AMS-5519, ASTM-A-666

Physical Properties
  • Minimum Tensile Strength - 185 ksi
  • Minimum Yield Strength (0.2% Offset) - 140 ksi
  • Elongation in 2 Inches (Up to 0.0150" Thick) - 8%
  • Elongation in 2 Inches (Over 0.0150" Thick) - 9%
  • Minimum Hardness - 41 HRC (Product shall not be rejected on the basis of hardness if tensile properties … are acceptable)
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Unit of Measure
Items
0.0040 Inch (in) Thickness Stainless Steel Sheets

T301 Full Hard 0.0040" x 12" x 12"
List Price $75.00
0.0040 Inch (in) Thickness Stainless Steel Sheets

T301 Full Hard 0.0040" x 12" x 18"
List Price $85.00
0.0040 Inch (in) Thickness Stainless Steel Sheets

T301 Full Hard 0.0040" x 12" x 24"
List Price $95.00
0.0040 Inch (in) Thickness Stainless Steel Sheets

T301 Full Hard 0.0040" x 24" x 24"
List Price $115.00
0.0040 Inch (in) Thickness Stainless Steel Sheets

T301 Full Hard 0.0040" x 24" x 36"
List Price $135.00
Description N/A AMS-5519, ASTM-A-666

Physical Properties
  • Minimum Tensile Strength - 185 ksi
  • Minimum Yield Strength (0.2% Offset) - 140 ksi
  • Elongation in 2 Inches (Up to 0.0150" Thick) - 8%
  • Elongation in 2 Inches (Over 0.0150" Thick) - 9%
  • Minimum Hardness - 41 HRC (Product shall not be rejected on the basis of hardness if tensile properties … are acceptable)
Width N/A 12 in N/A 12 in N/A 12 in N/A 24 in N/A 24 in
Length N/A 12 in N/A 18 in N/A 24 in N/A 24 in N/A 36 in
Alloy N/A T301 Stainless Steel Alloy
Thickness N/A 0.0040 in
Thickness Tolerance N/A 5 %
American Society for Testing and Materials (ASTM) Steel Standard N/A ASTM-A-666
Aerospace Material Specification (AMS) N/A AMS-5519
Alloy Steel Type N/A Stainless Steel
Material Form N/A Sheet
Temper N/A Full Hard Temper
Maximum Carbon Composition N/A 0.15 %
Maximum Manganese Composition N/A 2.00 %
Maximum Silicon Composition N/A 1.00 %
Maximum Phosphorus Composition N/A 0.04 %
Maximum Sulfur Composition N/A 0.03 %
Maximum Chromium Composition N/A 18.00 %
Maximum Nickel Composition N/A 8.00 %
Maximum Molybdenum Composition N/A 0.75 %
Maximum Copper Composition N/A 0.75 %
Chemical Composition Table N/A

Minimum Tensile Strength N/A 185 ksi
Minimum Yield Strength (0.2 Percent (%) Offset) N/A 140 ksi
Minimum Elongation in 2 Inch (in) (Up to 0.0150 Inch (in) Thick) N/A 8 %
Minimum Elongation in 2 Inch (in) (Over 0.0150 Inch (in) Thick) N/A 9 %
Minimum Hardness1 N/A 41 Rockwell C
  • 1 Product shall not be rejected on the basis of hardness if tensile properties are acceptable