FabDigit

Steel 4340M

AISI/SAE 4340M · UNS K44220 · AMS 6419 · also 300M

4340M (300M, UNS K44220) is a silicon- and vanadium-modified 4340 low-alloy steel, usually vacuum-arc remelted, that reaches higher strength, toughness and fatigue resistance than standard 4340.

CNC machiningSheet metalStandard cost $$

Values for the HR condition

4340M tempers and conditions

4340M is supplied in 9 conditions, soft to hard. HR is the default FabDigit quotes; the values on this page are for it.

Compare all 9 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed (AMS 6417 / spheroidize annealed bar)
Softest supply condition — pick for rough machining, deep drilling and forming before final quench and temper.6909301526 HRC36 W/m·K
Cold rolled
Thin strip/sheet condition for parts that will be formed then hardened; limited availability and limited cold-work capability.8301,000930 HRC7 % IACS
Cold drawn
Small-diameter annealed bar/wire cold drawn to size for tight tolerance and better surface before heat treatment; rarely stocked in this grade.8601,0301031 HRC7 % IACS
Normalized & Tempered
Normalize ~925 °C then temper for uniform grain and moderate hardness — a machining/stock condition and a grain-refining step before final hardening.9651,2401240 HRC—
HRDefault
Hot rolled
Mill product as rolled or forged — air-hardened martensite, too hard and brittle to machine; always annealed or normalized before use.1,1501,550647 HRC7 % IACS
Q&T 1790 MPa
Slightly higher temper for parts where fracture toughness and ductility matter more than peak strength.1,5201,7901151 HRC7 % IACS
Quenched and tempered
The standard 300M service condition (AMS 6419): highest strength/toughness balance for landing gear, actuator rods and shafts.1,6201,9301054 HRC—
VAR / CEVM premium-melt bar
Consumable-electrode vacuum remelted stock — choose for fatigue- and fracture-critical aerospace parts needing best transverse ductility and low inclusion count.1,6401,9301254 HRC7 % IACS
Q&T 2070 MPa
Maximum-strength condition for weight-critical rocket motor cases and springs; accept lower toughness and high notch sensitivity.1,7202,070856 HRC—

What is 4340M?

4340M (300M, UNS K44220) is a silicon- and vanadium-modified 4340 low-alloy steel, usually vacuum-arc remelted, that reaches higher strength, toughness and fatigue resistance than standard 4340. It is used for ultra-high-strength aerospace structure and landing gear, and is supplied as HR, CR, CD, annealed, normalized, VAR and Q&T bar including the 1790 MPa and 2070 MPa strength levels. Default Q&T values are 1150 MPa yield, 1550 MPa tensile, 6 % elongation and 444 HB (47 HRC). Machinability rates 15, it is not weldable when hardened, has no corrosion resistance and is sensitive to hydrogen embrittlement; 4340 is the lower-cost alternative. 4340M has a density of 7.83 g/cm³ (0.283 lb/in³), lighter than 80% of steel grades. It melts at 1,420°C (2,588 °F). 4340M has a yield strength of 1,150 MPa (167 ksi) and a tensile strength of 1,550 MPa (225 ksi) — stronger than 94% of steel grades. Elongation at break is 6% and the elastic modulus is 205 GPa (29.7 Msi).

What is 4340M used for?

  • Aircraft landing gear cylinders and axles
  • Arresting hooks
  • High-strength airframe fittings
  • Rocket motor cases
  • Torsion bars
  • High-strength drive shafts
  • Aerospace fasteners

Advantages

  • High strength — 1,150 MPa (167 ksi), better than 94% of steel grades
  • Polishes to a fine finish — 75/100, better than 94% of steel grades

Limitations

  • Limited formability — 5/100, worse than 99% of steel grades
  • Difficult to machine — 15/100, worse than 98% of steel grades
  • Limited ductility — 6%, worse than 97% of steel grades
  • Difficult to weld — 12/100, worse than 96% of steel grades
  • Low fracture toughness — 40 MPa·√m (36.4 ksi·√in), worse than 92% of steel grades

4340M properties

Typical room-temperature values for 4340M-HR; bars are the position among steel grades.

Physical3

4340M has a density of 7.83 g/cm³ (0.283 lb/in³), lighter than 80% of steel grades. It melts at 1,420°C (2,588 °F).

