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Aluminum Plate
7075-T651
Description

One of the highest strength, commerically available alloys with fair corrosion resistance and machinability. Low workability rating and welded only by the resistance and machinability.
Typical Applications
  • Aircraft skins
  • Cowls
  • Structures
  • Molds and Mold Bases
Chemical Composition Limits
  • Silicon: 0.40
  • Iron: 0.50
  • Copper: 1.2 - 2.0
  • Manganese: 0.30
  • Magnesium: 2.1 - 2.9
  • Chromium: 0.18 - 0.28
  • Zinc: 5.1 - 6.1
  • Titanium: 0.20
  • Aluminum: Remainder
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