AMS-5507 / 5524, ASTM-A-240
Physical Properties
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 |
N/A 12 in |
Length |
N/A 24 in |
Alloy |
N/A T316 Stainless Steel Alloy |
Thickness |
N/A 0.0060 in |
Thickness Tolerance |
N/A 5 % |
American Society for Testing and Materials (ASTM) Steel Standard |
N/A ASTM-A-240 |
Aerospace Material Specification (AMS) |
N/A AMS-5507 / 5524 |
Alloy Steel Type |
N/A Stainless Steel |
Material Form |
N/A Sheet |
Temper |
N/A Annealed Temper |
Chemical Composition
Maximum Carbon Composition |
N/A 0.08 % |
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 14.00 % |
Maximum Molybdenum Composition |
N/A 3.00 % |
Maximum Copper Composition |
N/A 0.75 % |
Chemical Composition Table |
N/A
|
Physical Properties
Minimum Tensile Strength |
N/A 75 ksi |
Minimum Yield Strength (0.2 Percent (%) Offset) |
N/A 30.0 ksi |
Minimum Elongation in 2 Inch (in) (Up to 0.0250 Inch (in) Thick) |
N/A 40 % |
Minimum Elongation in 2 Inch (in) (Over to 0.0250 Inch (in) Thick) |
N/A 45 % |
Maximum Hardness |
N/A 95 Rockwell B |