| Items |
 /Asset/-020-4.JPG T316 Annealed 0.0200" x 12" x 12" T316 Annealed 0.0200" x 12" x 12" List Price $75.00
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/Asset/-020-4.JPG T316 Annealed 0.0200" x 12" x 18" T316 Annealed 0.0200" x 12" x 18" List Price $85.00
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/Asset/-020-4.JPG T316 Annealed 0.0200" x 12" x 24" T316 Annealed 0.0200" x 12" x 24" List Price $95.00
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/Asset/-020-4.JPG T316 Annealed 0.0200" x 24" x 24" T316 Annealed 0.0200" x 24" x 24" List Price $115.00
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/Asset/-020-4.JPG T316 Annealed 0.0200" x 24" x 36" T316 Annealed 0.0200" x 24" x 36" List Price $135.00
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| Description |
AMS-5507 / 5524, ASTM-A-240 Physical Properties
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| Width | 12 in | 12 in | 12 in | 24 in | 24 in | |||||
| Length | 12 in | 18 in | 24 in | 24 in | 36 in | |||||
| Alloy | T316 Stainless Steel Alloy | |||||||||
| Thickness | 0.0200 in | |||||||||
| Thickness Tolerance | 0.001 in | |||||||||
| 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 | |||||||||
| 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 |
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| 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 | |||||||||
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