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Steel 30NCD16-N (Normalized)

Heat-treated state

EN 30NCD16

Grain-refining intermediate condition for forgings prior to final quench and temper.

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Values for the N condition

Other 30NCD16 tempers and conditions

30NCD16 is listed in 8 conditions; see the grade overview at 30NCD16.

Compare all 8 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Supply condition for rough machining, deep cold forming and subsequent hardening.56082020235 HB—
NThis page
Normalized
Grain-refining intermediate condition for forgings prior to final quench and temper.9001,2501239 HRC5.9 % IACS
Q&T 1080–1230 MPa
Toughest structural class — thick landing-gear forgings and shafts where impact and K_IC dominate.1,0001,1501436 HRC—
Q&T + gas nitrided
Pick for wear surfaces (pistons, rods, gears) where a 0.3–0.6 mm hard case plus tough core is required.1,1001,3001141 HRC5.7 % IACS
QT1230Default
Q&T 1230–1420 MPa
Most widely stocked balance of strength and toughness for landing-gear and highly stressed structure.1,1301,3201241 HRC—
Q&T 1420–1620 MPa
Higher strength for weight-critical pins, actuator rods and links where toughness margin is still acceptable.1,3301,5201046 HRC—
Q&T 1620–1770 MPa
Used where static strength governs; requires strict hydrogen and SCC control.1,4701,700949 HRC—
Q&T 1770–1960 MPa
Peak strength class for small highly loaded parts; lowest toughness and highest embrittlement risk.1,5701,860852 HRC—

What is 30NCD16-N?

30NCD16-N is 30NCD16 heat treated to N — grain-refining intermediate condition for forgings prior to final quench and temper. 30NCD16-N has a yield strength of 900 MPa (131 ksi) and a tensile strength of 1,250 MPa (181 ksi) — stronger than 90% of steel grades. Elongation at break is 12% and the elastic modulus is 205 GPa (29.7 Msi). 30NCD16-N has a density of 7.85 g/cm³ (0.284 lb/in³), heavier than 56% of steel grades. It melts at 1,420°C (2,588 °F). QT1230 is the default condition FabDigit quotes; N is available on request or by drawing note.

Advantages

  • High strength — 900 MPa (131 ksi), better than 90% of steel grades
  • Polishes to a fine finish — 70/100, better than 87% of steel grades

Limitations

  • High embodied carbon — 2.6 kg CO₂/kg, worse than 87% of steel grades
  • Limited ductility — 12%, worse than 84% of steel grades
  • Low electrical conductivity — 5.9 % IACS, worse than 79% of steel grades
  • Low fracture toughness — 60 MPa·√m (54.6 ksi·√in), worse than 78% of steel grades
  • Limited formability — 22/100, worse than 76% of steel grades

30NCD16-N properties

Typical room-temperature values for 30NCD16-N; 20 are specific to this condition. Other listed values are 30NCD16 reference data and may not represent this condition. Bars are the position among steel grades.

Physical3

30NCD16-N has a density of 7.85 g/cm³ (0.284 lb/in³), heavier than 56% of steel grades. It melts at 1,420°C (2,588 °F).

Density7.85 g/cm³0.28 lb/in³
Melting Point (Solidus)1,420°C2,588 °F
Liquidus Temperature1,480°C2,696 °F

Mechanical16

30NCD16-N has a yield strength of 900 MPa (131 ksi) and a tensile strength of 1,250 MPa (181 ksi) — stronger than 90% of steel grades. Elongation at break is 12% and the elastic modulus is 205 GPa (29.7 Msi).

Elastic (Young's) Modulus205 GPa29.7 Msi
Shear Modulus80 GPa11.6 Msi
Bulk Modulus160 GPa23.2 Msi
Poisson's Ratio0.29
Tensile Strength (Ultimate)1,250 MPa181 ksi
Yield Strength (0.2% offset)900 MPa131 ksi
Elongation at Break12%
Reduction in Area38%
Compressive Strength940 MPa136 ksi
Shear Strength750 MPa109 ksi
Fatigue Strength (Endurance Limit)560 MPa81.2 ksi
Fracture Toughness (K_IC)60 MPa·√m54.6 ksi·√in
Charpy V-Notch Impact (RT)25 J18.4 ft·lbf
Hardness, Brinell360 HB
Hardness, Rockwell C39 HRC
Hardness, Vickers378 HV

Thermal6

30NCD16-N is rated for continuous service to 350°C (662 °F). It conducts heat at 35 W/m·K (20.2 BTU/hr·ft·°F), worse than 75% of steel grades. Thermal expansion is 11.7 µm/m·K (6.5 µin/in·°F).

Thermal Conductivity35 W/m·K20.2 BTU/hr·ft·°F
Specific Heat Capacity460 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)11.7 µm/m·K6.5 µin/in·°F
Latent Heat of Fusion250 J/g107 BTU/lb
Max Service Temperature (continuous)350°C662 °F
Min Service Temperature-60°C-76 °F

Electrical3

30NCD16-N conducts electricity at 5.9 % IACS, worse than 79% of steel grades.

Electrical Conductivity5.9 % IACS
Electrical Resistivity2.9×10⁻⁷ Ω·m11.4 µΩ·in
Magnetic Responseferromagnetic

Chemical & Environmental3

Corrosion resistance is not recommended (14/100), better than 70% of steel grades.

