Print Back
ASTM-B-209, AMS-4025

Physical Properties
  • Maximum Tensile Strength - 22,000 psi
  • Maximum Yield Strength - 12,000 psi
  • Elongation (0.008 to 0.009" Thick) - 12%
  • Elongation (0.010 to 0.020" Thick) - 14%
  • Elongation (0.021 to 0.128" Thick) - 16%
0.0080 Inch (in) Thickness Aluminum Sheets
Unit of Measure
Items 0.0080 Inch (in) Thickness Aluminum Sheets
6061 "O" Soft 0.0080" x 12" x 12"
6061 "O" Soft 0.0080" x 12" x 12"
List Price $75.00
0.0080 Inch (in) Thickness Aluminum Sheets
6061 "O" Soft 0.0080" x 12" x 18"
6061 "O" Soft 0.0080" x 12" x 18"
List Price $85.00
0.0080 Inch (in) Thickness Aluminum Sheets
6061 "O" Soft 0.0080" x 12" x 24"
6061 "O" Soft 0.0080" x 12" x 24"
List Price $95.00
Description N/A ASTM-B-209, AMS-4025

Physical Properties
  • Maximum Tensile Strength - 22,000 psi
  • Maximum Yield Strength - 12,000 psi
  • Elongation (0.008 to 0.009" Thick) - 12%
  • Elongation (0.010 to 0.020" Thick) - 14%
  • Elongation (0.021 to 0.128" Thick) - 16%
Width N/A 12 in
Length N/A 12 in N/A 18 in N/A 24 in
Alloy N/A 6061 Aluminum Alloy
Thickness N/A 0.0080 in
Thickness Tolerance N/A 0.0008 in
American Society for Testing and Materials (ASTM) Steel Standard N/A ASTM-B-209
Aerospace Material Specification (AMS) N/A AMS-4025
Material Form N/A Sheet
Temper N/A "O" Soft Temper
Maximum Silicon Composition N/A 0.80 %
Maximum Copper Composition N/A 0.40 %
Maximum Manganese Composition N/A 0.15 %
Maximum Magnesium Composition N/A 1.20 %
Maximum Chromium Composition N/A 0.35 %
Maximum Zinc Composition N/A 0.25 %
Maximum Titanium Composition N/A 0.15 %
Maximum Others Composition (Each) N/A 0.05 %
Maximum Others Composition (Total) N/A 0.15 %
Chemical Composition Table N/A

Maximum Tensile Strength N/A 22,000 psi
Maximum Yield Strength N/A 12,000 psi
Minimum Elongation (0.008 to 0.009 Inch (in) Thick) N/A 12 %
Minimum Elongation (0.010 to 0.020 Inch (in) Thick) N/A 14 %
Minimum Elongation (0.021 to 0.128 Inch (in) Thick) N/A 16 %