4130 Steel Sheets
4130 Steel Sheets This chromium-molybdenum alloy is one of the most widely used aircraft steels because of its combination of weldability, ease of fabrication and mild hardenability. In relatively thin section
4130 STEEL SHEETS MIL-S-6345A NORMALIZED Formerly MIL-S-18729C This chromium-molybdenum alloy is one of the most widely used aircraft steels because of its combination of weldability, ease of fabrication and mild hardenability. It will respond to heat treatment to high strength levels and yet, in the annealed condition, it has adequate strength for many applications. Used for the manufacture of parts and components. Tensile strength 75,000-85,000 PSI. Sheared to sheet and strip sizes listed below. Subject to availability of normalized sheet, annealed 4130 sheet may be substituted. Less 10% discount on 6 sheets 18" x 36" or 3 sheets of 18" x 72" per part number. If Mfg. Test Reports are required, there's a minimum $15.00 charge per order. Please indicate P/N 01-01133 in the Special Instructions Box during the checkout process.
This chromium-molybdenum alloy is one of the most widely used aircraft steels because of its combination of weldability, ease of fabrication and mild hardenability. In relatively thin section
4130 A/Q ANN MILS 18729 1.5 - 87981
AVIATIONEU NEW ERA 4130 Alloy Steel (Chromoly) Sheets (Normalized
Ultrasonic additive manufacturing of 4130 steel using Ni
Hot Rolled Steel Iron Sheet ASTM SAE 1010 1015 1020 1025 1040 1045
AISI 4130 Steel Plate at Rs 130/kilogram
RSW steel to aluminium Archives - AHSS Guidelines
Aviation & Performance Parts Ltd Auckland
ACS Homebuilders Main Axle Nuts
SAE/AISI 4130 1095 8620 1018 4140 1010 1045 6150 1020 1023 Steel
