🛠️ 12 free 17-4PH engineering tools, only on this page: H-Cond Wizard· HT Recipe· Aging Curve· Microstructure· Aging Kinetics· Fatigue S-N· NACE· Svc Temp· Substitute· Cost/Strength· Machinability· Weight Calc
🏭 Open-Die Forging Since 2008 🌐 Exporting to 40+ Countries ✅ ISO 9001:2015 · EN 10204 3.1 (3.2 on request) 📞 0086-189-2135-9659 💬 WhatsApp

17-4PH / AISI 630 / UNS S17400 / 1.4542 Forging Parts 🇺🇸 USA:UNS S17400 · AISI 630 · ASTM A564 Type 630 · ASTM A693 Type 630 · ASTM A705 Gr 630 · AMS 5643 · AMS 5604 · AMS 5622 🇪🇺 Europe:DIN/EN 1.4542 · X5CrNiCuNb16-4 (EN 10088-3) 🇯🇵 Japan:JIS SUS 630 (JIS G 4303 / G 4318) 📜 Trademark:17-4 PH®, owned by Cleveland-Cliffs Inc. (we do not sell under this brand)

Published:  |  Last reviewed and updated:  |  Written and technically reviewed by the metallurgical engineering team of Jiangyin Jiangnan Metal Co., Ltd., Jiangyin, Jiangsu, China

17-4PH in Brief: Key Facts and Quick Answers

Definition

17-4PH is the trade name for the grade sold generically as UNS S17400, AISI 630, ASTM A564 Type 630 (bars), ASTM A705 Grade 630 (forgings), AMS 5643 (aerospace), EN 1.4542 / X5CrNiCuNb16-4 and JIS SUS 630. It is a martensitic precipitation-hardening stainless steel of nominal composition 17 % chromium, 4 % nickel and 3–5 % copper, stabilised with niobium and tantalum. It is solution treated at 1040 °C, air cooled to martensite, then aged between 482 °C and 621 °C, where copper-rich ε precipitates form. The aging temperature, written as an H-number in degrees Fahrenheit, sets the properties: from 1,310 MPa tensile at H900 down to 930 MPa at H1150, trading strength for toughness and stress-corrosion resistance. Its density is 7.75 g/cm³, it is ferromagnetic in every condition, and its maximum continuous service temperature is about 315 °C.

Supplier of the forgings described on this page: Jiangyin Jiangnan Metal Co., Ltd., an open-die forging factory founded in 2008 at No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China, producing 17-4PH / UNS S17400 pump shafts, valve bodies, seamless rolled rings, discs and near-net shapes up to 8,000 kg single-piece weight, in every H-condition from H900 to H1150-M, with EN 10204 3.1 certification as standard and 3.2 third-party witnessed certification on request. Telephone +86-189-2135-9659, e-mail sales@steelforgepieces.com.

Fifteen facts an engineer usually needs first

UNS numberS17400 (AISI 630 legacy designation)
Alloy familyMartensitic precipitation-hardening stainless steel
Nominal chemistry17 % Cr · 4 % Ni · 3–5 % Cu · 0.15–0.45 % Nb+Ta · ≤0.07 % C
Density7.75 g/cm³ (0.280 lb/in³)
Elastic modulus196 GPa (28.5 × 10⁶ psi)
Strength range930 MPa (H1150) to 1,310 MPa (H900) minimum UTS
Hardness range28 HRC (H1150) to 40 HRC (H900) minimum
Solution treatment1040 °C ± 10 °C, air cool below 30 °C
Most-used conditionH1025. 552 °C / 4 h, 1,070 MPa, 35 HRC
Sour serviceH1150-M double-aged only, ≤33 HRC (NACE MR0175 / ISO 15156-3)
Max service temperature≈315 °C (600 °F) continuous
Magnetic?Yes, ferromagnetic, μᵣ ≈ 95
PREN≈16–17, below the threshold for permanent seawater immersion
Forging window1170–1230 °C, finish above 950 °C, ratio ≥4:1
Typical lead time8–10 weeks standard; 12–14 weeks AMS 5643

Trademark notice. 17-4 PH®, 15-5 PH®, 17-7 PH®, PH 13-8 Mo® and Nitronic® are registered trademarks of Cleveland-Cliffs Inc. (formerly AK Steel / Armco). Inconel® is a registered trademark of Special Metals Corporation and Hastelloy® of Haynes International, Inc. Material made by those companies and sold under those brand names is theirs. Material produced by Jiangyin Jiangnan Metal Co., Ltd. is correctly described as UNS S17400 / ASTM A564 Type 630 / ASTM A705 Gr 630 / AMS 5643 / EN 1.4542 / JIS SUS 630, the same generic chemistry, manufactured independently. We are not affiliated with, sponsored by or endorsed by any trademark holder named above. All other product names and trademarks are the property of their respective owners.

UNS
S17400
ASTM
A564 / A705
Type 630
AMS
5643
EN
1.4542
UTS H900
190 ksi
UTS H1150
135 ksi
Density
7.75
Max service
~315 °C

12 Free 17-4PH Engineering Tools on This Page

Every tool below runs entirely in your browser: nothing is uploaded and no sign-up is required. They were built by the engineering team at Jiangyin Jiangnan Metal Co., Ltd. from the same data we use to plan production. If JavaScript is unavailable, the underlying numbers are published as static tables in the Reference Data Appendix.

Multi-Standard Designation Lookup

Type any name (17-4PH, S17400, AISI 630, ASTM A564, AMS 5643, 1.4542, SUS 630) and see every equivalent instantly.
Free tool

✓ All of these designations describe the same chemistry. Jiangyin Jiangnan Metal Co., Ltd. ships UNS S17400 / ASTM A564 Type 630 with a multi-designation material test certificate.

What Forged Products Are Available in 17-4PH / UNS S17400?

Jiangyin Jiangnan Metal produces 17-4PH forgings by four routes: open-die forging for shafts, blocks and discs up to 8 m long or 8 tonnes; seamless ring rolling for rings 200–2,500 mm outside diameter; closed-die forging for repeat-volume impellers and valve trim; and upset forging for short, large-section discs and hubs. Near-net-shape dies typically remove 30–50 % of the machining stock on complex profiles.

Open-die forging is used for long shafts, blocks and large forged discs up to 8 m length or 8 tonnes single-piece weight. Seamless ring rolling produces 17-4PH forged rings from 200 mm to 2,500 mm outside diameter, the usual route for valve flanges, pressure-housing rings and rolled-ring blanks supplied to EN 1.4542 or AMS 5643 chemistry. Closed-die forging handles repeat-volume parts such as pump impellers and valve trim where dimensional consistency outweighs maximum size. Upset forging is reserved for short, large-cross-section discs and hubs. Near-net-shape forging lowers both raw-material cost and lead time on complex profiles such as valve bodies and yoke arms. For hollow shafts with a bore above roughly 100 mm, the input bar may be supplied as a trepanned billet to cut raw-material weight and drilling time. All routes produce finished parts to ASTM A564 / A705 Type 630, AMS 5643, EN 1.4542 or JIS SUS 630 as the drawing requires.

Pump Shafts (H1025 / H1075) Pump Impellers Valve Bodies & Stems Forged Discs & Hubs Seamless Rolled Rings Forged Shafts (long) Aerospace Structural Forgings Marine Hardware Round & Hex Bars Forged Blocks & Blanks Custom Near-Net Forgings

17-4PH Development Timeline: From Invention to Industry Workhorse

17-4PH was invented by Armco in 1947, codified generically as UNS S17400 and ASTM A564 Type 630 in the 1960s, standardised in Europe as EN 1.4542 in the 1980s, and restricted by NACE MR0175 to the H1150-M condition for sour service in the 1990s. The trademark passed from Armco to AK Steel and then to Cleveland-Cliffs Inc. in 2020.

1947
Armco (USA) invents 17-4 PH®
Armco Steel Corporation develops the first precipitation-hardening martensitic stainless steel. The breakthrough is about 4 % copper added to a 17 % Cr – 4 % Ni matrix, which forms strengthening ε-Cu precipitates during low-temperature aging, the strength of an alloy steel with stainless corrosion resistance. The trademark 17-4 PH® is registered.
1950s
First aerospace adoption
US airframe builders adopt 17-4PH for fittings and hydraulic components. AMS 5643 is developed for aerospace bars and forgings, adding transverse tests and clean-melt requirements above the general ASTM A564.
1961
15-5 PH® developed
A cleaner version of 17-4PH, with lower delta-ferrite content achieved through a slightly different Cr/Ni balance, is introduced as 15-5 PH for applications needing better transverse toughness; primarily heavy aerospace forgings. See our 15-5PH forging page.
1960s
UNS S17400 codified; ASTM A564 published
The Unified Numbering System assigns S17400 to the 17-4PH chemistry. ASTM A564 Type 630 becomes the generic specification, separating the alloy from the Armco trademark and allowing licensed and independent production worldwide.
1970s
PH 13-8 Mo introduced for landing gear
A premium precipitation-hardening stainless with a molybdenum addition (UNS S13800) is developed for higher strength and better corrosion resistance, reserved for critical aerospace. 17-4PH remains the general industrial workhorse. See our PH13-8Mo page.
1980s
EN 10088-3 / 1.4542 standardised in Europe
European standardisation adopts the 17-4PH chemistry as 1.4542 (X5CrNiCuNb16-4) with tighter sulfur (≤0.015 %) and silicon (≤0.70 %) limits, driven by European demand for cleaner stainless in offshore and nuclear projects.
1990s
NACE MR0175 restricts 17-4PH to H1150-M for sour service
After sulfide-stress-cracking failures in oil and gas, NACE MR0175 (later ISO 15156) restricts 17-4PH in H₂S-containing environments to the double-aged H1150-M condition at 33 HRC maximum. This becomes the dominant H-condition for oilfield wellhead and downhole components.
2020
Trademarks transfer to Cleveland-Cliffs Inc.
After successive corporate restructurings the 17-4 PH®, 15-5 PH® and PH 13-8 Mo® trademarks pass from Armco to AK Steel and then to Cleveland-Cliffs Inc. The generic equivalents (UNS S17400, ASTM A564, ASTM A705, AMS 5643, EN 1.4542) remain unrestricted for independent producers such as Jiangyin Jiangnan Metal Co., Ltd.
2020s
Additive manufacturing and lower-carbon forging
17-4PH becomes one of the most widely used metals in laser powder-bed-fusion and binder-jet printing. In parallel, traditional forging producers move to scrap-based electric-arc melting with secondary metallurgy and lower embodied carbon, in response to aerospace and OEM sustainability requirements.

What Is 17-4PH / UNS S17400 Stainless Steel?

17-4PH is the most widely used precipitation-hardening martensitic stainless steel. A 17 % Cr – 4 % Ni – 3–5 % Cu chemistry, stabilised with Nb+Ta, transforms to martensite on cooling from 1040 °C and is then strengthened by a single low-temperature aging step that precipitates copper-rich ε particles. The result is alloy-steel strength (up to 1,310 MPa) with corrosion resistance broadly comparable to Type 304.

The defining feature of 17-4PH is the tunable strength-versus-toughness trade-off available through the choice of aging temperature. The H-number (H900, H1025, H1150 and so on) is that aging temperature in degrees Fahrenheit. Higher aging temperatures produce lower strength but higher impact toughness, better stress-corrosion cracking resistance and improved ductility. This single-grade flexibility is why 17-4PH dominates the pump and valve industries, aerospace structural parts, marine hardware, food and chemical processing equipment and many specialty industrial applications, and why Jiangyin Jiangnan Metal keeps all seven aging cycles qualified on its own heat-treatment lines.

17-4PH is martensitic and therefore magnetic in every condition (μᵣ ≈ 95 typical), which distinguishes it from the austenitic Cr-Ni stainless grades. It should not be used for prolonged service above about 315 °C (600 °F), because exposure at aging temperatures will over-age the precipitates and permanently reduce strength. For higher service temperatures see our A286 / UNS S66286 page. Where transverse toughness or cleanliness must be higher, see 15-5PH or PH 13-8 Mo.

What Are the EN 1.4542, SUS 630 and AMS 5643 Equivalents of 17-4PH?

They are the same alloy under different specifying bodies. UNS S17400, AISI 630, ASTM A564 Type 630, ASTM A693 Type 630, ASTM A705 Gr 630, AMS 5643 / 5604 / 5622, EN 1.4542 (X5CrNiCuNb16-4) and JIS SUS 630 all describe the 17Cr-4Ni-Cu-Nb chemistry. 17-4 PH® itself is a Cleveland-Cliffs trademark, not a specification.

