FabDigit

Steel 30NCD16

EN 30NCD16

30NCD16 is a French AFNOR high-nickel chromium-molybdenum ultra-high-strength steel, cross-referenced to 4340, available annealed, normalized, in quenched-and-tempered conditions from QT1080 to QT1770 and quenched-tempered-plus-nitrided.

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Reference datasheet — 30NCD16 is not in the instant-quote catalog. Upload your part and an engineer will quote it in this grade or suggest the closest stocked equivalent.

Values for the QT1230 condition

30NCD16 tempers and conditions

30NCD16 is supplied in 8 conditions, soft to hard. QT1230 is the default FabDigit quotes; the values on this page are for it.

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—
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?

30NCD16 is a French AFNOR high-nickel chromium-molybdenum ultra-high-strength steel, cross-referenced to 4340, available annealed, normalized, in quenched-and-tempered conditions from QT1080 to QT1770 and quenched-tempered-plus-nitrided. Engineers select it for aerospace landing gear and highly stressed structural parts because of its deep hardenability and toughness at high strength; usual forms are bar, billet and closed-die forgings. Default values are 1130 MPa yield, 1320 MPa tensile, 12 % elongation, 380 HB (41 HRC), service to 350 °C and a machinability score of 38. Weldability is poor and the steel has no corrosion resistance, so plating plus a de-embrittlement bake is mandatory. 30NCD16 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). 30NCD16 has a yield strength of 1,130 MPa (164 ksi) and a tensile strength of 1,320 MPa (191 ksi) — stronger than 93% of steel grades. Elongation at break is 12% and the elastic modulus is 205 GPa (29.7 Msi).

What is 30NCD16 used for?

  • aircraft landing gear
  • high-strength fasteners
  • structural forgings

Advantages

  • High strength — 1,130 MPa (164 ksi), better than 93% 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
  • Poor heat conductor — 33 W/m·K (19.1 BTU/hr·ft·°F), worse than 80% of steel grades
  • Low electrical conductivity — 5.7 % IACS, worse than 80% of steel grades
  • Difficult to machine — 38/100, worse than 80% of steel grades

30NCD16 properties

Typical room-temperature values for 30NCD16-QT1230; bars are the position among steel grades.

Physical3

30NCD16 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 has a yield strength of 1,130 MPa (164 ksi) and a tensile strength of 1,320 MPa (191 ksi) — stronger than 93% 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)1,320 MPa191 ksi
Yield Strength (0.2% offset)1,130 MPa164 ksi
Elongation at Break12%
Reduction in Area52%
Compressive Strength1,180 MPa171 ksi
Shear Strength800 MPa116 ksi
Fatigue Strength (Endurance Limit)620 MPa89.9 ksi
Fracture Toughness (K_IC)95 MPa·√m86.5 ksi·√in
Charpy V-Notch Impact (RT)45 J33.2 ft·lbf
Hardness, Brinell380 HB
Hardness, Rockwell C41 HRC
Hardness, Vickers400 HV

Thermal6

30NCD16 is rated for continuous service to 350°C (662 °F). It conducts heat at 33 W/m·K (19.1 BTU/hr·ft·°F), worse than 80% of steel grades. Thermal expansion is 11.7 µm/m·K (6.5 µin/in·°F).

Thermal Conductivity33 W/m·K19.1 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 conducts electricity at 5.7 % IACS, worse than 80% of steel grades.

Electrical Conductivity5.7 % IACS
Electrical Resistivity3×10⁻⁷ Ω·m11.8 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 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's machinability is fair (38/100, worse than 80% of steel grades); weldability poor (25/100); formability poor (20/100).

MachinabilityFair38/100
Machinability Rating (AISI 1212 = 100 %)35%
WeldabilityPoor25/100
Formability (cold)Poor20/100
CastabilityFair35/100
Brazeability / SolderabilityFair40/100
PolishabilityVery good70/100

Common Calculations5

Specific Strength (UTS / density)calculated168 kN·m/kg
Specific Stiffness (E / density)calculated26.1 MN·m/kg
Modulus of Resiliencecalculated3,114 kJ/m³
Thermal Diffusivitycalculated9.1 mm²/s
Thermal Shock Resistance Indexcalculated18

Values are nominal handbook figures for design screening. Certified mill or lot data ships with every FabDigit order on request.

Strength versus weight in the steel family

Yield strength against density for every steel grade FabDigit runs. 30NCD16 is highlighted; hover a dot for its name, or open the interactive family chart.

2005001,0002,0007.588.5Density (g/cm³)Yield strength (MPa) — log scale30NCD16

Working with 30NCD16

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.

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

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.

Surface treatments FabDigit runs on steel parts — pick them in the quote configurator or call them out on the drawing. Each links to its datasheet in the surface-finish library (thickness, specs, call-out, material verdicts).

Equivalent designations

Standards and trade names that resolve to Steel 30NCD16 in FabDigit's catalog. Equivalence is nominal — check the exact specification when certification matters.

Similar grades
4340

How much does 30NCD16 cost?

30NCD16 is a premium-cost steel ($$$), cheaper than about 51% of the materials FabDigit quotes. Part price depends far more on geometry, tolerance and quantity than on the raw stock — upload a CAD file for a live quote.

30NCD16 — frequently asked

What is 30NCD16 used for?

30NCD16 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?

30NCD16 has a typical yield strength of 1,130 MPa (164 ksi) and a tensile strength of 1,320 MPa (191 ksi) — stronger than 93% of steel grades. Strength varies by condition: see the 8 listed tempers.

Is 30NCD16 easy to machine?

Not especially — machinability is rated fair (38/100, worse than 80% 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 be welded?

Not readily — weldability is rated poor (25/100). 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?

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 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?

30NCD16 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.

How much does 30NCD16 cost?

30NCD16 is a premium-cost steel ($$$), cheaper than about 51% of the materials FabDigit quotes. Part price depends far more on geometry, tolerance and quantity than on the raw stock — upload a CAD file for a live quote.

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; hardness values on non-Brinell scales are converted approximately for charting only. Manufacturability limits are FabDigit quote-engine defaults and may be relaxed by engineering review. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.