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SAE 4340 – UNS G43400

High-hardenability nickel-chromium-molybdenum low-alloy steel

Medium-carbon Ni-Cr-Mo steel with hardenability superior to 4140, which allows high strength and toughness in the core of large sections. Supplied annealed or quenched and tempered; VAR version (AMS 6414) for aerospace use.

Technical review Oct 2026 · minimum values per the cited standard; physical properties are typical; values marked * to be confirmed in the standard

FamilyAlloy steel
UNSG43400
W.Nr. / EN≈ 34CrNiMo6 – 1.6582 (EN ISO 683-2); ≈ 36CrNiMo4 – 1.6511
Carbon equivalent (IIW)≈ 0.85 (nominal composition)

Designations and equivalents

Designations of SAE 4340 – UNS G43400
SystemDesignation
UNS G43400
W.Nr./EN ≈ 34CrNiMo6 – 1.6582 (EN ISO 683-2); ≈ 36CrNiMo4 – 1.6511
DIN 34CrNiMo6
JIS SNCM439
Trade names 4340, BS 817M40 (EN24)
Others AMS 6414 (VAR), AMS 6415; E4340 (electric furnace)

Standards by product form

Standards for SAE 4340 – UNS G43400
FormStandard
Bar (composition) SAE J404 / ASTM A29
Quenched and tempered bar ASTM A434
Aerospace bar/forging AMS 6414 (VAR) / AMS 6415
Forging ASTM A668 / to customer specification
Mechanical tubing ASTM A519
Plate ASTM A829
Bolting ASTM A320 L43 (A194 grade 4 or 7 nuts)

Tolerances and HS codes

  • Forged bars (round and square): machining allowance from 2 mm (Ø 6–16 mm) to 24 mm (Ø 400–500 mm) on the diameter. E.g. Ø 100–125 mm finished: +7 mm, tolerance +6 / −0 (length up to 3,500 mm).
  • Forged discs: allowance of 4 to 9 mm on the diameter and 3 to 11 mm on the height, plus-only tolerance.
  • Cutting and machining: band saw −0 / +5 to +15 mm on length; waterjet +10 % of thickness on the diameter (min. 2 mm); machined parts −0 / +2 to +5 mm on the diameter. See the full tables (INF 002 and INF 003, the same for every alloy).
Tariff classification of SAE 4340: NCM, HS, HTS and CN by product form
FormNCM (Brazil, 8 digits)HS (international, 6 digits)HTS (USA, 10 digits)*CN (European Union, 8 digits)*
Forged bar7228.40.007228.407228.40.00007228 40 90
Hot-rolled bar7228.30.007228.307228.30.80417228 30 61
Plate (> 10 mm, width ≥ 600 mm)7225.40.907225.407225.40.30507225 40 40
Seamless pipe7304.19.007304.197304.19.50507304 19 10
Welded pipe7306.19.007306.197306.19.51507306 19 00
Flange and fitting7307.91.007307.917307.91.50307307 91 00

Tariff class: alloy steel (by chemical composition, under the Chapter 72 Notes and Section XV Note 5).

Pipe: 7304.19 and 7306.19 are line pipe for oil and gas pipelines; boiler, heat exchanger or process tubes go under 7304.39/7304.59 (seamless) and 7306.30/7306.50 (welded).

*: US and EU codes for reference. NCM per current legislation (General Rules of Interpretation, Notes to Chapters 72, 74 and 75 and Section XV Note 5). Confirm the final code with your customs broker according to the item size and finish. HS = first 6 digits of the NCM.

Chemical composition (%)

SAE J404 / ASTM A29

Chemical composition of SAE 4340 – UNS G43400, per SAE J404 / ASTM A29
ElementRange (%)
C 0.38 – 0.43
Mn 0.60 – 0.80
P ≤ 0.035
S ≤ 0.040
Si 0.15 – 0.35
Ni 1.65 – 2.00
Cr 0.70 – 0.90
Mo 0.20 – 0.30
Fe balance

Mechanical properties

Quenched and tempered, section Ø 40–100 mm (reference 34CrNiMo6 +QT, EN 10083-3 / ISO 683-2)

Mechanical properties of SAE 4340 – UNS G43400
PropertyValue
Yield strength ≥ 800 MPa
Tensile strength 1,000 – 1,200 MPa
Elongation ≥ 11%
Charpy V (20 °C) ≥ 45 J
Hardness, commercial Q&T ≈ 28 – 36 HRC (typical; UTS 930–1,080 MPa)
Hardness, annealed ≤ 248 HB

Typical physical properties

Typical values at 20 °C
PropertyValue
Density 7.85 g/cm³
Melting range ≈ 1,425 – 1,500 °C
Modulus of elasticity ≈ 205 GPa
Thermal conductivity (20 °C) ≈ 44 W/m·K
Thermal expansion (20–100 °C) ≈ 12.3 µm/m·K

Heat treatment, welding and machining

ItemUsual practice
Service temperature Up to ≈ 400 °C in structural service, always below the tempering temperature. Not indicated for prolonged high temperature (use Cr-Mo-V).
Heat treatment Annealing 830–850 °C, slow cooling. Normalizing 850–880 °C. Hardening: austenitize 830–860 °C, oil. Tempering 200–650 °C according to strength (avoid 250–400 °C, temper embrittlement). Accepts nitriding and induction hardening.
Welding Difficult welding (CE ≈ 0.85, cold cracking risk): preheat 250–350 °C, low-hydrogen consumables (AWS E11018-M / E12018-M or E9018-B3 according to strength; ER100S-1/ER120S-1), immediate post-weld tempering. Prefer welding annealed and heat treating afterwards.
Machining Fair in the annealed condition (≈ 50–55% of 1212); quenched and tempered it requires carbide and rigidity.