Jiangyin Jiangnan Metal Co., Ltd. accepts purchase orders written under any of the designations below and supplies UNS S17400 / ASTM A564 Type 630 forgings certified against the equivalent specification named on the order.

Table 0: 17-4PH / UNS S17400 equivalent designations
Standard / bodyDesignationRegion and notes
USA · brand (Cleveland-Cliffs trademark)17-4 PH®Registered trademark of Cleveland-Cliffs Inc. We do not sell under this name; we ship the generic equivalents below.
USA · UNSUNS S17400Generic Unified Numbering System designation
USA · AISI (legacy)AISI 630Legacy AISI designation, still common on drawings and datasheets
USA · ASTM (bars, shapes)ASTM A564 Type 630Hot-rolled and cold-finished bars, rods and shapes
USA · ASTM (sheet, plate)ASTM A693 Type 630Sheet, strip and plate
USA · ASTM (forgings)ASTM A705 Gr 630The correct specification to cite on a forging order
USA · AMS (bars, forgings)AMS 5643Bars, forgings, tubing and rings; the usual aerospace specification
USA · AMS (sheet, strip)AMS 5604Sheet and strip
USA · AMS (alternate bars)AMS 5622Bars, alternate specification
USA · ASME BPVCSA-564 Type 630 / SA-705 Gr 630Pressure-vessel code equivalents
Europe · DIN / EN1.4542 / X5CrNiCuNb16-4EN 10088-3; tighter S and Si than ASTM
Japan · JISSUS 630JIS G 4303 (bars) / JIS G 4318 (cold finished)

What Is the Chemical Composition of 17-4PH / UNS S17400?

Per ASTM A564 Type 630: C ≤0.07, Mn ≤1.00, Si ≤1.00, P ≤0.040, S ≤0.030, Cr 15.00–17.50, Ni 3.00–5.00, Cu 3.00–5.00, Nb+Ta 0.15–0.45, balance Fe; all in weight per cent. AMS 5643, ASTM A705 Gr 630 and JIS SUS 630 use the same limits; EN 1.4542 is tighter on sulfur and silicon.

Chromium provides the corrosion resistance; the low nickel plus copper stabilises martensite with precipitation-strengthening capability; the niobium and tantalum addition prevents chromium-carbide sensitisation and controls precipitation during aging.

Table 1: 17-4PH / UNS S17400 chemical composition (wt %, ASTM A564 Type 630)
ElementMinMaxMetallurgical role
Carbon (C)0.07Strength contribution; capped low to preserve corrosion resistance
Manganese (Mn)1.00Deoxidiser
Silicon (Si)1.00Deoxidiser
Phosphorus (P)0.040Residual impurity
Sulfur (S)0.030Residual impurity; MnS inclusions act as pit initiators
Chromium (Cr)15.0017.50Corrosion resistance, martensite stabiliser
Nickel (Ni)3.005.00Toughness; controls martensite-finish temperature
Copper (Cu)3.005.00Primary precipitation-hardening element (ε-Cu phase)
Niobium + tantalum (Nb+Ta)0.150.45Stabiliser; controls precipitation during aging
Iron (Fe)BalanceMatrix

How Do ASTM A564, AMS 5643, EN 1.4542 and JIS SUS 630 Differ?

The mechanical minimums are effectively identical; the chemistry limits and test requirements are not. EN 1.4542 halves the sulfur limit to 0.015 %, cuts silicon to 0.70 %, narrows chromium to 15.0–17.0 % and permits up to 0.60 % molybdenum. AMS 5643 keeps ASTM chemistry but adds transverse tensile tests, clean melting, grain-flow verification and Class A ultrasonic inspection. A heat made to EN 1.4542 satisfies all four simultaneously.

Most competitor pages claim the four specifications are identical. Technically they are not. Jiangyin Jiangnan Metal Co., Ltd. procures raw stock to the most restrictive applicable limit so that a single heat can satisfy several specifications at once on the material test certificate.

Chemistry limits side by side

Table 1b: chemistry limits by standard (wt %, maxima unless a range is shown)
Element ASTM A564
Type 630 (USA)
AMS 5643
(US aerospace)
EN 1.4542
(Europe)
JIS SUS 630
(Japan)
Carbon (C)0.070.070.070.07
Silicon (Si)1.001.000.701.00
Manganese (Mn)1.001.001.501.00
Phosphorus (P)0.0400.0400.0400.040
Sulfur (S)0.0300.0300.0150.030
Chromium (Cr)15.00–17.5015.00–17.5015.00–17.0015.00–17.50
Nickel (Ni)3.00–5.003.00–5.003.00–5.003.00–5.00
Copper (Cu)3.00–5.003.00–5.003.00–5.003.00–5.00
Niobium + Ta0.15–0.450.15–0.45≤0.45 (no minimum)0.15–0.45
Molybdenum (Mo)not specifiednot specified≤0.60 permittednot specified
Tighter than ASTM (cleaner steel required) Looser than ASTM Element permitted that ASTM does not specify

Bottom line on chemistry: a single 17-4PH heat meeting EN 1.4542 (the most restrictive on sulfur and silicon) automatically satisfies ASTM A564, AMS 5643 and JIS SUS 630 as well, provided the EN-permitted molybdenum is verified low. Our standard practice is to procure to the strictest applicable limit and issue a multi-designation material test certificate.

Test and quality requirements side by side

Minimum mechanical properties are essentially identical across all four standards for the same H-condition. The real differences are which tests are required, in which direction, and what non-destructive examination is performed.

Table 1c: typical test requirements by standard
Test / requirement ASTM A564
(general bars)
AMS 5643
(aerospace)
EN 10088-3
(EU bars)
JIS G 4303
(JP bars)
Tensile, longitudinalRequiredRequiredRequiredRequired
Tensile, transverseNot requiredRequiredOptionalOptional
HardnessRequired per condition (HRC)Required per condition (HRC)Required (HB)Required (HRC)
Charpy V-notch impactOptional, per buyerRequired, tight limitsOptionalOptional
Grain flow / macroetchOptionalRequired for forgingsOptionalOptional
Clean / vacuum meltingNot requiredRequired (VIM-VAR or AOD)Not requiredNot required
Ultrasonic inspectionPer ASTM A388Per AMS-STD-2154 Class APer EN 10228Per JIS G 0801
Penetrant / magnetic particlePer ASTM E165 / E1417ASTM E1417 Type I Method C, Sens. 3+Per EN ISO 3452Per JIS Z 2343
Inclusion ratingPer ASTM E45 if orderedPer AMS 2301 / 2304Per ISO 4967Per JIS G 0555
Heat-treat traceabilityHeat numberLot-level furnace chart recordingsHeat + cast numberHeat + cast number
Certificate formatEN 10204 3.1 typical3.1 or 3.2 + AMS source approvalEN 10204 3.1 / 3.2Mill test report

Which standard should you specify?

🇺🇸 US general industrial
ASTM A705 Gr 630
(A564 Type 630 for bars)
Pumps, valves, non-aerospace structural. EN 10204 3.1 mill certificate. The most economical and most common route.
✈ US aerospace
AMS 5643
Required for airframe and engine accessory work. Cleaner melt, transverse tests, grain flow, Class A UT and source-approval flow-down.
🇪🇺 European projects
EN 10088-3
1.4542 / X5CrNiCuNb16-4
EU offshore, oil and gas, nuclear and chemical plant, CE-marked equipment. Tighter S and Si than ASTM, so a cleaner microstructure.
🇯🇵 Japanese projects
JIS SUS 630
(JIS G 4303 / G 4318)
Japanese OEM supply chains in automotive, machinery and marine. Chemistry matches ASTM; the certificate format is the differentiator.
🛢 Sour service, any region
NACE MR0175 / ISO 15156
plus the underlying spec
Oil and gas in H₂S. Restricts 17-4PH to H1150-M double-aged at ≤33 HRC. Added on top of the base specification, check with the NACE checker.

Multi-standard material test certificates

For customers who need cross-border traceability, Jiangyin Jiangnan Metal supplies single-heat material certified to several standards at once. The material test certificate lists:

  • the primary specification ordered, for example AMS 5643, EN 1.4542 or ASTM A705 Gr 630;
  • every equivalent designation the chemistry and mechanicals also satisfy, stated as "also conforms to: UNS S17400, ASTM A564 Type 630, JIS SUS 630";
  • heat-treatment chart recordings, lot level for AMS work, batch level for general work;
  • EN 10204 3.1 as standard, or 3.2 with third-party witness (Lloyd's, DNV, BV, ABS, TÜV) on request;
  • a NACE MR0175 / ISO 15156 compliance statement where applicable.

Practical takeaway: if you are unsure which standard to specify, ASTM A705 Gr 630 for forgings (or ASTM A564 Type 630 for bar) is the safest default. We cross-certify to EN 1.4542 and JIS SUS 630 on the same certificate at no extra cost. AMS 5643 aerospace certification is quoted as a separate lot because of the additional testing burden.

What Are the Mechanical Properties of 17-4PH in Every H-Condition?

Minimum properties per ASTM A564 / A705: H900 = 1,310 MPa UTS, 1,170 MPa YS, 40 HRC; H925 = 1,170 / 1,070 MPa, 38 HRC; H1025 = 1,070 / 1,000 MPa, 35 HRC; H1075 = 1,000 / 860 MPa, 32 HRC; H1100 = 965 / 795 MPa, 31 HRC; H1150 = 930 / 725 MPa, 28 HRC; H1150-M = 795 / 515 MPa, ~24 HRC. Condition A is 1,030 / 760 MPa at ≤38 HRC.

The H-number is the aging temperature in degrees Fahrenheit. Values below are minimums for longitudinal tests on bars and forgings up to 75 mm thick; thicker sections typically show a 5–8 % reduction. Charpy values are typical room-temperature results measured on our own coupons rather than specification minimums.

Table 2: 17-4PH / UNS S17400 minimum mechanical properties by aging condition
ConditionAging cycleUTS minYS min (0.2 %)Elong. min %RA min %Hardness minCharpy V (typ.)
H900482 °C (900 °F) / 1 h / AC1,310 MPa (190 ksi)1,170 MPa (170 ksi)104040 HRC~18 J
H925496 °C (925 °F) / 4 h / AC1,170 MPa (170 ksi)1,070 MPa (155 ksi)104438 HRC~22 J
H1025552 °C (1025 °F) / 4 h / AC1,070 MPa (155 ksi)1,000 MPa (145 ksi)124535 HRC~35 J
H1075580 °C (1075 °F) / 4 h / AC1,000 MPa (145 ksi)860 MPa (125 ksi)134532 HRC~50 J
H1100593 °C (1100 °F) / 4 h / AC965 MPa (140 ksi)795 MPa (115 ksi)144531 HRC~60 J
H1150621 °C (1150 °F) / 4 h / AC930 MPa (135 ksi)725 MPa (105 ksi)165028 HRC~75 J
H1150-M (double aged)760 °C / 2 h + 621 °C / 4 h / AC795 MPa (115 ksi)515 MPa (75 ksi)1855~24 HRC (≤33 HRC req.)~135 J
Condition A (solution only)1040 °C / AC, no aging1,030 MPa (150 ksi)760 MPa (110 ksi)5≤38 HRC (max)~30 J

Data compiled by Jiangyin Jiangnan Metal Co., Ltd. from ASTM A564/A564M, ASTM A705/A705M and SAE AMS 5643, cross-checked against production test records. Hardness figures are specification minimums, except Condition A which is a maximum and H1150-M where NACE MR0175 imposes a 33 HRC ceiling. Reproduced in machine-readable form in the Reference Data Appendix.

How Do You Choose Between 17-4PH H900, H1025, H1075 and H1150?

Choose by the failure mode you fear most. H900 for maximum static strength and hardness with no impact or chloride exposure. H1025 as the general-purpose default. H1075 where fatigue governs, such as pump shafts. H1150 where impact toughness or chloride stress-corrosion resistance governs. H1150-M whenever H₂S is present, because NACE MR0175 accepts no other 17-4PH condition.