Galvanic Potential (seawater, vs SCE)-0.6 V
Corrosion ResistanceNot recommended14/100
Chemical Resistance SummaryNo inherent corrosion resistance: rusts in humid air and seawater; high-strength tempers are susceptible to hydrogen embrittlement and stress-corrosion cracking, so cadmium/Al-coating or LHE plating with bake-out is mandatory.

Sustainability4

Producing a kilogram of 30NCD16-N takes about 36 MJ of energy and emits 2.6 kg of CO₂ — more than 89% of steel grades. Typical recycled content is 20%.

Embodied Energy (primary production)36 MJ/kg15,477 BTU/lb
Embodied Carbon (primary production)2.6 kg CO₂/kg
Embodied Water60 L/kg7.2 gal/lb
Typical Recycled Content20%

Manufacturability7

30NCD16-N's machinability is fair (42/100, worse than 73% of steel grades); weldability poor (28/100); formability poor (22/100).

MachinabilityFair42/100
Machinability Rating (AISI 1212 = 100 %)40%
WeldabilityPoor28/100
Formability (cold)Poor22/100
CastabilityFair35/100
Brazeability / SolderabilityFair40/100
PolishabilityVery good70/100

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with 30NCD16-N

Is 30NCD16 easy to machine?

Rough machine annealed (~235 HB), finish after Q&T with rigid setups, carbide/coated tools, 60–120 m/min at 40 HRC; grind or use ceramic inserts above 50 HRC.

Can 30NCD16 be welded?

Poor weldability: preheat 250–350 °C, low-hydrogen or TIG filler, immediate post-weld temper below the part's tempering temperature; avoid welding on high-strength tempers.

Can 30NCD16 be formed, bent or molded?

Hot forge 1100–1180 °C with slow cooling and normalize; cold forming only in the annealed condition, bend radii ≥3t.

What surface finishes work on 30NCD16?

Shot peen highly stressed surfaces, then cadmium/LHE-zinc-nickel plate, hard chrome or HVOF WC on bearing diameters; bake 190–210 °C for ≥23 h after plating to relieve hydrogen.

30NCD16 chemical composition (wt %)

Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.

ElementSpec limit (wt %)Nominal
C0.26 – 0.340.3
Si0.1 – 0.40.25
Mn0.3 – 0.60.45
Nigives the deep hardenability and low-temperature toughness3.6 – 4.23.9
Cr1.6 – 21.8
Mosuppresses temper embrittlement0.25 – 0.450.35
Paerospace melt, often ≤0.010≤ 0.02—
SVAR/VD grades ≤0.005≤ 0.01—
Cu≤ 0.2—
Febalance—

30NCD16-N — frequently asked

What is 30NCD16-N used for?

30NCD16-N is typically used for aircraft landing gear, high-strength fasteners and structural forgings. In short: aerospace ultra-high-strength steel; 4340-class deep hardenability; poor weldability, needs plating.

What is the yield strength of 30NCD16-N?

30NCD16-N has a typical yield strength of 900 MPa (131 ksi) and a tensile strength of 1,250 MPa (181 ksi) — stronger than 90% of steel grades. Strength varies by condition: see the 8 listed tempers.

Is 30NCD16-N easy to machine?

Not especially — machinability is rated fair (42/100, worse than 73% of steel grades). Rough machine annealed (~235 HB), finish after Q&T with rigid setups, carbide/coated tools, 60–120 m/min at 40 HRC; grind or use ceramic inserts above 50 HRC.

Can 30NCD16-N be welded?

Not readily — weldability is rated poor (28/100). Poor weldability: preheat 250–350 °C, low-hydrogen or TIG filler, immediate post-weld temper below the part's tempering temperature; avoid welding on high-strength tempers.

What surface finishes work on 30NCD16-N?

Shot peen highly stressed surfaces, then cadmium/LHE-zinc-nickel plate, hard chrome or HVOF WC on bearing diameters; bake 190–210 °C for ≥23 h after plating to relieve hydrogen.

Can 30NCD16-N be formed, bent or molded?

Hot forge 1100–1180 °C with slow cooling and normalize; cold forming only in the annealed condition, bend radii ≥3t.

What is the maximum service temperature of 30NCD16-N?

30NCD16-N is rated for continuous use to about 350°C (662 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between 30NCD16-QT1230 and 30NCD16-ANN?

QT1230 is the default condition — most widely stocked balance of strength and toughness for landing-gear and highly stressed structure. ANN: supply condition for rough machining, deep cold forming and subsequent hardening. Yield strength is 1,130 MPa in QT1230 versus 560 MPa in ANN.

Sources

  1. NF A35-565 / AIR 9160 — 30NCD16 aerospace alloy steel bars and forgings — AFNOR / BNAE (1990)
  2. 30NCD16 high-strength Ni-Cr-Mo steel datasheet — Aubert & Duval (2021)
  3. ASM Handbook Vol.1 — Properties and Selection: Irons, Steels and High-Performance Alloys — ASM International (1990)
  4. ASM Handbook Vol.19 — Fatigue and Fracture — ASM International (1996)
  5. MMPDS-17 (4340 / low-alloy UHS steel chapters) — Battelle/FAA (2022)

Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.