Density7.83 g/cm³0.28 lb/in³
Melting Point (Solidus)1,420°C2,588 °F
Liquidus Temperature1,480°C2,696 °F

Mechanical16

4340M has a yield strength of 1,150 MPa (167 ksi) and a tensile strength of 1,550 MPa (225 ksi) — stronger than 94% of steel grades. Elongation at break is 6% and the elastic modulus is 205 GPa (29.7 Msi).

Elastic (Young's) Modulus205 GPa29.7 Msi
Shear Modulus78 GPa11.3 Msi
Bulk Modulus160 GPa23.2 Msi
Poisson's Ratio0.29
Tensile Strength (Ultimate)1,550 MPa225 ksi
Yield Strength (0.2% offset)1,150 MPa167 ksi
Elongation at Break6%
Reduction in Area18%
Compressive Strength1,200 MPa174 ksi
Shear Strength930 MPa135 ksi
Fatigue Strength (Endurance Limit)640 MPa92.8 ksi
Fracture Toughness (K_IC)40 MPa·√m36.4 ksi·√in
Charpy V-Notch Impact (RT)10 J7.4 ft·lbf
Hardness, Brinell444 HB
Hardness, Rockwell C47 HRC
Hardness, Vickers470 HV

Thermal6

4340M is rated for continuous service to 290°C (554 °F). It conducts heat at 34 W/m·K (19.6 BTU/hr·ft·°F), worse than 77% of steel grades. Thermal expansion is 11.7 µm/m·K (6.5 µin/in·°F).

Thermal Conductivity34 W/m·K19.6 BTU/hr·ft·°F
Specific Heat Capacity475 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)290°C554 °F
Min Service Temperature-73°C-99 °F

Electrical3

4340M conducts electricity at 7 % IACS, worse than 74% of steel grades.

Electrical Conductivity7 % IACS
Electrical Resistivity2.4×10⁻⁷ Ω·m9.45 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 SummaryRusts readily in humid air and seawater; highly susceptible to hydrogen embrittlement and stress-corrosion cracking at 1930 MPa — requires low-embrittlement plating (Cd, Al-IVD) with post-plate bake and strict acid-pickling control.

Sustainability4

Producing a kilogram of 4340M takes about 36 MJ of energy and emits 2.6 kg of CO₂ — more than 89% of steel grades. Typical recycled content is 25%.

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 Content25%

Manufacturability8

4340M's machinability is poor (15/100, worse than 98% of steel grades); weldability not recommended (12/100); formability not recommended (5/100).

MachinabilityPoor15/100
Machinability Rating (AISI 1212 = 100 %)15%
WeldabilityNot recommended12/100
Formability (cold)Not recommended5/100
CastabilityPoor25/100
Brazeability / SolderabilityPoor20/100
PolishabilityVery good75/100
Anodizing Responsen/a — ferrous alloy; use Cd or Al-IVD plating, phosphate or WC-Co HVOF instead

Common Calculations5

Specific Strength (UTS / density)calculated198 kN·m/kg
Specific Stiffness (E / density)calculated26.2 MN·m/kg
Modulus of Resiliencecalculated3,226 kJ/m³
Thermal Diffusivitycalculated9.1 mm²/s
Thermal Shock Resistance Indexcalculated22

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. 4340M 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 scale4340M

Working with 4340M

Is 4340M easy to machine?

Rough machine in the annealed condition (≈40% of B1112) with carbide and rigid setups; at 52–56 HRC only hard turning with CBN, creep-feed or plunge grinding is practical — grind gently to avoid re-tempering burn and grinding cracks.

Can 4340M be welded?

Not weldable in the hardened state; if welding is unavoidable use electron-beam or GTAW with matching filler, 260–320 °C preheat/interpass, and immediately re-austenitize, quench and temper the whole part.

Can 4340M be formed, bent or molded?

Hot forge/upset at 1050–1200 °C with finish above 900 °C, then normalize and anneal; no meaningful cold forming above the annealed condition — bend and straighten only warm and re-stress-relieve.

Manufacturability

The process limits FabDigit applies to 4340M. Every 4340M part is priced by an engineer; design inside these and the quote comes back without a redesign loop.

