AMS-5517, ASTM-A-666

Physical Properties
  • Minimum Tensile Strength - 125 ksi
  • Minimum Yield Strength (0.2% Offset) - 75.0 ksi
  • Elongation in 2 Inches - 25%
  • Minimum Hardness - 25 HRC (Product shall not be rejected on the basis of hardness if tensile properties … are acceptable)
Unit of Measure

Specifications

Width

N/A 12 in

Length

N/A 18 in

Alloy

N/A T301 Stainless Steel Alloy

Thickness

N/A 0.0120 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-5517

Alloy Steel Type

N/A Stainless Steel

Material Form

N/A Sheet

Temper

N/A Quarter Hard Temper

Chemical Composition

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

Physical Properties

Minimum Tensile Strength

N/A 125 ksi

Minimum Yield Strength (0.2 Percent (%) Offset)

N/A 75.0 ksi

Minimum Elongation in 2 Inch (in)

N/A 25 %
Minimum Hardness1 N/A 25 Rockwell C
  • 1 Product shall not be rejected on the basis of hardness if tensile properties are acceptable