Table 2b: how to pick the right H-condition
ConditionChoose this when…Avoid this if…Typical industries
H900Maximum strength and hardness are needed under static loadingImpact, fatigue or chloride SCC are credible concernsTooling, fasteners, knives, wear parts
H925A small toughness gain over H900 is wantedRarely specified. H900 or H1025 is usually chosen insteadAerospace fasteners
H1025You want the best all-round balance of strength and toughnessA severe chloride SCC environment is presentAerospace structural, valve bodies, general industrial
H1075Fatigue and corrosion fatigue govern the designVery high static loading is requiredPump industry: chemical, water, marine
H1100Large sections need consistent through-agingHighest yield strength is requiredHeavy industrial, oil and gas
H1150Impact toughness and chloride SCC resistance dominateYield strength above ~700 MPa is requiredMarine, chemical, severe service
H1150-MMaximum impact toughness; any H₂S-containing serviceStrength is the primary criterionOil and gas downhole and wellhead, NACE applications

H-Condition Decision Wizard

Answer four short questions and get the optimal H-condition for your 17-4PH part, with the reasoning behind it.
Exclusive
1 / 4: What is the primary application?
2 / 4: Which property is most critical?
3 / 4: What is the service environment?
4 / 4: What certification applies?

Sequence reminder. Aging is always performed after solution treatment (1040 °C then air cool to below 30 °C) and after rough machining. Because aging produces a dimensional change of under 0.1 %, tight-tolerance features should be finish-machined after aging, see ordering mistake 5.

17-4PH Heat Treatment Recipe Generator

Pick a target H-condition or required UTS and get a complete, printable solution-plus-aging recipe for your heat-treatment vendor.
Exclusive

Recipes follow ASTM A564 / A705 and AMS 2759/3 standard cycles. Hold times scale with section thickness above 25 mm at roughly 30 minutes per 12 mm. Vacuum or inert atmosphere is preferred. Ensure complete austenitisation on heating and full martensite transformation before aging. Final properties must be confirmed by hardness check plus a tensile test on coupons from the same heat.

17-4PH Aging Temperature → Mechanical Properties

Drag the slider to watch UTS, yield, hardness and impact toughness trade off against each other across the whole aging range.
Exclusive
482 °C: H900, maximum strength 621 °C. H1150, maximum toughness
1400 1100 800 500 200 MPa 482 510 540 575 605 621 Aging temperature (°C) UTS (MPa) YS 0.2 % (MPa) Hardness (HRC × 30) Charpy V (J × 8)
UTS
1070 MPa
Yield (0.2 %)
1000 MPa
Hardness
35 HRC
Charpy V (RT)
35 J
SCC risk
Moderate
Best use
General service

Curves are built from the ASTM A564 / A705 and AMS 5643 minimums in Table 2, with typical Charpy values from our own coupon tests. Properties are minimums for sections up to 75 mm; thicker sections may show a 5–8 % reduction. The hardness and Charpy curves are scaled to share the MPa axis, the legend shows the multipliers.

17-4PH Microstructure Visualiser: Watch the Precipitates Form

See how copper-rich ε precipitates evolve from solution-treated Condition A through every H-condition. Their size and density is what gives 17-4PH its strength.
Exclusive
Cu-rich precipitates Martensite laths
≈1,000× magnification
Schematic only
Precipitate size
7 nm
Density
High
Hardness
35 HRC
UTS
1070 MPa
What you are seeing: the red dots are copper-rich ε precipitates; the yellow-brown background is the martensite matrix with its parallel lath pattern, formed during solution treatment and cooling. Use the selector above to see how the microstructure changes with H-condition.

Schematic illustration only. Real precipitates range from about 1 nm to 50 nm and are visible only under transmission electron microscopy; sizes here are exaggerated for legibility. Precipitation behaviour based on published studies of 15-5PH (Habibi Bajguirani, 2002) and PH 13-8 Mo (Hochanadel et al., 1994), which share 17-4PH's copper-precipitation mechanism.

17-4PH Aging Kinetics Simulator: Temperature, Time and Strength

Choose an aging temperature and time and see the predicted strength curve. Useful for planning custom cycles, judging the effect of accidental over-aging, and comparing time-temperature trade-offs.
Exclusive
552 °C
4.0 h
15001400 13001200 11001000900 0.5 h2 h4 h 8 h16 h48 h UTS (MPa) Aging time (log scale) Peak
Current UTS
1200 MPa
Peak UTS at this temperature
1230 MPa
Time to peak
3.0 h
Distance from peak
-2%
Status: Approaching peak strength, the typical commercial aging window. Small variations in time will have little effect on properties.

Model based on published 17-4PH aging kinetics, copper precipitation followed by coarsening. Real properties depend on prior solution-treatment quality, section thickness and where the heat sits within the chemistry band. The curve combines an Avrami-type rise with an Ostwald-ripening decline, fitted to the ASTM A564 nominal property table. For production heat treatment, always validate with hardness tests on coupons from the same heat.

17-4PH Fatigue S-N Curve

Pick an H-condition and stress amplitude to see predicted cycles to failure. Rotating-bending data, R = −1, smooth specimen, room temperature, with optional Goodman mean-stress correction.
Exclusive
300 600 MPa 900
0 = fully reversed (R = −1)
1400 1100 800 500 200 Stress amplitude (MPa) 10³ 10⁴ 10⁵ 10⁶ 10⁷ 10⁸ Cycles to failure (N) H900 (highest strength) H1025 (general) H1075 (pump shafts) H1150 (max toughness)
Selected stress
600 MPa amplitude
Predicted life
2.5 × 10⁵ cycles
Service hours at 30 Hz
2.3 hours
Endurance limit (10⁷)
590 MPa
Verdict
Finite life
Goodman correction
No

Curves are built from typical published 17-4PH rotating-bending fatigue data (R = −1, smooth specimen, room temperature). Real fatigue life depends strongly on surface finish (multiply by 0.6–0.8 for as-machined and 0.4–0.6 for as-forged) plus notch geometry, corrosive environment and mean stress. For design, apply a factor of safety of at least 2 on stress or 10 on cycles. Endurance limits are tabulated in the Reference Data Appendix.

Worked Design Calculations Using 17-4PH Data

Three worked examples show how the tabulated 17-4PH properties feed real decisions: a pump-shaft critical speed check using E = 196 GPa, a valve-stem Euler buckling check, and a modified-Goodman infinite-life fatigue check that fails and shows the three ways to fix it. All are simplified for teaching; production designs need finite-element verification and the applicable code factors.

Example 1: centrifugal pump shaft critical speed

A vertical centrifugal pump shaft in 17-4PH H1075 must be checked against its first lateral critical speed.

Given Shaft diameter D = 150 mm; bearing span L = 2,000 mm; impeller mass m = 80 kg at mid-span; operating speed 1,800 rpm. Material 17-4PH H1075, E = 196 GPa, ρ = 7.75 g/cm³.
Formula (Rayleigh) First critical speed for a concentrated mass mid-span between simple supports: Nc = (60 / 2π) × √(48EI / mL³), with I = πD⁴/64.
Solution I = π × (0.15)⁴ / 64 = 2.485 × 10⁻⁵ m⁴
48 × E × I = 48 × 196 × 10⁹ × 2.485 × 10⁻⁵ = 2.338 × 10⁸ N·m²
mL³ = 80 × (2.0)³ = 640 kg·m³
ω = √(2.338 × 10⁸ / 640) = √(3.653 × 10⁵) = 604 rad/s
Nc = 604 × 60 / 2π ≈ 5,770 rpm
Verdict Operating speed is about 31 % of critical, which is safe; the usual rule is to keep the operating speed below 0.7 × Nc. Specify H1075 for fatigue, or H1025 if higher yield is needed (a UTS gain of roughly 7 %). Do not use H900, its fatigue behaviour is worse despite the higher yield.

Example 2: valve stem buckling (Euler)

A high-pressure valve stem in 17-4PH H1025 must resist axial seating force without buckling.

Given Stem diameter d = 25 mm; unsupported length 600 mm, fixed-pinned so K = 0.7; applied axial force F = 50 kN.
Formula (Euler) Pcr = π²EI / (KL)²
Solution I = π × (0.025)⁴ / 64 = 1.917 × 10⁻⁸ m⁴
(KL)² = (0.7 × 0.6)² = 0.1764 m²
Pcr = π² × 196 × 10⁹ × 1.917 × 10⁻⁸ / 0.1764
Pcr ≈ 210 kN, giving a factor of safety of 210 / 50 = 4.2
Verdict A buckling safety factor of 4.2 exceeds the typical valve requirement of 3.0. The yield check still applies: stress = F/A = 50,000 / (π × 0.025² / 4) = 102 MPa, far below the H1025 yield of 1,000 MPa. The stem passes both criteria.

Example 3: fatigue safety factor (modified Goodman)

A 17-4PH H1025 component sees fluctuating tensile stress. Does it meet an infinite-life criterion?

Given Stress amplitude σa = 350 MPa; mean stress σm = 250 MPa; surface-finish factor Cs = 0.7 (as machined); reliability factor Cr = 0.81 (99 %). H1025: UTS 1,070 MPa, laboratory endurance limit Se′ = 590 MPa.
Formula σa/Se + σm/UTS = 1/n, with corrected Se = Cs × Cr × Se′.
Solution Corrected Se = 0.7 × 0.81 × 590 = 334 MPa
1/n = 350/334 + 250/1,070 = 1.048 + 0.234 = 1.282
n = 1 / 1.282 = 0.78
Verdict A safety factor of 0.78 is below 1.0, so only finite life is achieved. Three fixes: reduce the stress amplitude by increasing cross-section 15–20 %; move to H900 if the static-strength budget allows (raw Se ≈ 620 MPa) while accepting the SCC penalty; or shot-peen, which raises Cs to about 1.1 and pushes n above 1.0 with no geometry change. The most economical fix is usually shot-peening plus a 10 % size increase.

These worked examples are simplified for teaching. Production designs must also consider temperature derating, multi-axial stress, corrosion fatigue and hydrogen, code-specified safety factors under ASME, API or EN 13445, and lifecycle cost. The engineering team at Jiangyin Jiangnan Metal Co., Ltd. is available for project-specific review.

What Are the Physical Properties of 17-4PH: Density, Thermal and Magnetic?

Density 7.75 g/cm³ (0.280 lb/in³); elastic modulus 196 GPa; shear modulus 77 GPa; Poisson's ratio 0.27; thermal conductivity ≈17.8 W/m·K; specific heat 460 J/kg·K; electrical resistivity 0.80 µΩ·m; relative magnetic permeability ≈95; Curie point ≈480 °C; melting range 1400–1440 °C.

Table 3: 17-4PH / UNS S17400 physical properties, aged condition
PropertyValueUnitCondition
Density7.75 (0.280)g/cm³ (lb/in³)Aged, room temperature
Modulus of elasticity, E196 (28.5 × 10⁶)GPa (psi)Room temperature
Shear modulus, G77GPaRoom temperature
Poisson's ratio0.27Room temperature
Coefficient of thermal expansion10.8 / 11.6 / 12.2×10⁻⁶ per °C20–100 / 20–315 / 20–540 °C
Thermal conductivity≈17.8W/m·KRoom temperature
Specific heat460J/kg·KRoom temperature
Electrical resistivity0.80µΩ·mRoom temperature
Relative magnetic permeability, µᵣ≈95Ferromagnetic, martensitic matrix
Curie temperature≈480°C
Melting range1400–1440°CSolidus to liquidus

How Corrosion-Resistant Is 17-4PH in Seawater, Acids and Sour Service?

Roughly comparable to Type 304, far better than carbon or low-alloy steel, clearly worse than 316L, which carries 2–3 % molybdenum. The PREN of 17-4PH is about 16–17, below the threshold for chloride pitting resistance in seawater, so marine use is normally limited to splash zones and intermittent immersion. Higher aging temperatures (H1100, H1150) markedly improve stress-corrosion resistance.

The H-condition changes corrosion behaviour. Low-temperature aging (H900, H925) gives the highest strength but raises susceptibility to chloride stress-corrosion cracking. High-temperature aging (H1100, H1150) reduces strength but substantially improves SCC resistance. For oil and gas service under NACE MR0175 / ISO 15156, 17-4PH is restricted to the H1150-M double-aged condition with hardness 33 HRC or lower.

NACE MR0175 / ISO 15156 Sour-Service Compliance Checker

Enter your service conditions for an immediate first-pass verdict on whether 17-4PH at your specification meets sour-service requirements.
Exclusive
Sour threshold: ≥0.3 kPa (0.05 psi)

Disclaimer. This is a first-pass screening tool based on NACE MR0175 / ISO 15156-3 Table A.20 for precipitation-hardening stainless steels. Final material acceptance requires review by a qualified materials engineer against the current edition of the standard, and may involve project-specific qualification testing. Jiangyin Jiangnan Metal Co., Ltd. provides this tool for guidance and accepts no liability for application decisions.

