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Steel 40CrNiMoA Q&T 38-42 HRC

Hardness band

GB 40CrNiMoA · AISI/SAE 4340

Q&T 38-42 HRC = lower temper

Use for higher-strength ~1300 MPa parts such as aerospace fittings and heavy-duty bolts where some ductility is still needed.

CNC machiningSheet metalStandard cost $$

Values for the Q&T 38-42 HRC condition

Other 40CrNiMoA tempers and conditions

40CrNiMoA is listed in 10 conditions; see the grade overview at 40CrNiMoA.

Compare all 10 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
full anneal ~820–840 °C, slow cool
Softest condition for deep machining, cold forming or as a pre-heat-treat stock; hardness capped at 269 HB per GB/T 3077.47074522217 HB—
Hot rolled
Cheapest mill condition, bought as forging or machining blank when the shop will heat treat afterwards; properties vary with section and cooling rate.6209501430 HRC7 % IACS
Cold drawn
Bright, close-tolerance bar for direct machining of moderately loaded parts without further heat treatment.7208601224 HRC7 % IACS
~860–880 °C, air cool
Uniform, refined structure for forgings before final Q&T; already strong but with limited ductility because of the air-hardened bainite/martensite.8601,2801239 HRC—
High-temper condition
Pick when toughness and machinability matter more than strength, e.g. large forged shafts and pressure-containing parts.8601,0001830 HRC—
Q&TDefault
Quenched and tempered
Standard stocked condition: balanced ~1000–1100 MPa strength with high toughness for shafts, gears and high-strength fasteners.9501,0801634 HRC—
Mid-temper condition
Most common ordered hardness band for gears, connecting rods and driveline shafts; good strength/toughness compromise.1,0001,1001534 HRC—
Q&T 38-42 HRCThis page
Lower temper
Use for higher-strength ~1300 MPa parts such as aerospace fittings and heavy-duty bolts where some ductility is still needed.1,2001,3001240 HRC—
Low temper
High-strength ~1500 MPa condition for torsion bars, landing-gear-type parts and tooling; toughness and machinability drop sharply.1,3501,5001044 HRC—
Quench and stress-relief temper
Maximum strength (~1800 MPa) condition for wear parts and tooling; brittle, notch- and hydrogen-sensitive, so avoid stress concentrations and plate only with post-bake.1,6001,800850 HRC—

What is 40CrNiMoA Q&T 38-42 HRC?

40CrNiMoA Q&T 38-42 HRC is 40CrNiMoA heat treated to Q&T 38-42 HRC — use for higher-strength ~1300 MPa parts such as aerospace fittings and heavy-duty bolts where some ductility is still needed. 40CrNiMoA Q&T 38-42 HRC has a yield strength of 1,200 MPa (174 ksi) and a tensile strength of 1,300 MPa (189 ksi) — stronger than 94% of steel grades. Elongation at break is 12% and the elastic modulus is 207 GPa (30 Msi). 40CrNiMoA Q&T 38-42 HRC 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). Q&T is the default condition FabDigit quotes; Q&T 38-42 HRC is available on request or by drawing note.

Advantages

  • High strength — 1,200 MPa (174 ksi), better than 94% of steel grades
  • Polishes to a fine finish — 65/100, better than 78% of steel grades

Limitations

  • Difficult to machine — 30/100, worse than 89% of steel grades
  • Limited ductility — 12%, worse than 84% of steel grades

40CrNiMoA Q&T 38-42 HRC properties

Typical room-temperature values for 40CrNiMoA Q&T 38-42 HRC; 13 are specific to this condition. Other listed values are 40CrNiMoA reference data and may not represent this condition. Bars are the position among steel grades.

Physical3

40CrNiMoA Q&T 38-42 HRC 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 Temperature1,500°C2,732 °F

Mechanical16

40CrNiMoA Q&T 38-42 HRC has a yield strength of 1,200 MPa (174 ksi) and a tensile strength of 1,300 MPa (189 ksi) — stronger than 94% of steel grades. Elongation at break is 12% and the elastic modulus is 207 GPa (30 Msi).

