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AMS-5516 / 5513, ASTM-A-666 / A-240

Physical Properties
  • Minimum Tensile Strength - 75 ksi
  • Minimum Yield Strength (0.2% Offset) - 30.0 ksi
  • Elongation in 2 Inches (0.002 to 0.003" Thick) - 30%
  • Elongation in 2 Inches (0.003 to 0.004" Thick) - 35%
  • Elongation in 2 Inches (Over 0.004" Thick) - 40%
  • Maximum Hardness - 92 HRB (Hardness (for ref. only)
Unit of Measure

Specifications

Width

24 in

Length

36 in

Alloy

T302 / 304 Stainless Steel Alloy

Thickness

0.0155 in

Thickness Tolerance

0.001 in

American Society for Testing and Materials (ASTM) Steel Standard

ASTM-A-666 / A-240

Aerospace Material Specification (AMS)

AMS-5516 / 5513

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

19.00 %

Maximum Nickel Composition

10.00 %

Maximum Molybdenum Composition

0.75 %

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) (0.002 to 0.003 Inch (in) Thick)

30 %

Minimum Elongation in 2 Inch (in) (0.003 to 0.004 Inch (in) Thick)

35 %

Minimum Elongation in 2 Inch (in) (Over 0.004 Inch (in) Thick)

40 %

Maximum Hardness

92 Rockwell B