17-4PH Service Temperature Safety Assessment

Enter service temperature and expected duration to get a safety verdict, predicted strength retention and alternative materials if 17-4PH is unsuitable.
Exclusive

17-4PH service-temperature limits are governed by over-aging kinetics. Aging is performed between 480 °C and 620 °C, so any service temperature approaching the aging temperature will progressively soften the part. The conservative continuous-service limit is about 315 °C (600 °F). For higher temperatures consider A286 / UNS S66286 up to about 700 °C, or Inconel 718 up to about 650 °C.

For severe chloride or aggressive acid environments, consider upgrading to:

  • PH 13-8 Mo (UNS S13800), premium aerospace PH grade with a molybdenum addition for better corrosion resistance and toughness;
  • 904L (UNS N08904), super-austenitic for sulfuric acid service;
  • Nitronic 50 (UNS S20910), high-strength austenitic widely accepted for sour service;
  • 2205 or super-duplex, where continuous seawater immersion is unavoidable.

17-4PH Failure Modes and How to Prevent Them

Twelve failure modes account for almost all 17-4PH service failures: chloride stress-corrosion cracking, sulfide stress cracking, service over-aging, sigma-phase embrittlement, galvanic corrosion, chloride pitting, high-cycle fatigue, hydrogen embrittlement, incorrect heat treatment, forging bursts and laps, crevice corrosion in threads, and weld heat-affected-zone softening. Each is prevented at the specification stage rather than in service.

Chloride stress-corrosion cracking
Cause
High-strength conditions (H900, H925) in chloride environments combined with tensile residual stress. Cracks start at surface pits and run transgranularly.
Detection
Penetrant or magnetic-particle testing shows linear surface cracks; ultrasonic testing may show branched subsurface cracking. Often catastrophic before detection.
Prevention
Use H1100 or H1150 for any chloride exposure. For seawater, upgrade to 2205 or super-duplex.
Sulfide stress cracking (NACE)
Cause
H₂S service above 33 HRC. Atomic hydrogen from H₂S dissociation enters the lattice, embrittles the martensite and cracks it under tensile load.
Detection
In-service inspection finds intergranular cracks at high-stress points; propagation can be rapid.
Prevention
Mandatory H1150-M double-aged condition with hardness ≤33 HRC verified at every region, per NACE MR0175 / ISO 15156.
Service over-aging
Cause
Service temperature above about 315 °C. The Cu-rich ε precipitates coarsen and lose coherency, and strength drops 15–40 % over months.
Detection
Hardness falls from roughly 35 HRC to 25 HRC or below. Ductility rises, yield strength falls, and plastic deformation can occur at design load.
Prevention
Do not use 17-4PH above 315 °C continuously. Check with the service-temperature tool and move to A286 or Inconel 718 if needed.
Sigma-phase embrittlement
Cause
Extended exposure between 565 °C and 870 °C (slow cooling from high-temperature service, or an improper post-weld cycle) precipitates brittle Fe-Cr sigma phase at grain boundaries.
Detection
Charpy impact toughness collapses, often by more than half. Frequently discovered only post-fracture by metallography.
Prevention
Cool rapidly through 565–870 °C. After welding, re-solution and re-age. Avoid intermediate-temperature soaking.
Galvanic corrosion
Cause
17-4PH coupled to more noble alloys (nickel alloys, copper alloys) in an electrolyte. 17-4PH becomes the anode and corrodes locally at an accelerated rate.
Detection
Pitting and crevice attack at the junction, with an asymmetric pattern affecting only one side.
Prevention
Isolate dissimilar metals with insulating sleeves or gaskets, apply cathodic protection, and avoid coupling to copper-based alloys in seawater.
Chloride pitting
Cause
PREN ≈16–17, below the threshold for pit-free service in seawater. Pits nucleate at MnS inclusions or surface defects and deepen autocatalytically.
Detection
Localised deep pits, sometimes under 1 mm wide but 5 mm or more deep, which may link into crack-like features.
Prevention
For chloride service specify EN 1.4542, whose lower sulfur means fewer MnS pit initiators. Limit exposure, or move to 316L or 2205 for continuous chloride.
High-cycle fatigue
Cause
Cyclic stress above the endurance limit, about 620 MPa for H900 down to about 460 MPa for H1150. Surface defects, machining marks and notches cut fatigue strength 30–50 %.
Detection
Beach marks on the fracture surface. The crack starts at the surface and grows slowly until the remaining section fails. Check with the fatigue tool.
Prevention
Surface roughness Ra ≤1.6 µm, shot-peening or low-stress grinding, generous radii at stress concentrations. H1075 gives the best fatigue balance.
Hydrogen embrittlement
Cause
Hydrogen introduced during pickling, electroplating, welding or cathodic protection diffuses to martensite lath boundaries and causes delayed brittle cracking.
Detection
Delayed cracking days to weeks after service start, usually at threads or other notches, with intergranular fracture features.
Prevention
Bake at 190–220 °C for 4–24 hours after plating or pickling. Avoid cathodic over-protection. Prefer H1150 or H1150-M for plated or pickled parts.
Improper heat treatment
Cause
Incomplete solution treatment, interrupted cooling so that transformation is incomplete, or the wrong aging cycle; leaving retained austenite and an incorrect precipitate state.
Detection
Hardness out of specification, high or low; tensile strength that does not match the nominal H-condition; confirmed by metallography.
Prevention
Verify both cycles on the certificate, check the actual furnace charts, and use the recipe generator for correct parameters.
Forging bursts and laps
Cause
Forging below about 950 °C, in the work-hardening regime, or excessive reduction in one stroke. Produces internal bursts or surface laps of folded oxide.
Detection
Ultrasonic testing shows internal indications; surface penetrant or magnetic-particle testing shows linear lap indications. Often hidden until final machining exposes them.
Prevention
Hold the forging window at 1170–1230 °C and never finish below 950 °C. Use multi-step incremental reduction and ultrasonic acceptance to ASTM A388 Class B or better.
Crevice corrosion in threads and joints
Cause
Stagnant electrolyte in threads, gaskets or lap joints becomes acidic and chloride-rich; the local PREN drops below threshold and attack starts.
Detection
Discolouration in the crevice, eventually deep pits. Often unnoticed until a pressure test fails.
Prevention
Design crevices out with radiused corners and flush gasket seating. For chloride service use H1150 or upgrade to duplex.
Weld heat-affected-zone softening
Cause
Welding without proper preparation. The HAZ ends up partly re-solutioned and partly over-aged, so properties vary across the joint.
Detection
A hardness traverse across the weld shows a soft band in the HAZ; failure often occurs there rather than in the weld metal.
Prevention
Weld in Condition A, then re-solution and age the assembly. Use ER630 matching filler and 150 °C preheat for thick or restrained joints.

When Should You Choose 17-4PH Over PH 13-8 Mo, 15-5PH or 316L?

Choose 17-4PH when you need alloy-steel strength with stainless corrosion resistance at industrial cost. Choose PH 13-8 Mo when transverse toughness or corrosion margin must be higher and the budget allows two to three times the price. Choose 15-5PH for heavy aerospace forgings needing better through-thickness properties. Choose 316L when chloride corrosion, not strength, governs.

Table 4: 17-4PH versus other precipitation-hardening and common stainless grades
Property17-4PH (H1025)PH 13-8 Mo (H1000)15-5PH (H1025)304L316L
UNSS17400S13800S15500S30403S31603
TypeMartensitic PHMartensitic PHMartensitic PHAusteniticAustenitic
UTS~1,070 MPa~1,520 MPa~1,070 MPa~515 MPa~485 MPa
Yield (0.2 %)~1,000 MPa~1,410 MPa~1,000 MPa~205 MPa~170 MPa
Density7.75 g/cm³7.78 g/cm³7.78 g/cm³7.99 g/cm³7.99 g/cm³
MagneticYesYesYesNoNo
PREN, approx.16–172216–171926
Max service temperature~315 °C~430 °C~315 °C~870 °C (low yield)~870 °C (low yield)
Transverse toughnessModerateExcellent (cleaner alloy)Better than 17-4PHExcellentExcellent
Relative material cost2 ×4–5 ×2.5 ×1 × (baseline)1.3 ×
Best useGeneral PH workhorseAerospace landing gearHeavy aerospace forgingsGeneral serviceMarine and mild chloride

Material Substitution Finder: Can I Replace X with 17-4PH?

Pick what you use today and see whether 17-4PH is a valid substitute, which H-condition to specify, what you gain and what to watch for.
Exclusive

Substitution analysis is based on published typical properties; see the individual material datasheets for verified values. Final substitution decisions belong to a qualified materials engineer, considering cyclic loading, environment, certification, weldability and supply chain.

Cost-per-Strength Comparison: 17-4PH Against Five Alternatives

Enter part weight and quantity to see total cost across eight materials, ranked either by absolute cost or by cost per MPa of yield strength.
Exclusive

Price transparency. 17-4PH raw-material cost is dominated by nickel, chromium, copper and niobium content, and mill prices track the LME nickel and ferro-chrome indices with a typical two-to-four-week lag. We do not publish absolute prices because they move weekly and depend on quantity, dimensions, certification level and lead time, but we do offer index-linked pricing in long-term supply agreements. The reference prices in this calculator are indicative average mill prices for hot-forged round bar in standard sizes, FOB China, Q3 2026, and are tabulated in the Reference Data Appendix. Cost per MPa uses the minimum yield strength of each material's standard production condition. Forging conversion, machining and finishing costs are separate.

How Do You Weld, Machine and Forge 17-4PH / UNS S17400?

Weld in Condition A with ER630 or AMS 5825/5826 filler, then re-solution and age. Machine in Condition A where possible (machinability is roughly 50 % of free-machining 416) using sharp rigid carbide, positive rake, 50–80 m/min in turning and generous coolant. Forge between 1170 °C and 1230 °C, never finishing below 950 °C, with a forging ratio of at least 4:1 and slow cooling afterwards.

Welding 17-4PH

17-4PH is one of the most weldable precipitation-hardening stainless steels. GTAW and GMAW are the usual processes; matching filler per AMS 5825 / 5826 is preferred, with ER630 as the generic equivalent. Weld in Condition A, then perform a full solution treatment plus aging to restore properties in and around the weld zone. Preheat is generally unnecessary for thin sections, while thick or highly restrained joints benefit from 150 °C preheat to reduce hydrogen-cracking risk. Welding in the aged condition over-ages the heat-affected zone and can cost 20–40 % of local strength.

Machining 17-4PH

Machinability is approximately 50 % of free-machining 416 stainless and somewhat better than 304 or 316L. Machining in Condition A, at about 33 HRC, is preferred, because the alloy work-hardens less than the austenitic grades. Use sharp, rigid carbide tooling with positive rake geometry, moderate cutting speed (roughly 50–80 m/min for turning) heavy positive feed and generous coolant. The correct production sequence is rough machine in Condition A → solution treat → age → finish machine, because aging produces a dimensional change of under 0.1 % which can still exceed tolerance on close-fit features.

Forging 17-4PH

17-4PH forges within a 1170–1230 °C (2150–2250 °F) window, with a finishing temperature above 950 °C to stay out of the work-hardening and δ-ferrite regimes. Forging ratio should be at least 4:1 to break down the as-cast structure and meet AMS 5643 grain-flow requirements. The grade suits every common route, open-die forging for shafts and discs, hot ring rolling for seamless rings, closed-die forging for repeat-volume small parts and upset forging for short, large-section blanks. Near-net-shape forging is practical where 30–50 % of the rough machining can be removed by the die profile, as on compressor impeller hubs and valve bodies. Slow furnace cooling after the final blow is essential: an air or water quench from forging temperature can leave residual ferrite stringers visible on macroetch and may fail AMS 5643 cleanliness checks. For long bored shafts with bores above roughly 100 mm, ordering a trepanned billet instead of solid bar cuts material input by 40–60 % and shortens drilling time.

17-4PH Machinability Parameter Calculator

Pick H-condition, operation and tool material to get recommended cutting speed, feed, depth of cut and expected tool life; an afternoon of handbook lookups in one click.
Exclusive

Parameters are starting values; final selection depends on machine rigidity, setup stiffness, tool-holder geometry and surface-finish requirements. 17-4PH work-hardens, so maintain positive feed contact and never dwell. Coolant is recommended for all operations. For deep drilling, peck cycles reduce chip clogging and tool-life loss. Base values are tabulated in the Reference Data Appendix.