Elastic (Young's) Modulus207 GPa30 Msi
Shear Modulus80 GPa11.6 Msi
Bulk Modulus160 GPa23.2 Msi
Poisson's Ratio0.29
Tensile Strength (Ultimate)1,300 MPa189 ksi
Yield Strength (0.2% offset)1,200 MPa174 ksi
Elongation at Break12%
Reduction in Area45%
Compressive Strength980 MPa142 ksi
Shear Strength660 MPa95.7 ksi
Fatigue Strength (Endurance Limit)620 MPa89.9 ksi
Fracture Toughness (K_IC)75 MPa·√m68.3 ksi·√in
Charpy V-Notch Impact (RT)40 J29.5 ft·lbf
Hardness, Brinell375 HB
Hardness, Rockwell C40 HRC
Hardness, Vickers400 HV

Thermal6

40CrNiMoA Q&T 38-42 HRC is rated for continuous service to 350°C (662 °F). It conducts heat at 44 W/m·K (25.4 BTU/hr·ft·°F), better than 57% of steel grades. Thermal expansion is 12.3 µm/m·K (6.83 µin/in·°F).

Thermal Conductivity44 W/m·K25.4 BTU/hr·ft·°F
Specific Heat Capacity475 J/kg·K0.11 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)12.3 µm/m·K6.8 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

40CrNiMoA Q&T 38-42 HRC conducts electricity at 7 % IACS, worse than 74% of steel grades.

Electrical Conductivity7 % IACS
Electrical Resistivity2.48×10⁻⁷ Ω·m9.76 µΩ·in
Magnetic Responseferromagnetic

Chemical & Environmental3

Corrosion resistance is poor (15/100), better than 75% of steel grades.

Galvanic Potential (seawater, vs SCE)-0.6 V
Corrosion ResistancePoor15/100
Chemical Resistance SummaryRusts freely in humid air and water; no resistance to acids or chlorides. Requires oil, phosphate, Zn/Cd plating, nitriding or paint. High-hardness conditions are sensitive to hydrogen embrittlement from acid pickling and electroplating (bake after plating).

Sustainability4

Producing a kilogram of 40CrNiMoA Q&T 38-42 HRC takes about 32 MJ of energy and emits 2.3 kg of CO₂ — more than 70% of steel grades. Typical recycled content is 30%.

Embodied Energy (primary production)32 MJ/kg13,758 BTU/lb
Embodied Carbon (primary production)2.3 kg CO₂/kg
Embodied Water55 L/kg6.6 gal/lb
Typical Recycled Content30%

Manufacturability8

40CrNiMoA Q&T 38-42 HRC's machinability is poor (30/100, worse than 89% of steel grades); weldability poor (30/100); formability poor (25/100).

MachinabilityPoor30/100
Machinability Rating (AISI 1212 = 100 %)33%
WeldabilityPoor30/100
Formability (cold)Poor25/100
CastabilityFair40/100
Brazeability / SolderabilityFair45/100
PolishabilityGood65/100
Anodizing Responsen/a — ferrous alloy; use black oxide, phosphating, Zn/Cd/Cr plating or nitriding instead

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

Working with 40CrNiMoA Q&T 38-42 HRC

Is 40CrNiMoA easy to machine?

Machine in the annealed or ≤32 HRC condition with rigid setups, sharp carbide and generous coolant; above 40 HRC switch to CBN/ceramic turning or grinding, and rough before final temper where possible.

Can 40CrNiMoA be welded?

High carbon equivalent means preheat 250–350 °C, low-hydrogen filler (e.g. ER100S/ER110S or matching), interpass control and immediate PWHT/re-temper; avoid welding parts already at high hardness.

Can 40CrNiMoA be formed, bent or molded?

