AMS-5507 / 5524, ASTM-A-240

Physical Properties
  • Minimum Tensile Strength - 75 ksi
  • Minimum Yield Strength (0.2% Offset) - 30.0 ksi
  • Elongation in 2 Inches (Up to 0.0250" Thick) - 40%
  • Elongation in 2 Inches (Over 0.0250" Thick) - 45%
  • Maximum Hardness - 95 HRB
Unit of Measure

Specifications

Width

 12 in

Length

 24 in

Alloy

 T316 Stainless Steel Alloy

Thickness

 0.0120 in

Thickness Tolerance

 5 %

American Society for Testing and Materials (ASTM) Steel Standard

 ASTM-A-240

Aerospace Material Specification (AMS)

 AMS-5507 / 5524

Alloy Steel Type

 Stainless Steel

Material Form

 Sheet

Temper

 Annealed Temper

Chemical Composition

Maximum Carbon Composition

 0.08 %

Maximum Manganese Composition

 2.00 %

Maximum Silicon Composition

 1.00 %

Maximum Phosphorus Composition

 0.04 %

Maximum Sulfur Composition

 0.03 %

Maximum Chromium Composition

 18.00 %

Maximum Nickel Composition

 14.00 %

Maximum Molybdenum Composition

 3.00 %

Maximum Copper Composition

 0.75 %

Chemical Composition Table

Physical Properties

Minimum Tensile Strength

 75 ksi

Minimum Yield Strength (0.2 Percent (%) Offset)

 30.0 ksi

Minimum Elongation in 2 Inch (in) (Up to 0.0250 Inch (in) Thick)

 40 %

Minimum Elongation in 2 Inch (in) (Over to 0.0250 Inch (in) Thick)

 45 %

Maximum Hardness

 95 Rockwell B