Material datasheet · Low-alloy steel

AISI 4130 Cr-Mo Alloy Steel

UNS G41300 · Normalized or annealed; commonly TIG/MIG welded as tubing

The weldable Cr-Mo alloy steel. Aircraft tubing standard.

UTS
97 ksi
670 MPa
Yield strength
63 ksi
435 MPa
Elongation
25%
in 2″
Hardness
HRB 92 (normalized)
Typical
Density
0.284
lb/in³ · 7.85 g/cc
Modulus E
29.0
Mpsi · 200 GPa
CTE
6.8
µin/in·°F
Service T (max)
800°F
Continuous

Chemical composition

Nominal % by weight.

Element% by wt
FeBal.
C0.28–0.33
Cr0.80–1.10
Mo0.15–0.25

Applicable specifications

AMS / ASTM / MIL.

  • AMS 6345
  • AMS 6360 (tube)
  • AMS 6373
  • MIL-T-6736

Machining guidance

CNC parameters and tooling.

Roughing SFM
300–400
Finishing SFM
400–500
Machinability rating
70 / 100
Steel scale (AISI B1112 = 100)
Coolant
Flood
Tooling

Carbide; standard geometry

Notes

The weldable Cr-Mo. Holds up well after weld + stress relief. Lower hardenability than 4140.

Stock & cost

Forms and Q1 2026 pricing.

Available forms
Tube (round/rectangular)BarPlate
Stock cost
$1.50–$3.00/lb
Mid-quantity bar/plate, Q1 2026 USD
Common finishes
  • Powder coat
  • Paint (zinc primer)
  • Phosphate
  • Black oxide

Typical applications

Where 4130 Chromoly is the right pick.

  • Aircraft tubular structure
  • Race car frames
  • Firearms barrels
  • Bicycle frames
  • Roll cages

Alternative materials

Substitute or upgrade options.

  • 4140 (higher strength, lower weldability)
  • 1020 mild steel (cheaper, lower strength)

Digital Machine · Quick-Turn CNC · California

Machine your part in 4130 Chromoly.

Production CNC milling and turning. Confirm material, inspection and documentation requirements when requesting a quote.

Phone: 805-697-7829
Email: sales@digitalmachine.com
Web: digitalmachine.com
Datasheet generated 2026 · Mechanical values are typical room-T averages from MMPDS / ASM. Verify against MTRs for design-critical applications.
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