Production Capability: 17-4PH / UNS S17400 Forging Manufacturer

Jiangyin Jiangnan Metal Co., Ltd. forges 17-4PH shafts up to 8 m long, discs to 1,800 mm diameter, seamless rolled rings to 2,500 mm outside diameter and bar from 25 to 500 mm diameter, at single-piece weights up to 8,000 kg, with all seven aging conditions qualified in-house and ultrasonic, penetrant and magnetic-particle inspection on site.

The eight-stage 17-4PH forging process

Every 17-4PH forging leaving Jiangyin passes through these eight controlled stages. Each is logged on the heat-treatment chart and traceable on the final certificate.

1
Raw material
Bar or billet
Heat number traced
Chemistry verified
2
Forging
1170–1230 °C
Ratio ≥4:1
Multi-step reduction
3
Slow cool
Furnace cool
Avoid 565–870 °C dwell
4
Rough machine
±2 mm stock
Condition A
UT after
5
Solution treat
1040 °C ±10 °C
30 min per 12 mm
Air cool below 30 °C
6
Aging
H1025 = 552 °C / 4 h
H1150-M = two stage
Air cool
7
NDE and test
UT per ASTM A388
PT / MT surface
Hardness + tensile
8
Certificate and ship
EN 10204 3.1 / 3.2
Multi-standard cert
Marked and packed

Production equipment qualified for 17-4PH

The equipment below is qualified and calibrated for 17-4PH / UNS S17400 production. Sizes and weights are tested limits for this alloy, which differ from the carbon-steel limits.

Forging: heavy
Open-die hydraulic press, 40 MN
Max ingot 12 t
Max diameter 1,800 mm
Max length 8,000 mm
Forging; medium
Open-die hydraulic press, 25 MN
Max ingot 6 t
Best for shafts and bars
Faster cycle than the 40 MN
Ring rolling
Radial-axial ring mill
Max OD 2,500 mm
Max height 600 mm
Min wall 30 mm
Heat treatment
Bogie-hearth solution furnace
8 × 4 × 2 m chamber
1100 °C maximum
±5 °C uniformity
Heat treatment
Aging furnace
Ø2.5 m × 6 m
200–700 °C range
±3 °C uniformity
Heat treatment
Forced-air quench station
Rapid cool from 1040 °C
Ensures full martensite
All H-conditions
NDE, ultrasonic
Phased-array ultrasonic
ASTM A388 Class A/B/C
AMS-STD-2154 Class A
Automated scan and report
NDE, penetrant
Fluorescent penetrant line
ASTM E1417 Type I
Method C, sensitivity 3–4
Aerospace capable
NDE, magnetic particle
Wet fluorescent magnetic particle
ASTM E1444
Coil and yoke methods
Surface defects
Laboratory, chemistry
Optical emission spectrometer
Full elemental analysis
Calibrated daily
Traceable standards
Laboratory, mechanical
300 kN universal test machine
Tensile per ASTM E8
Charpy V per ASTM E23
Hardness HRC / HB / HV
Laboratory, metallography
Microstructure laboratory
Up to 1000× optical
Grain size per ASTM E112
Macroetch per ASTM E381

Delivery performance on 17-4PH orders

Transparent delivery data, refreshed quarterly, drawn from the 387 17-4PH / UNS S17400 orders shipped between Q3 2021 and Q2 2026. The percentage is the share of orders dispatched ex-works within the stated number of weeks, measured from order confirmation.

H1025 / H1075 standard
92 % in 8 wk
H900 / H925 high strength
88 % in 9 wk
H1150 / H1150-M
86 % in 10 wk
AMS 5643 aerospace certified
82 % in 12 wk
Large forgings above 3 t
78 % in 14 wk
NACE with 3.2 witness (DNV, BV, Lloyd's)
75 % in 14 wk

For short-lead stock items (common bar sizes in Condition A) dispatch in 4–6 weeks is sometimes possible. Contact us for current stock.

Max disc Ø
1,800 mm
Max ring OD
2,500 mm
Max shaft length
8 m
Max single weight
8,000 kg
Bar Ø range
25–500 mm
H-conditions
H900 · H925
H1025 · H1075
H1100 · H1150
H1150-M

Available forms in 17-4PH / UNS S17400

  • Pump shafts up to 8 m long, usually supplied in H1025 or H1075;
  • pump impellers and casings, closed-die or rough-machined open-die;
  • valve bodies, valve stems and valve trim to API 6A / 6D requirements;
  • forged discs and hubs up to 1,800 mm diameter;
  • seamless rolled rings up to 2,500 mm outside diameter, rectangular, contoured or T-section;
  • aerospace structural forgings to AMS 5643;
  • marine hardware such as rudder and propeller shafts for splash-zone use;
  • round, hex and square bars to ASTM A564 or AMS 5643;
  • forged blocks and blanks for further machining;
  • custom near-net-shape forgings to customer drawings.

17-4PH Forging Weight Calculator

Pick a shape and enter dimensions for an instant weight at the 17-4PH density of 7.75 g/cm³, then push the result straight into your RFQ.
Exclusive

Calculated at the 17-4PH density of 7.75 g/cm³ (0.280 lb/in³). The result is the net finished weight; allow 20–35 % machining stock for the rough forging weight depending on geometry and tolerance. Maximum single-piece capability at Jiangyin Jiangnan Metal Co., Ltd. is 8,000 kg.

Which Standards and Quality Systems Apply to 17-4PH Forgings?

For general industrial work, ASTM A705 Gr 630 (forgings) or ASTM A564 Type 630 (bars). For aerospace, AMS 5643. For Europe, EN 10088-3 / 1.4542. For Japan, JIS SUS 630. For pressure equipment, ASME SA-564 / SA-705. For H₂S service, NACE MR0175 / ISO 15156 on top of the base specification. Jiangyin Jiangnan Metal is certified to ISO 9001:2015 and issues EN 10204 3.1 certificates as standard.

Quality management certification

ISO 9001:2015

Material and inspection standards followed

ASTM A564 Type 630 ASTM A693 Type 630 ASTM A705 Gr 630 AMS 5643 AMS 5604 AMS 5622 EN 1.4542 EN 10088-3 JIS SUS 630 NACE MR0175* EN 10204 3.1 EN 10204 3.2* ASTM A388 (UT) ASTM E165 / E1417 (PT)

* NACE MR0175 / ISO 15156 sour-service compliance for 17-4PH requires the H1150-M double-aged condition with hardness ≤33 HRC. EN 10204 3.2 third-party witnessed certificates are issued through client-nominated inspection bodies (Lloyd's, DNV, BV, ABS or TÜV) on a per-order basis.

Quality assurance and non-conformance policy

Production quality gates

Each 17-4PH / UNS S17400 order passes six mandatory hold points where production cannot continue without QA sign-off: raw-material chemistry verification; forging-temperature compliance; post-forging ultrasonic inspection; heat-treatment chart approval; mechanical test acceptance; and final NDE plus dimensional inspection. Customer-witnessed hold points can be added on request at no charge.

Non-conformance handling

Any out-of-specification finding triggers a formal non-conformance report within 24 hours. Root-cause analysis is completed within five working days. The customer receives the report with a proposed disposition (rework, regrade, scrap, or use-as-is under concession) before any action is taken. There is no silent rework.

Replacement guarantee

Material found to be non-conforming within six months of delivery, verified by independent third-party test, is replaced free of charge including freight. Shipping and test documentation is retained for ten years to support any warranty claim.

Witness inspection rights

Customers retain an unrestricted right to witness any production stage, including chemistry analysis, heat-treatment cycles, mechanical testing and final NDE. Witness visits are coordinated with our QA team, and a dedicated quality liaison is assigned for ASME and aerospace customers.

How to Specify a 17-4PH / UNS S17400 Forging Order

Seven steps: state the generic designation rather than the trademark; choose the H-condition; provide the drawing; state whether material ships in Condition A or aged; define NDE; state the certificate type; then give quantity, delivery date and destination. The H-condition is the one decision that does not arise with most other stainless grades, and it is where most ambiguity enters a purchase order.

Confirm the material designation

State the grade as UNS S17400 / ASTM A705 Gr 630 for forgings, or ASTM A564 Type 630 for bar, plus AMS 5643 for aerospace, EN 1.4542 for European projects or JIS SUS 630 for Japanese projects. Avoid writing "17-4 PH®" alone, because that is a Cleveland-Cliffs trademark and implies their material specifically.

Select the H-condition

Match the aging condition to your strength-versus-toughness need: H900 for highest strength, H1025 for general purpose, H1075 for pump shafts, H1150 for best toughness, H1150-M for NACE sour service. When in doubt, H1025 is the most common general-purpose choice, or use the H-Condition Wizard.

Provide the drawing

Submit a 2D drawing or 3D model with all critical dimensions, tolerances, surface roughness and grain-flow requirements. See the drawing specification guide for a ready-made callout block.

Specify the supply condition

State whether material ships in Condition A (solution annealed, for further fabrication) or in the final aged H-condition. Most finished parts are supplied aged. Leaving this out is the single most common cause of shipment disputes.

Define NDE requirements

Specify ultrasonic acceptance per ASTM A388, plus penetrant or magnetic-particle requirements per ASTM E165 / E1417. For pressure-containing parts, specify ASME Section V acceptance criteria; for aerospace, AMS-STD-2154 Class A.

Specify certification

State whether EN 10204 3.1 (mill certificate) or 3.2 (third-party witnessed) is required. For NACE service, specify NACE MR0175 / ISO 15156 compliance and the required hardness limit.

Give quantity and delivery target

Provide order quantity, target delivery date and shipping destination. Standard 17-4PH lead time is 8–10 weeks; AMS-certified aerospace material is 12–14 weeks.

Ten Mistakes Engineers Make When Ordering 17-4PH Forgings

The most frequent and most expensive errors are: specifying the trademark instead of the generic designation; using H900 in chloride service; forgetting H1150-M for sour service; welding in the aged condition; aging after finish machining; running above 315 °C; omitting the supply condition; mixing ASTM and EN limits; under-specifying NDE on fatigue-critical parts; and omitting grain-flow direction.

  • Specifying "17-4 PH®" without recognising it is a registered trademark
    A purchase order requiring "17-4 PH" can technically only be filled by Cleveland-Cliffs. Independent producers cannot legally supply under that exact name.
    Fix: specify the generic designation, "UNS S17400 / ASTM A705 Gr 630" for forgings, or ASTM A564 Type 630 for bar.
  • Using H900 in chloride environments
    H900 has the highest strength but the greatest susceptibility to chloride stress-corrosion cracking. Marine air, food processing and chlorinated cooling water all count as chloride service.
    Fix: use H1100 or H1150 for any chloride exposure. Verify with the H-Condition Wizard.
  • Forgetting H1150-M for sour service
    Where H₂S partial pressure reaches 0.3 kPa, NACE MR0175 / ISO 15156 mandates the H1150-M double-aged condition at 33 HRC or lower. Anything else fails certification.
    Fix: run the NACE compliance checker before specifying anything for oil and gas.
  • Welding 17-4PH in the aged condition
    Welding aged material over-ages the heat-affected zone and drops local strength by 20–40 %. Welds made in aged material rarely meet the original specification.
    Fix: weld in Condition A, then re-solution and age the whole welded assembly.
  • Aging after finish machining
    Aging causes a dimensional change of under 0.1 %, but on a tight-tolerance feature such as an Ø80 H7 bore that still exceeds tolerance, and thin-wall parts can distort.
    Fix: rough machine in Condition A → solution treat → age → finish machine. Or compensate for the shrinkage in CAD.
  • Using 17-4PH above 315 °C continuously
    Continuous service above about 315 °C progressively over-ages the precipitates, and the strength loss is permanent. Failure at design load is not uncommon.
    Fix: check the service-temperature tool, then move to A286 (≤700 °C) or Inconel 718 (≤650 °C continuous).
  • Failing to state the supply condition
    Many purchase orders say "17-4PH H1025" without saying whether the part should arrive in Condition A, ready for the customer to machine and age, or in final H1025 ready to install.
    Fix: write explicitly "supplied in Condition A" or "supplied in final H1025 condition, post-machined and aged".
  • Mixing ASTM and EN limits without confirmation
    EN 1.4542 has tighter sulfur (≤0.015 %) and silicon (≤0.70 %) than ASTM. Material made to ASTM limits may not satisfy the requirements for EN-marked equipment.
    Fix: when exporting to the EU or supplying CE-marked equipment, specify EN 1.4542 explicitly, or require a multi-designation certificate confirming EN compliance.
  • Under-specifying NDE on fatigue-critical components
    Pump shafts and rotor components fail by surface-initiated fatigue. Specifying only "visual inspection" misses the surface defects that cut fatigue strength by 30–50 %.
    Fix: specify UT per ASTM A388 Class B plus PT per ASTM E165 on machined surfaces. For aerospace, AMS-STD-2154 Class A UT is mandatory.
  • Specifying section thickness without grain-flow direction
    17-4PH is anisotropic: transverse toughness runs 10–20 % below longitudinal. On impact-critical parts the grain flow must align with the primary loading direction.
    Fix: for forged parts above 50 mm cross-section, state "longitudinal grain flow parallel to the primary axis" and verify by macroetch per ASTM E381.

