
The AFNOR 35NCD14 is a high-performance, high-hardenability nickel-chromium-molybdenum alloy steel specified under the French AFNOR standard. It is renowned for its exceptional tensile strength, toughness, and fatigue resistance, making it a staple material in aerospace, defense, and heavy-duty mechanical engineering applications.
Here is a comprehensive breakdown of its technical specifications, equivalents, chemical composition, and typical applications for round bars and rods.
The precise balance of nickel ($Ni$), chromium ($Cr$), and molybdenum ($Mb$) gives this grade its deep-hardening characteristics and excellent impact toughness.
| Element | Minimum (%) | Maximum (%) |
| Carbon (C) | 0.32 | 0.39 |
| Nickel (Ni) | 3.60 | 4.10 |
| Chromium (Cr) | 1.20 | 1.60 |
| Molybdenum (Mo) | 0.40 | 0.60 |
| Silicon (Si) | 0.15 | 0.40 |
| Manganese (Mn) | 0.30 | 0.60 |
| Phosphorus (P) | â | 0.025 |
| Sulfur (S) | â | 0.020 |
While 35NCD14 is uniquely heavily alloyed (especially with its high nickel content near 4%), it closely aligns with or replaces several global high-tensile standards:
Germany (DIN / WNr): 36CrNiMo16 / 1.6773
United Kingdom (BS): 835M30
USA (AISI/SAE): Closest to 4340 / E4340 (Note: 35NCD14 has significantly higher Nickel content for superior toughness at high strength levels)
Europe (EN): 36NiCrMo16
Italy (UNI): 38NiCrMo16
When quenched and tempered, 35NCD14 round bars achieve a remarkable combination of high tensile strength and high yield stress without becoming brittle.
Tensile Strength ($R_m$): $1100 - 1300\text{ MPa}$ (can exceed $1500\text{ MPa}$ depending on heat treatment)
Yield Strength ($R_{e}$): $\ge 900\text{ MPa}$
Elongation ($A_5$): $\ge 10\%$
Impact Energy ($KV$): $\ge 35\text{ J}$ (at room temperature)
Deep Hardenability: Thanks to the high nickel and chromium content, heavy-section round bars maintain uniform mechanical properties from the surface right to the core.
Fatigue & Impact Resistance: Excellent performance under cyclic loading and high-stress shock environments.
Machinability: Best machined in the annealed or normalized condition; requires rigid setups and carbide tooling if machined in the fully hardened state.
Because of its premium structural integrity, 35NCD14 round bars and rods are heavily utilized in critical components:
Aerospace & Defense: Landing gear components, high-stress structural shafts, and engine mountings.
Automotive & Motorsport: High-torque drive shafts, crankshafts, connecting rods, and stub axles.
Heavy Machinery: Heavy-duty gears, pinions, turbine rotors, and high-tensile clamping bolts/fasteners.
Finishes: Hot-rolled, forged, cold-drawn, centerless ground, or turned.
Heat Treatment States: Supplied as annealed (for ease of machining) or pre-hardened (Quenched + Tempered to specific strength bands).
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