aluminium as “preventing grain growth during welding“. That is wrong. Aluminium is a ferrite former; by narrowing the austenite field it prevents martensite. Grain coarsening is still a problem in 405 and aluminium does not solve it.
4) Quoting the nickel ceiling as a single number.ASTM A240: Ni ≤0.60 % · the SA-268 route: ≤0.50 %. A heat at Ni 0.55 % passes one and fails the other. The number is unusable unless the governing document is stated.
5) Giving the yield without the product form.A240 (plate): 170 MPa · SA-268 (tube): 205 MPa. Hardness likewise: ≤179 HB against ≤207 HB. This is not a contradiction but a product form difference — although unstated, it looks like one and wrecks the calculation.
6) Copying the thermal expansion from an austenitic datasheet. Some 405 pages give expansion as 9.2 (68–212 °F) and 20.5 (68–1832 °F). 9.2 × 10⁻⁶ in/in/°F ≈ 16.6 × 10⁻⁶ /K, and that is the value for AUSTENITIC 316. The published figure for ferritic 405 is 10.8 × 10⁻⁶ /K — nearly a third lower. This is a copy-paste error that directly corrupts a design.
7) Printing numbers without units. One published 405 page gives thermal conductivity as “416” with no unit at all (most probably Btu·in/hr·ft²·°F). Never pass on a number without its unit. The verified value is 27 W/(m·K) (one source gives 30).
8) Carrying the 475 °C and sigma warnings over blindly. Those warnings were written for high-chromium ferritics (430, 444, 26-1). The literature’s own threshold for sigma is above 25 % Cr; 405 carries 11.5–14.5 %. Print the warning, but print the level with it — the dominant embrittlement mechanism for 405 is not these phases but grain coarsening in the weld.
9) Giving the 475 °C band as a single range. Three different bands are published: 399–566 °C, 250–550 °C, 375–525 °C. The common intersection is roughly 400–525 °C. A page that shows only one band has not seen the other two.
10) The phrase “good corrosion resistance”. The producer’s own words are “marginal” and “only mild atmospheric and fresh water”. A page claiming good corrosion resistance for 405 has most likely carried its text over from a 304 page.
11) Calling the filler “405”. The correct consumable is 405Cb — the electrode containing columbium instead of aluminium. Aluminium oxidises under the arc and does not survive in the pool. In practice 309 / 310 / 312 austenitic fillers are also used, in which case the weld metal expands about 1.5× as much as the parent metal and that must be allowed for under cyclic loading.
12) Contradictory annealing temperatures. Two independent sources give 649–760 °C, a third gives 700–800 °C. The first band is better supported; the second has most likely migrated from the general post-weld annealing practice for ferritics (750–800 °C).
13) Publishing typical mechanicals as single numbers. The two data sets in circulation give yields of 276 MPa and 200 MPa — a 38 % spread. Tensile: 448 and 470 MPa. Hardness: 131 HB and 170 HB. Design to the specification minimum, not to typical values.
14) Hiding the density and modulus conflicts. Density appears as 7.70 / 7.75 / 7.80 g/cm³ and the modulus of elasticity as 200 GPa (three sources) and 190 GPa (one source). The majority sits at 200 GPa; footnote the difference.
15) Lumping all chloride resistance under one heading. 405 resists chloride SCC but does not resist chloride pitting and crevice corrosion. A page that merges the two mechanisms into one line will show 405 as either better or worse than it is. The ferritic advantage exists only in SCC.