How Do You Specify 17-4PH on an Engineering Drawing?

Use a callout block that names the generic designation, the H-condition with its actual cycle, the hardness band and where it is verified, the grain-flow requirement, the NDE standards, the certificate type, the surface finish and the marking requirement. The template below is accepted under ASTM, AMS, EN and JIS practice and removes almost all ordering ambiguity.

MATERIAL: UNS S17400 / ASTM A705 Gr 630 (also satisfies ASTM A564 Type 630, AMS 5643, EN 1.4542, JIS SUS 630) CONDITION: H1025: solution 1040 °C/AC + age 552 °C/4 h/AC // or H1150-M for NACE sour service HARDNESS: 35–42 HRC, verified at locations A, B and C // for NACE work: "≤33 HRC verified" GRAIN FLOW: Longitudinal, parallel to the primary axis (verify by macroetch per ASTM E381) NDE: UT per ASTM A388 Class B PT per ASTM E165 Type I, Method C, Sensitivity 3 // use AMS-STD-2154 Class A for aerospace CERTIFICATION: EN 10204 3.1 mill certificate // or 3.2 with third-party witness on request SURFACE: Ra ≤1.6 µm on bearing journals Ra ≤3.2 µm elsewhere MARKING: Heat number, condition and drawing number vibro-etched on a non-functional surface

Copy this template into the material callout box on your drawing and adjust the H-condition, hardness and NDE to suit the application, see the H-Condition Wizard for selection. For sour service, replace "H1025" with "H1150-M double aged" and the hardness band with "≤33 HRC verified".

Instant RFQ Specification Generator

Pick the H-condition and the rest of your specification to get a complete RFQ text, ready to email, WhatsApp or download.
Free tool

Request a Quote: 17-4PH / UNS S17400 Forging Parts

For pump shafts, valve bodies, marine hardware or aerospace structural forgings in 17-4PH / UNS S17400, send your specification (including the required H-condition) and we reply within 24 hours with pricing, lead time and confirmation of the applicable standards. For complex enquiries, use the RFQ generator above to produce a complete specification sheet first.

Where Is 17-4PH / UNS S17400 Used?

Pumps and valves account for about a third of 17-4PH forging demand, followed by oil and gas, aerospace structural parts, chemical and process equipment, marine hardware, and a small share in nuclear, food and research. Pump shafts in H1025 or H1075 are the single largest application worldwide.

17-4PH shipments by industry

Approximate distribution of the 387 17-4PH / UNS S17400 forging orders shipped by Jiangyin Jiangnan Metal Co., Ltd. between Q3 2021 and Q2 2026, by end-user industry. Customer names are protected by non-disclosure agreement.

17-4PH 387 orders 2021–2026
Pumps and valves35 %
Oil and gas22 %
Aerospace18 %
Chemical and process12 %
Marine and shipbuilding8 %
Other, nuclear, food, R&D5 %

Pump shafts and impellers, the largest single application of 17-4PH worldwide. H1025 or H1075 delivers high strength, good corrosion resistance and excellent fatigue performance for centrifugal pumps in chemical, water and marine service.

Sector: pump industry, chemical, water, marine

Oil and gas valves and wellhead components, typically H1150-M double aged for NACE MR0175 compliance, used in choke valves, valve bodies, valve trim and sucker-rod couplings.

Sector: oil and gas: NACE MR0175

Aerospace structural forgings: H1025 or H1150 to AMS 5643, used in hydraulic actuator bodies, brackets, accessory-drive components and landing-gear parts where PH 13-8 Mo is not required.

Sector: commercial and military aerospace

Marine hardware, propeller shafts, rudder shafts and deck hardware for splash-zone or short-immersion service. Continuous full-immersion seawater service requires an upgrade to duplex or super-duplex.

Sector: shipbuilding and marine

Food and chemical processing equipment, agitator shafts, mixer paddles and high-strength components in non-chloride environments, where the higher strength allows thinner and lighter parts than 304L.

Sector: food and process industries

Nuclear power components, control-rod drive mechanisms, primary-coolant pump shafts and instrument-tube connections, where moderate strength, corrosion resistance and ferromagnetic behaviour are all needed together.

Sector: nuclear power

Industry-specific specification guides

Each industry has its own dominant H-condition, certification pattern and design pitfalls. These six guides distil what matters in the highest-volume 17-4PH sectors, with a ready-made specification callout for each.

Pumps and rotating equipment

17-4PH for pump shafts, impellers and casings

Dominant condition: H1075 for shafts, the best fatigue and corrosion balance. H1025 for impellers and casings, H1150 where chloride exposure is continuous.

Critical factor: shaft critical speed must stay below 70 % of operating speed. Prefer H1075 over H900: the endurance limits are 520 MPa against 620 MPa, but H1075 is far less susceptible to chloride SCC over a multi-year pump life.

Typical callout"UNS S17400 / ASTM A705 Gr 630, H1075 (580 °C/4 h/AC), UT per ASTM A388 Class B, PT per ASTM E165 on bearing journals (Ra ≤1.6 µm), EN 10204 3.1."
Valve industry

17-4PH for valve bodies, stems and trim

Dominant condition: H1025 for bodies and stems in general industrial service, H1150-M for anything in oil and gas, H900 only for non-corrosive high-pressure trim such as seats.

Critical factor: API 6A sour-service trim classes impose hardness ceilings that only the double-aged H1150-M condition can meet. Where castings are used instead, verify the ASME B16.34 pressure-temperature rating separately.

Typical callout"UNS S17400 / ASTM A705 Gr 630, H1150-M double aged (760 °C/2 h + 621 °C/4 h), hardness ≤33 HRC verified at three locations, NACE MR0175 / ISO 15156-3 compliance, EN 10204 3.2 witnessed."
Aerospace structural

17-4PH to AMS 5643, actuators and brackets

Dominant condition: H1025 for general structural work, H1150 only where a high-fatigue regime demands maximum impact toughness. H900 is not used for aerospace structural parts.

Critical factor: AMS 5643 mandates transverse tensile tests, clean melting, macroetch grain-flow verification, Charpy minimums and AMS-STD-2154 Class A ultrasonic inspection, plus source approval from the prime contractor.

Typical callout"AMS 5643, Condition H1025, clean melted, longitudinal grain flow per ASTM E381, UT per AMS-STD-2154 Class A, PT per ASTM E1417 Type I Method C Sensitivity 3, EN 10204 3.1 plus AMS source-approval flow-down."
Oil and gas, sour service

17-4PH for wellhead, christmas tree and subsea

Dominant condition: H1150-M double aged, the only 17-4PH condition compliant with NACE MR0175 / ISO 15156-3 for sour service, with hardness ≤33 HRC verified across the whole part.

Critical factor: hardness must be mapped at multiple locations including any weld heat-affected zone. For subsea and deepwater, also verify Charpy impact at the lowest service temperature. Above about 175 °C in sour service, move to Inconel 718 or 925.

Typical callout"UNS S17400 / ASTM A705 Gr 630, H1150-M (760 °C/2 h + 621 °C/4 h, both air cooled), hardness ≤33 HRC mapped, NACE MR0175 / ISO 15156-3 Table A.20 compliance statement, EN 10204 3.2 with DNV, BV or Lloyd's witness."
Marine and shipbuilding

17-4PH for propeller and rudder shafts

Dominant condition: H1150 for splash-zone or short-immersion service. Avoid H900 and H925, the chloride SCC risk is too high. For continuous full immersion, upgrade to 2205 duplex or super-duplex.

Critical factor: the PREN of 17-4PH is about 16–17, well below the 32–35 needed for pit-free seawater service. Limit exposure to splash zone, intermittent submersion or freshwater-flushed environments. Class-society approval (DNV, BV, LR, ABS, KR, CCS) normally requires a 3.2 certificate.

Typical callout"UNS S17400 / ASTM A705 Gr 630, H1150 (621 °C/4 h/AC), UT per ASTM A388 Class A or B, surface PT, EN 10204 3.2 with class-society witness."
Food and process

17-4PH for agitator shafts and mixer paddles

Dominant condition: H1025 for general non-chloride food and chemical service, H1075 for fatigue-loaded agitator shafts, H1150 for any chloride-containing process fluid such as cleaning solutions or brine.

Critical factor: hygienic-design compliance for food contact normally requires a surface finish of Ra ≤0.8 µm, typically electropolished. 17-4PH is harder to electropolish than austenitic grades, so coordinate with the finisher early. For process fluids below pH 3, upgrade to 904L or duplex.

Typical callout"UNS S17400 / ASTM A705 Gr 630, H1075, surface Ra ≤0.8 µm post-electropolish on contact surfaces, EN 10204 3.1 with traceability to the forging stage."

Representative Project Scenarios

The following are representative project scenarios rather than named references. Specific project performance data and customer references are available under non-disclosure agreement on request.

Industry: pump manufacturing Component: centrifugal pump shaft Material: UNS S17400, H1075

17-4PH H1075 pump shaft for chemical process service

Typical challenge: chemical process pump shafts need high strength for deflection control, good corrosion resistance against the process fluid, and excellent fatigue resistance under reversed bending and torsion.

Typical solution: an open-die forged UNS S17400 shaft, Ø180 mm × 2.5 m long, supplied in H1075 (about 1,000 MPa UTS and 860 MPa yield). Solution treated at 1040 °C with air cool, then aged at 580 °C for 4 hours and air cooled. Ultrasonic acceptance per ASTM A388 Class B; surface penetrant inspection per ASTM E165.

Documentation: EN 10204 3.1 as standard; 3.2 with TÜV or BV witness available on request.

Industry: oil and gas Component: wellhead valve body Material: UNS S17400, H1150-M, NACE MR0175

17-4PH H1150-M valve body for sour-service wellhead

A wellhead valve body for sour gas requires NACE MR0175 / ISO 15156 compliance, which limits 17-4PH to the double-aged H1150-M condition at 33 HRC or below. A forged block of UNS S17400 of about 600 kg single-piece weight is double aged on the standard cycle of 760 °C for 2 hours then 621 °C for 4 hours, with final hardness verified at 33 HRC maximum. A NACE compliance statement is included on the certificate. Lead time runs 12–14 weeks including third-party witness of the heat treatment.

Industry: aerospace Component: hydraulic actuator body Material: UNS S17400, AMS 5643, H1025

17-4PH H1025 aerospace hydraulic actuator forging

A near-net-shape forging for an aircraft hydraulic actuator body of about 25 kg single-piece weight, supplied to AMS 5643 in H1025. Ultrasonic inspection per AMS-STD-2154 Class A; penetrant inspection per ASTM E1417 Type I, Method C, Form a-1, Sensitivity Level 3. Full chemistry, mechanical and grain-flow verification appear on the certificate, issued as EN 10204 3.1 with optional aerospace OEM source-approval flow-down.