Filler metal for welding

The wire composition is usually not identical to the material: each page explains why.

Typical applications

  • Large-section shafts and spindles
  • Heavy transmission gears and crown wheels
  • Landing gear and aircraft structural components (VAR)
  • Highly stressed crankshafts and connecting rods
  • Forgings for oil and gas and mining
  • High-strength bolts
  • Drilling tools and mandrels
  • Pressure vessels and high-pressure hydraulic components
  • Rocket motor cases and defense components

Alternatives: 4140 for smaller sections and lower cost; 300M (4340 + Si, V) for strength > 1,900 MPa; 18Ni maraging for ultra-high strength; nitrided 8550 for surface wear.

SAE 4340: complete guide

Why choose 4340

Nickel (1.65 – 2.00%), added to chromium and molybdenum, gives 4340 greater hardenability than 4140. The part thus reaches high strength and toughness also in the core of large sections, where other alloy steels fall short. That is why it is chosen for highly stressed parts: transmission shafts and gears, landing gear, pressure vessels and defense components.

Supply condition

It is supplied annealed or quenched and tempered, typically with a tensile strength of 930 to 1,080 MPa. Annealed, it has good ductility: it can be bent, formed and machined by the usual methods. Oil quenching and tempering, or normalizing and tempering, raise strength and fatigue resistance.

Surface hardening

Parts already quenched and tempered accept induction or flame hardening and nitriding. The result is a hard surface, resistant to wear and abrasion, over a tough core that withstands shock and impact.

4340 for large-diameter bolting (A320 L43, "4340 PET")

In low-temperature studs above Ø 2½", 4140 (A320 L7) no longer hardens well at the core. ASTM A320 grade L43 uses 4340: C 0.38 – 0.43%, Mn 0.75 – 1.00%, Ni 1.65 – 2.00%, Cr 0.70 – 0.90% and Mo 0.20 – 0.30%, quenched and tempered. Up to Ø 4" it requires tensile ≥ 860 MPa (125 ksi), yield ≥ 724 MPa (105 ksi), elongation ≥ 16%, reduction of area ≥ 50% and Charpy ≥ 27 J (20 ft·lbf) at −101 °C. A194 grade 4 or 7 nuts.

In orders for Petrobras this material sometimes appears as "4340 PET"*. As with 4140, the purchase name should be the ASTM bolting specification. L43 does not appear in the materials table of one of the bolting supply procedures consulted (which lists B7, B7M, L7 and L7M); confirm in the requisition that it is accepted*. Rolled thread, stress relief and coating requirements are the same as for B7 studs.

Frequently asked questions

What is the chemical composition of SAE 4340?

Per SAE J404 / ASTM A29: C 0.38 – 0.43; Mn 0.60 – 0.80; P ≤ 0.035; S ≤ 0.040; Si 0.15 – 0.35; Ni 1.65 – 2.00.

Which standards cover SAE 4340?

Bar (composition): SAE J404 / ASTM A29. Quenched and tempered bar: ASTM A434. Aerospace bar/forging: AMS 6414 (VAR) / AMS 6415. Forging: ASTM A668 / to customer specification. Mechanical tubing: ASTM A519. Plate: ASTM A829. Bolting: ASTM A320 L43 (A194 grade 4 or 7 nuts).

Up to what temperature can SAE 4340 be used?

Up to ≈ 400 °C in structural service, always below the tempering temperature. Not indicated for prolonged high temperature (use Cr-Mo-V).

Which materials can replace SAE 4340?

4140 for smaller sections and lower cost; 300M (4340 + Si, V) for strength > 1,900 MPa; 18Ni maraging for ultra-high strength; nitrided 8550 for surface wear.

When should 4340 be used instead of 4140?

When the section is large or the part requires more core toughness. For the same reference (Ø 40 – 100 mm, quenched and tempered), 34CrNiMo6 has a yield strength ≥ 800 MPa, versus ≥ 650 MPa for 42CrMo4.

Can 4340 steel be welded?

Yes, with care: carbon equivalent ≈ 0.85, preheat of 250 – 350 °C, low-hydrogen consumable and tempering right after welding. The safest route is to weld annealed and quench and temper afterwards.

What is 4340 PET steel?

It is the name used in orders for 4340 intended for Petrobras bolts and studs*, usually large-diameter and low-temperature. The corresponding specification is ASTM A320 L43 (quenched and tempered 4340, Charpy ≥ 27 J at −101 °C, A194 grade 4 or 7 nuts). Order by the ASTM grade, not the nickname.

Need SAE 4340?Bars, forgings and parts with EN 10204 3.1 certificate.

See also

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