PRESIDENT METAL & ALLOYS

8740 ALLOY BAR

8740 ALLOY BAR

8740 is a Nickel Chrome Moly produced for case hardening. It can often be found in aerospace applications, when wear resistance, toughness, and strength are needed.

APPLICATIONS:

  • Aerospace Engine Parts
  • Aerospace Subassemblies
  • Aerospace Fasteners

Typical Chemical Properties

Minimum Properties Tensile Strength , psi 167,000
Yield Strength, psi 152,000
Elongation 15%
Hardness bhn 229
Chemistry Carbon( C) .38 -.43%
Chrome (Cr) 0.40-0.60 %
Manganese (Mn) 0.75-1.00 %
Molybdenum (Mo) 0.20 – .30%
Nickel ( Ni) 0.40 -0.70%
Phosphorus (P) .035% max
Sulphur (S) 0.04% max
Silicon (Si) 0.15- 0.30%