Glossary of Key 17-4PH Terms

17-4 PH®
Registered trademark of Cleveland-Cliffs Inc. (formerly AK Steel / Armco) for the original 17 % Cr – 4 % Ni – Cu precipitation-hardening stainless steel. Generic equivalents: UNS S17400, ASTM A564 Type 630, ASTM A705 Gr 630, AMS 5643, EN 1.4542, JIS SUS 630.
UNS S17400
Generic Unified Numbering System designation for the 17 % Cr – 4 % Ni – Cu – Nb precipitation-hardening martensitic stainless steel.
AISI 630
Legacy American Iron and Steel Institute designation for the 17-4PH chemistry. AISI no longer maintains active steel-numbering specifications, but AISI 630 remains widely used on legacy drawings, datasheets and procurement specifications. Fully equivalent to UNS S17400 / ASTM A564 Type 630.
ASTM A564 Type 630
Generic ASTM specification for the 17-4PH chemistry in bars and shapes.
ASTM A705 Gr 630
Generic ASTM specification for the 17-4PH chemistry in forgings, the correct specification to cite on a forging purchase order.
AMS 5643
Aerospace Material Specification for 17-4PH bars, forgings, tubing and rings; adds transverse testing, Charpy limits, clean melting, grain-flow verification and Class A ultrasonic inspection.
Condition A
Solution-annealed condition, 1040 °C then air cool to below 30 °C. Martensitic and machinable but not yet aged; hardness 38 HRC maximum.
H900
Aged at 482 °C (900 °F) for 1 hour. Highest strength: 1,310 MPa UTS, 1,170 MPa yield, 40 HRC minimum. Lowest toughness and the highest chloride SCC risk.
H1025
Aged at 552 °C (1025 °F) for 4 hours. The most common general-purpose condition: 1,070 MPa UTS, 1,000 MPa yield, 35 HRC minimum.
H1075
Aged at 580 °C (1075 °F) for 4 hours: 1,000 MPa UTS, 860 MPa yield, 32 HRC minimum. Common for pump shafts, with good fatigue resistance.
H1150
Aged at 621 °C (1150 °F) for 4 hours: 930 MPa UTS, 725 MPa yield, 28 HRC minimum. Best impact toughness and chloride SCC resistance of the single-stage conditions.
H1150-M (double aged)
Two-stage cycle, 760 °C for 2 hours then 621 °C for 4 hours, for maximum impact toughness. Hardness ≤33 HRC; the only 17-4PH condition accepted for NACE sour service.
Precipitation hardening
Strengthening mechanism in which copper-rich ε precipitates form in the martensitic matrix during aging, raising strength without a large loss of corrosion resistance.
PREN
Pitting Resistance Equivalent Number, calculated as %Cr + 3.3 × %Mo + 16 × %N. 17-4PH scores about 16–17 because it carries no deliberate molybdenum, which is why it is not used for permanent seawater immersion.
NACE MR0175 / ISO 15156
Standard governing materials for H₂S-containing oil and gas service. Limits 17-4PH to the H1150-M condition at 33 HRC maximum.
EN 1.4542
European designation X5CrNiCuNb16-4 per EN 10088-3, the same chemistry as UNS S17400 with tighter sulfur and silicon limits.
EN 10204 3.1 / 3.2
Inspection document types. A 3.1 certificate is issued by the manufacturer's own independent quality department; a 3.2 certificate is countersigned by a third-party inspector nominated by the purchaser.

Frequently Asked Questions: 17-4PH / UNS S17400

Are 17-4PH, AISI 630, UNS S17400, ASTM A564 Type 630, EN 1.4542 and JIS SUS 630 the same material?
Yes: they all refer to the identical 17 % Cr – 4 % Ni – Cu – Nb martensitic precipitation-hardening stainless steel.
  • 17-4 PH®, registered trademark of Cleveland-Cliffs Inc., for material made by them.
  • UNS S17400, generic Unified Numbering System designation.
  • AISI 630, legacy AISI designation, still common on drawings.
  • ASTM A564 Type 630, generic ASTM specification for bars and shapes.
  • ASTM A705 Grade 630, generic ASTM specification for forgings.
  • AMS 5643, aerospace specification for bars, forgings, tubing and rings.
  • EN 1.4542 / X5CrNiCuNb16-4: European designation per EN 10088-3.
  • JIS SUS 630: Japanese designation per JIS G 4303 / G 4318.

Trademark notice: 17-4 PH® is a registered trademark of Cleveland-Cliffs Inc. Material produced by Jiangyin Jiangnan Metal Co., Ltd. is correctly described as UNS S17400 / ASTM A564 Type 630 / ASTM A705 Gr 630 / AMS 5643 / EN 1.4542. We are not affiliated with Cleveland-Cliffs Inc.

What are the H-conditions of 17-4PH and which should I choose?
The H-number is the aging temperature in degrees Fahrenheit. The standard conditions are:
  • H900: 482 °C, ~1,310 MPa UTS, 40 HRC. Highest strength; tooling and fasteners.
  • H925: 496 °C, ~1,170 MPa UTS, 38 HRC. A small toughness gain over H900.
  • H1025: 552 °C, ~1,070 MPa UTS, 35 HRC. The most common general-purpose condition.
  • H1075: 580 °C, ~1,000 MPa UTS, 32 HRC. Pump shafts and fatigue applications.
  • H1100: 593 °C, ~965 MPa UTS, 31 HRC. Heavy industrial sections.
  • H1150: 621 °C, ~930 MPa UTS, 28 HRC. Best impact toughness and chloride SCC resistance.
  • H1150-M: double aged, 760 °C/2 h + 621 °C/4 h. Maximum toughness, NACE sour-service compliance.
When in doubt: H1025 for general industrial, H1075 for pump shafts, H1150-M for sour-service oil and gas.
Is EN 1.4542 the same as ASTM A564 Type 630? Are AMS 5643 and JIS SUS 630 identical too?
Functionally equivalent, but not identical. The chemistry and test limits differ in subtle but real ways:
  • ASTM A564 Type 630 (US, general bars), the baseline: S ≤0.030, Si ≤1.00, Mn ≤1.00, Cr 15.0–17.5.
  • AMS 5643 (US aerospace), the same chemistry, but adds clean melting, transverse tensile tests, tighter Charpy limits, grain-flow verification and Class A ultrasonic inspection.
  • EN 1.4542 (Europe), tighter: S ≤0.015, half the ASTM limit; Si ≤0.70; Cr narrowed to 15.0–17.0; but Mn up to 1.50 and Mo up to 0.60 permitted.
  • JIS SUS 630 (Japan), essentially identical to ASTM A564.

A single heat made to EN 1.4542 limits satisfies all the others simultaneously. We supply multi-designation certificates on request, see the standards comparison above.

What is the chemical composition of 17-4PH?
Per ASTM A564 Type 630: C 0.07 max, Mn 1.00 max, Si 1.00 max, Cr 15.00–17.50, Ni 3.00–5.00, Cu 3.00–5.00, Nb+Ta 0.15–0.45, P 0.040 max, S 0.030 max, balance Fe; all weight per cent.
What is the maximum service temperature of 17-4PH?
About 315 °C (600 °F) for continuous service. Above that the precipitation hardening over-ages and strength is permanently lost. For higher temperatures see our A286 / UNS S66286 page (about 700 °C) or use Inconel 718 (about 650 °C). Check your specific case with the service-temperature tool.
What is the density of 17-4PH, and how do I estimate forging weight?
The density of 17-4PH / UNS S17400 is 7.75 g/cm³ (0.280 lb/in³). Multiply the finished part volume in cm³ by 7.75 and divide by 1,000 for kilograms, then add 20–35 % machining stock for the rough forging weight. The weight calculator does this for shafts, discs, rings, blocks and hollow cylinders.
Is 17-4PH magnetic?
Yes. 17-4PH has a martensitic microstructure in Condition A and in every aged condition and is ferromagnetic, with relative permeability typically µᵣ ≈ 95. This distinguishes it from austenitic stainless steels such as 304, 316 and 904L, which are essentially non-magnetic.
Is 17-4PH suitable for NACE MR0175 sour service?
Yes, but only in the H1150-M double-aged condition with hardness ≤33 HRC, per NACE MR0175 / ISO 15156-3 Table A.20. No other H-condition qualifies. Hardness must be verified across the whole part, including any weld heat-affected zone. Above about 175 °C in sour service, a nickel alloy such as Inconel 718 or 925 is normally required. Screen your case with the NACE compliance checker.
How does 17-4PH compare to PH 13-8 Mo?
PH 13-8 Mo (UNS S13800) is the premium aerospace alternative:
  • cleaner chemistry, lower phosphorus and sulfur, so better transverse toughness;
  • higher strength, about 1,520 MPa UTS in H1000 against about 1,070 MPa for 17-4PH H1025;
  • better corrosion resistance, the molybdenum addition raises PREN from about 17 to about 22;
  • roughly two to three times the price.
17-4PH is the general-purpose workhorse; PH 13-8 Mo is reserved for critical aerospace structural applications such as landing gear and rotor heads. See our PH13-8Mo page.
Can 17-4PH be welded?
Yes: it is one of the most weldable PH stainless grades. Use matching filler per AMS 5825 / 5826, or generic ER630. Weld in Condition A; a post-weld solution treatment plus aging is recommended for full-strength service. Preheat is not normally required for thin sections, while thick or restrained joints benefit from 150 °C preheat.
Does 17-4PH change size during aging?
Yes, but only slightly, under 0.1 %, normally a small contraction. On tight-tolerance features such as H7 bores this can still exceed tolerance, so the recommended sequence is rough machine in Condition A, solution treat, age, then finish machine.
Should I write 17-4PH or ASTM A705 Grade 630 on a forging purchase order?
For a forging, write ASTM A705 Grade 630, which is the forging-specific ASTM specification, rather than ASTM A564 Type 630, which covers bars and shapes. Writing "17-4 PH" alone names a Cleveland-Cliffs trademark and can technically only be filled by that producer, so use the generic designation when sourcing from an independent forge.
What is the maximum forging size available in 17-4PH?
Jiangyin Jiangnan Metal Co., Ltd. produces 17-4PH / UNS S17400 forged shafts up to 8 m long, discs up to Ø1,800 mm, seamless rolled rings up to 2,500 mm outside diameter and bar from Ø25 mm to Ø500 mm, with single-piece weights up to 8,000 kg.
What is the lead time for 17-4PH forgings?
Standard 17-4PH forgings in Condition A or in H1025, H1075 or H1150 typically ship in 8–10 weeks from order confirmation. AMS 5643 aerospace-certified material with the full quality chain extends to 12–14 weeks. Common bar sizes held in Condition A stock can sometimes ship in 4–6 weeks.
Who supplies 17-4PH / UNS S17400 forgings, and how do I request a quote?
Jiangyin Jiangnan Metal Co., Ltd. is an open-die forging factory founded in 2008 at No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province, China, exporting to more than 40 countries. It supplies custom 17-4PH / UNS S17400 / ASTM A705 Gr 630 forgings in every H-condition, with EN 10204 3.1 certification as standard and 3.2 third-party witnessed certification on request.

Telephone +86-189-2135-9659, e-mail sales@steelforgepieces.com, or use the RFQ generator to produce a complete specification sheet in about a minute.

Reference Data Appendix: The Numbers Behind the Tools

Every figure used by the twelve interactive tools on this page is published below as a plain table, so the data can be read, printed, quoted or checked without running any script. The same dataset is available in machine-readable form at 17-4ph-data.json.

A1: Aging temperature versus properties (aging-curve tool)

Table A1: 17-4PH / UNS S17400 properties by aging temperature
ConditionAging temp (°C)Aging temp (°F)UTS (MPa)YS (MPa)Hardness (HRC)Charpy V, RT (J)Chloride SCC riskTypical use
H900482900131011704018HighTooling, fasteners
H925496925117010703822HighAerospace fasteners
H10255521025107010003535ModerateGeneral purpose
H1075580107510008603250ModeratePump shafts
H110059311009657953160LowHeavy industrial
H115062111509307252875LowMarine, severe service
H1150-M760 + 6211400 + 1150795515≤33 (typ. 24)135LowestNACE sour service
Condition Anonenone1030760≤3830ModerateMachining, welding stock

A2: Fatigue endurance limits (S-N tool)

Table A2: rotating-bending fatigue data, R = −1, smooth specimen, room temperature
ConditionUTS (MPa)Stress at 10³ cycles (MPa)Endurance limit at 10⁷ cycles (MPa)Endurance ratio Se/UTS
H900131011796200.47
H102510709635900.55
H107510009005200.52
H11509308374600.49

Surface-finish knock-down factors used in design: polished 1.0; ground 0.85–0.9; as-machined 0.6–0.8; as-forged 0.4–0.6. Apply a mean-stress correction by the modified Goodman relation. Apply a design factor of at least 2 on stress or 10 on cycles.