CNC machining

MachinabilityFair15 / 100
ISO material groupP.2
Cutting speed (rough / finish)180 / 210 m/min
Minimum wall0.8 mm
Minimum internal radius1 mm
Drill depth limit5× diameter
Best surface (machined / polished)Ra 1.6 / —
Hardenable after machiningNo

Sheet metal

FormabilityFair5 / 100
WeldabilityFair12 / 100

4340M 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
C0.4 – 0.460.43
Sikey modification vs 4340 — raises temper resistance1.45 – 1.81.6
Mn0.6 – 0.90.75
Cr0.7 – 0.950.82
Ni1.65 – 21.83
Mo0.3 – 0.450.38
Vgrain refinement0.05 – 0.10.07
P≤ 0.010.01
S≤ 0.010
Cu≤ 0.350.1
Febalance

What surface finishes work on 4340M?

Shot peen highly stressed fillets, then low-hydrogen-embrittlement cadmium or IVD aluminium plating (or HVOF WC-Co on journals) with a 190 °C/23 h bake within 4 h of plating; chrome plating requires strict bake and peening control.

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 4340M in FabDigit's catalog. Equivalence is nominal — check the exact specification when certification matters.

UNS
K44220
AMS
6419
Trade names
300M
Other
6417/6419

How much does 4340M cost?

4340M is a standard-cost steel ($$), cheaper than about 62% 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.

4340M — frequently asked

What is 4340M used for?

4340M is typically used for aircraft landing gear cylinders and axles, arresting hooks, high-strength airframe fittings, rocket motor cases, torsion bars and high-strength drive shafts. In short: high-strength aerospace bar.

What is the yield strength of 4340M?

4340M has a typical yield strength of 1,150 MPa (167 ksi) and a tensile strength of 1,550 MPa (225 ksi) — stronger than 94% of steel grades. Strength varies by condition: see the 9 listed tempers.

Is 4340M easy to machine?

Not especially — machinability is rated poor (15/100, worse than 98% of steel grades). Rough machine in the annealed condition (≈40% of B1112) with carbide and rigid setups; at 52–56 HRC only hard turning with CBN, creep-feed or plunge grinding is practical — grind gently to avoid re-tempering burn and grinding cracks.

Can 4340M be welded?

Not readily — weldability is rated not recommended (12/100). Not weldable in the hardened state; if welding is unavoidable use electron-beam or GTAW with matching filler, 260–320 °C preheat/interpass, and immediately re-austenitize, quench and temper the whole part.

What surface finishes work on 4340M?

Shot peen highly stressed fillets, then low-hydrogen-embrittlement cadmium or IVD aluminium plating (or HVOF WC-Co on journals) with a 190 °C/23 h bake within 4 h of plating; chrome plating requires strict bake and peening control.

Can 4340M be formed, bent or molded?

Hot forge/upset at 1050–1200 °C with finish above 900 °C, then normalize and anneal; no meaningful cold forming above the annealed condition — bend and straighten only warm and re-stress-relieve.

What is the maximum service temperature of 4340M?

4340M is rated for continuous use to about 290°C (554 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between 4340M-HR and 4340M-VAR?

HR is the default condition — mill product as rolled or forged — air-hardened martensite, too hard and brittle to machine; always annealed or normalized before use. VAR: consumable-electrode vacuum remelted stock — choose for fatigue- and fracture-critical aerospace parts needing best transverse ductility and low inclusion count. Yield strength is 1,150 MPa in HR versus 1,640 MPa in VAR.

How much does 4340M cost?

4340M is a standard-cost steel ($$), cheaper than about 62% 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.

Can FabDigit make parts in 4340M?

Yes — 4340M 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. AMS 6419 — Steel Bars, Forgings, Tubing 1.6Si-0.82Cr-1.8Ni-0.40Mo-0.08V, Consumable Electrode Melted, 1930 MPa — SAE International (2020)
  2. AMS 6417 — 300M Steel Bars and Forgings, Normalized and Tempered / Annealed — SAE International (2019)
  3. MMPDS-2023, Chapter 2 (Low-Alloy Ultrahigh-Strength Steels) — Battelle / FAA (2023)
  4. Aerospace Structural Metals Handbook — 300M — CINDAS (2015)
  5. ASM Handbook Vol.1: Properties and Selection — Irons, Steels and High-Performance Alloys — ASM International (1990)
  6. 300M (UNS K44220) alloy steel bar data — Carpenter Technology / Aubert & Duval (2022)
  7. 40CrNi2Si2MoVA (2015)
  8. 300M/40CrNi2Si2MoVA — 1688 / Mysteel (2026)

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.