Grade: 7050 (Aviation Grade)
Temper: O, T351, T451, T7451, T7651, etc.
Thickness: 4-260mm
Width: 1000-3800mm
Length: 2000-38000mm
Application: Aircraft Structural Parts.
Standard: AMS 4050, AMS 4342, AMS 4201, UNS A97050
7050 Aluminum Plates are the principal choice for aerospace applications, especially in the 3-6 inch thickness range.
7050 aluminum has better toughness/corrosion resistance characteristics than alloy 7075. Since it is less quench-sensitive than most other aerospace alloys, this alloy maintains its strength properties in thicker sections. While retaining good stress corrosion cracking resistance and fracture toughness levels.
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| Chemical Composition Limits | Others | |||||||||||
| Weight % | Al | Zr | Si | Fe | Cu | Mn | Mg | Cr | Zn | Ti | Each | Total |
| Minimum | 87.3 | 0.08 | – | – | 2 | – | 1.9 | – | 5.7 | – | – | – |
| Maximum | 90.3 | 0.15 | 0.12 | 0.15 | 2.6 | 0.1 | 2.6 | 0.04 | 6.7 | 0.06 | 0.05 | 0.15 |
Aluminum 7050-T7451 (7050-T73651)Subcategory: 7000 Series Aluminum Alloy; Aluminum Alloy; Metal; Nonferrous Metal Close Analogs: Composition Notes: Key Words: AA7050-T7451; AA7070-T73651, UNS A97050; ISO AlZn6CuMgZr; Aluminium 7050-T7451; Aluminium 7070-T73651
Material Notes:
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