Hot forge 1100–1200 °C, finish above 900 °C and normalize afterwards; cold forming is limited to the annealed condition and mild bends only.

What surface finishes work on 40CrNiMoA?

Not anodizable — protect with black oxide, phosphate + oil, Zn or Cd plating, hard chrome, or gas nitriding (surface 550–650 HV); bake 190–220 °C after electroplating high-hardness parts to relieve hydrogen.

40CrNiMoA 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
C0.37 – 0.440.4
Si0.17 – 0.370.27
Mn0.5 – 0.80.65
Cr0.6 – 0.90.75
Ni1.25 – 1.651.45
Mo0.15 – 0.250.2
PA grade (high-quality) limit≤ 0.03
SA grade (high-quality) limit≤ 0.03
Curesidual≤ 0.3
Febalance

40CrNiMoA Q&T 38-42 HRC — frequently asked

What is 40CrNiMoA Q&T 38-42 HRC used for?

40CrNiMoA Q&T 38-42 HRC is typically used for aircraft landing gear components, drive shafts, industrial axles, gearbox shafts and pinions, heavy-duty crankshafts and high-strength bolts and studs. In short: premium Ni-Cr-Mo bar.

What is the yield strength of 40CrNiMoA Q&T 38-42 HRC?

40CrNiMoA Q&T 38-42 HRC has a typical yield strength of 1,200 MPa (174 ksi) and a tensile strength of 1,300 MPa (189 ksi) — stronger than 94% of steel grades. Strength varies by condition: see the 10 listed tempers.

Is 40CrNiMoA Q&T 38-42 HRC easy to machine?

Not especially — machinability is rated poor (30/100, worse than 89% of steel grades). Machine in the annealed or ≤32 HRC condition with rigid setups, sharp carbide and generous coolant; above 40 HRC switch to CBN/ceramic turning or grinding, and rough before final temper where possible.

Can 40CrNiMoA Q&T 38-42 HRC be welded?

Not readily — weldability is rated poor (30/100). High carbon equivalent means preheat 250–350 °C, low-hydrogen filler (e.g. ER100S/ER110S or matching), interpass control and immediate PWHT/re-temper; avoid welding parts already at high hardness.

What surface finishes work on 40CrNiMoA Q&T 38-42 HRC?

Not anodizable — protect with black oxide, phosphate + oil, Zn or Cd plating, hard chrome, or gas nitriding (surface 550–650 HV); bake 190–220 °C after electroplating high-hardness parts to relieve hydrogen.

Can 40CrNiMoA Q&T 38-42 HRC be formed, bent or molded?

Hot forge 1100–1200 °C, finish above 900 °C and normalize afterwards; cold forming is limited to the annealed condition and mild bends only.

What is the maximum service temperature of 40CrNiMoA Q&T 38-42 HRC?

40CrNiMoA Q&T 38-42 HRC 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 40CrNiMoA Q&T and 40CrNiMoA-HR?

Q&T is the default condition — standard stocked condition: balanced ~1000–1100 MPa strength with high toughness for shafts, gears and high-strength fasteners. HR: cheapest mill condition, bought as forging or machining blank when the shop will heat treat afterwards; properties vary with section and cooling rate. Yield strength is 950 MPa in Q&T versus 620 MPa in HR.

Can FabDigit make parts in 40CrNiMoA Q&T 38-42 HRC?

Yes — 40CrNiMoA Q&T 38-42 HRC is available for CNC machining and sheet metal; every part is priced by an engineer rather than instantly. Upload a STEP file to get a price and a DFM check.

Sources

  1. GB/T 3077 Alloy structural steels (2015)
  2. ASTM A29/A29M and SAE J404 (4340) — ASTM / SAE (2020)
  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-2023 typical properties for 4340 steel — Battelle/FAA (2023)
  6. Machinery's Handbook, 31st ed. (machinability ratings) — Industrial Press (2020)
  7. (40CrNiMoA) — Mysteel / 1688 (2025)

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.