AMS-5529, ASTM-A-693

Physical Properties
  • Minimum Tensile Strength - 200 ksi
  • Minimum Yield Strength (0.2% Offset) - 175 ksi
  • Elongation in 2 Inches - 1%
  • Maximum Hardness - 41 HRC (Product shall not be rejected on the basis of hardness if tensile properties … are acceptable. This is a heat treatable alloy (CH-900) - expected physical properties are available on a per lot, per request basis.)
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Unit of Measure
Items
0.0250 Inch (in) Thickness Stainless Steel Sheets

17-7PH Condition 'C' 0.0250" x 12" x 12"
List Price $85.00
0.0250 Inch (in) Thickness Stainless Steel Sheets

17-7PH Condition 'C' 0.0250" x 12" x 18"
List Price $95.00
0.0250 Inch (in) Thickness Stainless Steel Sheets

17-7PH Condition 'C' 0.0250" x 12" x 24"
List Price $105.00
0.0250 Inch (in) Thickness Stainless Steel Sheets

17-7PH Condition 'C' 0.0250" x 24" x 24"
List Price $125.00
0.0250 Inch (in) Thickness Stainless Steel Sheets

17-7PH Condition 'C' 0.0250" x 24" x 36"
List Price $145.00
Description N/A AMS-5529, ASTM-A-693

Physical Properties
  • Minimum Tensile Strength - 200 ksi
  • Minimum Yield Strength (0.2% Offset) - 175 ksi
  • Elongation in 2 Inches - 1%
  • Maximum Hardness - 41 HRC (Product shall not be rejected on the basis of hardness if tensile properties … are acceptable. This is a heat treatable alloy (CH-900) - expected physical properties are available on a per lot, per request basis.)
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 17-7PH Stainless Steel Alloy
Thickness N/A 0.0250 in
Thickness Tolerance N/A 0.001 in
American Society for Testing and Materials (ASTM) Steel Standard N/A ASTM-A-693
Aerospace Material Specification (AMS) N/A AMS-5529
Alloy Steel Type N/A Stainless Steel
Material Form N/A Sheet
Temper N/A Condition 'C' Temper
Maximum Carbon Composition N/A 0.09 %
Maximum Manganese Composition N/A 1.00 %
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 7.75 %
Maximum Aluminum Composition N/A 1.50 %
Chemical Composition Table N/A

Minimum Tensile Strength N/A 200 ksi
Minimum Yield Strength (0.2 Percent (%) Offset) N/A 175 ksi
Minimum Elongation in 2 Inch (in) N/A 1 %
Minimum Hardness1 N/A 41 Rockwell C
  • 1 Product shall not be rejected on the basis of hardness if tensile properties are acceptable