Technical guide · 2026-08-03
2xxx Aluminum-Copper Alloys
2xxx wrought alloys use copper as the principal alloying element and are generally heat treatable. They provide high specific strength and fatigue performance for aerospace and transport structures, while corrosion protection, fracture toughness and welding limitations need explicit review.
01
Definition and boundary
The series is a first filter only; exact alloy, temper, product form and governing standard control acceptance and substitution.
Reference information only: final acceptance is controlled by the ordered product specification, condition, dimensions and certified test results.
02
How the material system works
Principal alloying elements define the series and available strengthening response.
Temper records strain hardening and/or thermal processing history.
Thickness, direction and product route influence guaranteed properties.
03
Representative grades and systems
| Grade or system | Selection focus | Qualification |
|---|---|---|
| 2014 | High-strength forging/extrusion and machinery alloy. | Verify the ordered product specification, condition and dimensions before substitution. |
| 2024 | Major aerospace sheet/plate alloy with temper and grain-direction controls. | Verify the ordered product specification, condition and dimensions before substitution. |
| 2219 | Heat-treatable alloy used for welded and elevated-temperature aerospace systems. | Verify the ordered product specification, condition and dimensions before substitution. |
04
Properties and trade-offs
Density remains low, while strength varies widely by alloy and temper.
Corrosion, conductivity and finish response depend on chemistry and surface condition.
Joining can change local temper and usable design strength.
05
Product forms and supply conditions
06
Applications and selection
Applications and selection
- Aircraft skins, structures and fasteners
- High-strength transport and machinery components
- Cryogenic or welded tanks where the selected alloy is qualified
Properties and trade-offs
- Define structural, corrosion, thermal, electrical, forming and appearance priorities.
- Choose exact alloy and temper for the required product form and section.
- Verify weld-zone properties, galvanic contact and coating/anodizing route.
07
Fabrication, durability and inspection
Use forming, welding and machining practice for the exact alloy-temper and product thickness.
Control heat input because welding can reduce heat-treated or work-hardened strength near the joint.
Prevent embedded steel contamination and manage oxide, cleaning, anodizing or coating compatibility.
08
Procurement checklist
- Specify alloy, temper, product standard, dimensions, tolerances and surface condition as one identity.
- State direction-dependent properties, flatness, residual stress, conductivity, anodizing or corrosion tests when relevant.
- Define film/interleaf protection, packing, moisture control, traceability and certificate requirements.
09
Standards, sources and review
Standards and designation context
- The Aluminum Association international alloy registration records
- ANSI H35 alloy, temper and tolerance systems
- Product-specific ASTM/EN/ISO/AMS or national specifications
Authoritative research sources
The Aluminum Association · Standards portal, accessed 2026
The Aluminum Association · December 2025 registration record
The Aluminum Association · 2024 edition overview