A3: Precipitate state by H-condition (microstructure tool)

Table A3: approximate copper-rich ε precipitate state by aging condition
ConditionMean precipitate size (nm)Relative densityCoherency with matrixHardness (HRC)UTS (MPa)
Condition A≈1 (Cu still in solution)NegligibleNo precipitates≤381030
H900≈3Very highFully coherent401310
H925≈4Very highCoherent381170
H1025≈7HighCoherent, strain beginning to relax351070
H1075≈11MediumPartly coherent321000
H1100≈15MediumPartly incoherent31965
H1150≈22LowMostly incoherent, ripening started28930
H1150-M≈35Very lowFully incoherent, over-aged≤33 (typ. 24)795

A4: Base machining parameters (machinability tool)

Table A4: base parameters for coated carbide on 17-4PH H1025, before condition and tool factors
OperationCutting speed Vc (m/min)Feed (mm/rev or mm/tooth)Depth of cut (mm)Tool life (min)
Turning750.252.025
Face milling800.182.530
End milling600.101.020
Drilling, HSS140.108
Drilling, carbide450.1520
Tapping46
Reaming180.180.330
Table A4b: speed multipliers applied to the base values above
17-4PH conditionSpeed factorTool materialSpeed factor
Condition A (≈33 HRC)1.10Coated carbide (TiAlN / AlCrN)1.00
H1150 (28 HRC)1.20Uncoated carbide0.80
H1100 (31 HRC)1.10Cermet0.95
H1075 (32 HRC)1.05Ceramic (light cuts only)1.50
H1025 (35 HRC)1.00CBN (finishing only)2.20
H925 (38 HRC)0.85HSS-Co (M42)0.30
H900 (40 HRC)0.70

A5: Indicative material price index (cost tool)

Table A5: indicative mill prices for hot-forged round bar, FOB China, Q3 2026
Material and conditionIndicative price (USD/kg)Minimum yield strength (MPa)Cost per MPa per kg (USD)
AISI 4340, quenched and tempered3.511000.0032
17-4PH H10258.010000.0080
15-5PH H10259.010000.0090
316L, annealed9.01700.0529
17-7PH RH95011.012800.0086
PH 13-8 Mo H100025.014100.0177
A286, solution treated and aged30.05850.0513
Inconel 718, solution treated and aged60.010300.0583

Indicative only, for relative comparison. Prices move weekly with the LME nickel and ferro-chrome indices and depend on quantity, size, certification level and lead time. Forging conversion, machining and finishing are separate cost lines. Contact sales@steelforgepieces.com for a current quotation.

A6: Strength retention against service temperature (service-temp tool)

Table A6: approximate room-temperature strength retained after exposure
Service temperatureAfter 10,000 hAfter 100,000 hVerdictRecommended action
Up to 200 °C≈100 %≈100 %SafeAny H-condition, no restriction
200–280 °C97–99 %95–97 %AcceptablePrefer H1100 or H1150 for stability
280–315 °C94–97 %90–94 %CautionUse H1100 / H1150; add design margin
315–400 °C70–80 %<70 %Not recommendedMove to A286 or Inconel 718
Above 400 °C<60 %<50 %Do not useA286 (≤700 °C), Inconel 718/625, Nimonic 80A

A7: NACE MR0175 / ISO 15156 acceptance summary

Table A7: sour-service acceptance for 17-4PH / UNS S17400
ParameterRequirementNote
Sour-service thresholdH₂S partial pressure ≥0.3 kPa (0.05 psi)Below this, NACE MR0175 does not apply
Accepted H-conditionH1150-M double aged onlyH900, H925, H1025, H1075, H1100, H1150 and Condition A are all rejected
Hardness ceiling33 HRC maximumVerified across the whole part, including weld HAZ
Aging cycle760 °C / 2 h + 621 °C / 4 h, both air cooledFurnace charts required on the certificate
Practical temperature limitAbout 175 °C in sour serviceAbove this, move to Inconel 718 or 925
ReferenceNACE MR0175 / ISO 15156-3 Table A.20Always check the edition in force at contract date

A8: Forging and heat-treatment parameters

Table A8: process parameters used in production at Jiangyin Jiangnan Metal
Process stepParameterTolerance / note
Forging temperature1170–1230 °CFinish above 950 °C
Forging ratio≥4:1Required to meet AMS 5643 grain flow
Post-forge coolingFurnace coolAvoid dwell in the 565–870 °C sigma range
Solution treatment1040 °C±10 °C, 30 min per 12 mm of section
Quench from solutionAir cool to below 30 °CUninterrupted; required for full martensite
Aging, single stage482–621 °C per H-condition±8 °C, 1 h for H900, 4 h for the rest
Aging, double (H1150-M)760 °C / 2 h then 621 °C / 4 hAir cool after each stage
Dimensional change on aging<0.1 %Normally a contraction
Welding fillerAMS 5825 / 5826, generic ER630Weld in Condition A; re-solution and age after
Preheat for weldingNone for thin; 150 °C for thick or restrainedReduces hydrogen-cracking risk
Post-plating bake190–220 °C for 4–24 hPrevents hydrogen embrittlement

About the Manufacturer and the Authors of This Page

This page is written and maintained by the metallurgical engineering team of Jiangyin Jiangnan Metal Co., Ltd., an open-die forging factory founded in 2008 in Jiangyin, Jiangsu (one of China's largest forging clusters) exporting 17-4PH and other alloy forgings to more than 40 countries under ISO 9001:2015.

Who wrote this

The technical content is compiled by the in-house metallurgical engineering team that plans and releases 17-4PH production at Jiangyin Jiangnan Metal, the same people who sign off heat-treatment charts, review ultrasonic reports and answer customer non-conformances. Property data is taken from the published standards listed under Technical References and cross-checked against our own tensile, hardness, Charpy and metallographic records. The page is reviewed at least twice a year, and the review date appears at the top.

What we actually do

We are a forging factory, not a trading company or stockist. Material is forged, heat treated, inspected and certified on our own premises under our own quality system. The equipment list under production capability is our own plant, and the delivery statistics are drawn from our own order records rather than industry averages.

What we do not claim

We do not hold the 17-4 PH® trademark and do not sell under it. We do not publish customer names, logos or testimonials without written permission, and we publish no star ratings or review scores, because we have no verified public review system to base them on. Prices shown anywhere on this page are indicative index figures, not offers. Any project-specific recommendation on this page should be confirmed by your own qualified materials engineer.

Corrections

If you find an error in any figure on this page (a property value, a standard reference, a heat-treatment parameter) please write to sales@steelforgepieces.com with the detail and the source. Corrections are made on the page and noted in the review date.

Jiangyin Jiangnan Metal Co., Ltd.: Open-Die Forging Factory
Address: No.1 Chengxiqiao Road, Zhouzhuang Town, Jiangyin City, Jiangsu Province 214423, China
Telephone / WhatsApp: +86-189-2135-9659 (0086-189-2135-9659)
E-mail: sales@steelforgepieces.com
Website: www.steelforgepieces.com
Founded: 2008  ·  Quality system: ISO 9001:2015  ·  Certificates: EN 10204 3.1 standard, 3.2 on request  ·  Languages: English, Chinese, Japanese  ·  Export markets: 40+ countries

How to Cite or Reuse This Page

This page may be quoted, printed and referenced freely with attribution to Jiangyin Jiangnan Metal Co., Ltd. and a link to the canonical URL. Suggested citation formats are given below for reports, specifications and academic work.

Suggested citation

Jiangyin Jiangnan Metal Co., Ltd. (2026). 17-4PH / AISI 630 / UNS S17400 / 1.4542 Forging Parts. Properties, H-Conditions, Standards and Applications. Jiangyin, Jiangsu, China. Last reviewed 21 September 2026. https://www.steelforgepieces.com/Stainless-Steel/17-4ph.html

Short form, for a drawing note or specification

Property data per Jiangyin Jiangnan Metal Co., Ltd., 17-4PH / UNS S17400 technical guide, rev. 2026-09-21, steelforgepieces.com

Machine-readable dataset

The property tables in the Reference Data Appendix are also published as JSON at https://www.steelforgepieces.com/Stainless-Steel/17-4ph-data.json, with credit line "Jiangyin Jiangnan Metal Co., Ltd.. 17-4PH / UNS S17400 forging data, 2026".

Terms

Text, tables and tools on this page are © 2026 Jiangyin Jiangnan Metal Co., Ltd. You may quote from them, reproduce individual tables and link to the page for engineering, educational and procurement purposes provided the source is named. The underlying standards themselves (ASTM, SAE AMS, EN, JIS, ISO and NACE documents) remain the copyright of their publishers and must be purchased from them; this page summarises requirements and does not reproduce the standards.

Technical References

Chemistry, mechanical property, heat-treatment and corrosion data on this page are drawn from the published standards and engineering references below. Test results appearing on our material certificates are independent and traceable to calibrated equipment in our own laboratory.

  1. ASTM A564/A564M, "Standard Specification for Hot-Rolled and Cold-Finished Age-Hardening Stainless Steel Bars and Shapes", ASTM International, West Conshohocken, PA.
  2. ASTM A705/A705M, "Standard Specification for Age-Hardening Stainless Steel Forgings", ASTM International.
  3. ASTM A693/A693M, "Standard Specification for Precipitation-Hardening Stainless and Heat-Resisting Steel Plate, Sheet, and Strip", ASTM International.
  4. SAE AMS 5643, "Steel, Corrosion-Resistant, Bars, Wire, Forgings, Mechanical Tubing, and Rings, 16Cr – 4.0Ni – 0.30Cb – 4.0Cu, Solution Heat Treated, Precipitation Hardenable", SAE International.
  5. SAE AMS 5604, "Steel, Corrosion-Resistant, Sheet, Strip, and Plate, 16Cr – 4.0Ni – 0.30Cb – 4.0Cu, Solution Heat Treated", SAE International.
  6. SAE AMS 2759/3, "Heat Treatment of Precipitation-Hardening Corrosion-Resistant and Maraging Steel Parts", SAE International.
  7. EN 10088-3:2014, "Stainless steels: Part 3: Technical delivery conditions for semi-finished products, bars, rods, wire, sections and bright products of corrosion resisting steels for general purposes", CEN, Brussels.
  8. EN 10250-4, "Open die steel forgings for general engineering purposes. Part 4: Stainless steels", CEN.
  9. JIS G 4303, "Stainless steel bars", Japanese Standards Association, Tokyo.
  10. JIS G 4318, "Cold finished stainless steel bars", Japanese Standards Association.
  11. NACE MR0175 / ISO 15156-3:2020, "Petroleum and natural gas industries. Materials for use in H₂S-containing environments in oil and gas production. Part 3: Cracking-resistant CRAs and other alloys", ISO, Geneva.
  12. ASM Handbook, Volume 1: Properties and Selection: Irons, Steels, and High-Performance Alloys, ASM International, Materials Park, OH; section on precipitation-hardening stainless steels.
  13. ASM Handbook, Volume 4D: Heat Treating of Irons and Steels, ASM International, section on precipitation-hardening stainless steels.
  14. ASM Specialty Handbook: Stainless Steels, J. R. Davis (ed.), ASM International.
  15. Hochanadel, P. W., Edwards, G. R., Maguire, M. C. and Baeslack, W. A. III, "Heat Treatment of Investment Cast PH 13-8 Mo Stainless Steel", Welding Journal, Vol. 73, No. 9, 1994.
  16. Habibi Bajguirani, H. R., "The Effect of Ageing upon the Microstructure and Mechanical Properties of Type 15-5 PH Stainless Steel", Materials Science and Engineering A, Vol. 338, 2002.
  17. API Specification 6A, "Specification for Wellhead and Tree Equipment", American Petroleum Institute.
  18. ASME Boiler and Pressure Vessel Code, Section II Part A (Ferrous Materials) and Section VIII Division 1, ASME.
  19. EN 10204, "Metallic products: Types of inspection documents", CEN.
  20. ASTM A388/A388M, "Standard Practice for Ultrasonic Examination of Steel Forgings", ASTM International.
  21. ASTM E165/E165M, "Standard Practice for Liquid Penetrant Testing for General Industry", ASTM International.
  22. ASTM E1417/E1417M, "Standard Practice for Liquid Penetrant Testing", ASTM International.
  23. ASTM E381, "Standard Method of Macroetch Testing Steel Bars, Billets, Blooms, and Forgings", ASTM International.
  24. Cleveland-Cliffs Inc., technical data sheet for 17-4 PH® stainless steel, clevelandcliffs.com.

Standards referenced are the most recent revisions known at the time of the last page review. For procurement, always cite the revision in force at the contract date. All trademarks and copyrights belong to their respective owners.

Copied to clipboard ✓