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Aluminum Sheet
7075-T6 
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. Typically used as aircraft skins, cowls, and structures.

Typical Applications
  • Aircraft Skins and Structurals
Chemical Composition Limits
  • Silicon: 0.40
  • Iron: 0.50
  • Copper: 1.20 - 2.00
  • Manganese: .30
  • Magnesium: 2.10 - 2.90
  • Chromium: 0.18 - 0.28
  • Zinc: 5.10 - 6.10
  • Nickel: --
  • Titanium: 0.20
  • Aluminum: Remainder
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