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4130 Sheet 6 X 12 X .125

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Part Number(s): 03-55300

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Unit of Measure Name: Units
Internal Reference: RX1-03-55300

ThicknessSize
(in.)
Part No.
.1256 x 1203-55300

Overview

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.

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