- 7075 Aluminum T6, T73 & T76, for aircraft and aerospace structures,
combination of high strength with moderate toughness and corrosion resistance .
- 7055 Aluminum T7751, for applications where compressive strength
- 7475 Aluminum T61, T651, T7651 & T7351, for fracture critical components of
high performance aircraft
- 2324-T39 Aluminum, for higher strength, toughness and good resistance to fatigue
crack propagation is required.
- 6013 Aluminum T4 & T6, for fuselage panels, leading and trailing edges and
engine cowlings.
- 2124 Aluminum T851 for moderately elevated temperature applications (250-350°F,
121-177°C).
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