Steel Grade Datasheet

34CrNiMo6/ 1.6582 / ≈ 4340

Nickel-Chromium-Molybdenum Q&T Steel

Standard
EN 10083-3
Delivery Conditions
+A, +QT
Density
7.85 g/cm³
W.-Nr.
1.6582

What is 34CrNiMo6 steel?

34CrNiMo6 (Werkstoff No. 1.6582, ≈AISI 4340 / UK EN24) is a nickel-chromium-molybdenum high-strength quenched and tempered steel per EN 10083-3. The nickel addition delivers uniform through-hardening even in large sections (high hardenability) plus superior toughness. In the quenched and tempered (+QT) condition it provides a 600–1000 MPa yield and 800–1400 MPa tensile strength depending on section — the material for large shafts, gears and forgings under heavy load.

Chemical Composition

Cast analysis, % by weight (per the applicable EN standard)

ElementRange (%)
C0.30–0.38
Si≤ 0.40
Mn0.50–0.80
P≤ 0.025
S≤ 0.035
Cr1.30–1.70
Mo0.15–0.30
Ni1.30–1.70

Mechanical Properties (+QT)

Values depend on ruling section / thickness (d).

Section (mm)Yield Re min (MPa)Tensile Rm (MPa)Elongation A min (%)
d ≤ 1610001200–14009
16 < d ≤ 409001100–130010
40 < d ≤ 1008001000–120011
100 < d ≤ 160700900–110012
160 < d ≤ 250600800–95013

Hardness: +A (annealed): ≤ 248 HB · +QT: typically 270–330 HB (~28–36 HRC)

34CrNiMo6 / 1.6582 properties and use

34CrNiMo6 is the upper class of the quenched-and-tempered steels. Its key difference from 42CrMo4 is nickel content (1.3–1.7%): nickel markedly raises hardenability and low-temperature toughness. This lets 34CrNiMo6 give uniform mechanical properties even in large sections where 42CrMo4 cannot harden to the core — hence its use in large-diameter shafts, turbine shafts and aircraft landing gear. Typical heat treatment: oil quenching from 830–860 °C followed by tempering at 540–660 °C. Delivery conditions are +A (annealed) or +QT. Weldability is difficult: its high carbon equivalent requires 250–350 °C preheat and post-weld stress relief; it is generally used as a forged/machined part rather than welded. Aktif Çelik supplies 34CrNiMo6 as hot rolled bars and forged bars up to 1000 mm, with EN 10204 3.1 certification.

International Equivalents

Values marked ≈ are nearest matches, not exact equivalents. Always confirm against the governing standard.

SystemGrade
EN34CrNiMo6
W.-Nr. (DIN)1.6582
AISI/SAE≈ 4340 / 4337
ASTMA29 (4340)
JISSNCM447
GOST≈ 38ХН3МА (38KhN3MA)
BS 970 (UK)817M40 (EN24)
GB (China)≈ 40CrNiMoA

Applications

  • Heavy-duty shafts and large-diameter shafting
  • Turbine and generator shafts
  • Aircraft landing gear and aerospace parts
  • Large gears and pinions
  • High-strength bolts and studs
  • Heavy-industry forgings

Frequently Asked Questions

What is the difference between 34CrNiMo6 and 42CrMo4?+

The main difference is nickel: 34CrNiMo6 contains 1.3–1.7% nickel, 42CrMo4 has none. Nickel raises hardenability and toughness, so 34CrNiMo6 hardens to the core in large sections (e.g. >100 mm) and gives higher strength. 42CrMo4 is economical and sufficient for medium sections, while 34CrNiMo6 is chosen where heavy load and large diameter are required.

Is 34CrNiMo6 the same as AISI 4340?+

The nearest American equivalent is AISI 4340 (EN24 / 817M40 in the British system). The compositions are very close; 4340 typically has a slightly higher carbon range. In aerospace and defence both are treated as the same 'ultra-high-strength' class; for critical work, follow the ordering standard.

What hardness and strength does 34CrNiMo6 reach?+

In the quenched and tempered (+QT) condition, typical hardness is 270–330 HB (~28–36 HRC). Tensile strength ranges 800–1400 MPa and yield 600–1000 MPa depending on section. Thin sections can reach up to 1400 MPa tensile.

Is 34CrNiMo6 weldable?+

With difficulty. Its high carbon equivalent creates a high cracking risk, requiring 250–350 °C preheat, low-hydrogen consumables and post-weld stress relief. It is generally shaped by forging or machining rather than welded.

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Values on this page are reference data compiled from the applicable EN standard; certified material properties are defined by the mill test certificate (EN 10204 3.1).