Aluminum 2214-T6511
Temper
AA 2214 · EN AW-2214, AW 2214
T6511 = t6, stress relieved by stretching, minor straightening
Extruded bar, rod and profile equivalent of T651 for long machined structural members.
Values for the T6511 condition
Other 2214 tempers and conditions
2214 is listed in 7 conditions; see the grade overview at 2214.
Compare all 7 conditionsHide
| Condition · open for datasheet | Best for | Yield MPa | Tensile MPa | Elong. % | Hardness | Conductivity |
|---|---|---|---|---|---|---|
Annealed | Softest condition for deep forming, heavy bending or straightening before solution treatment. | 95 | 185 | 18 | 45 HB | 50 % IACS |
Solution heat treated and naturally aged | Choose when moderate strength with better ductility and forming/riveting capability is needed before final aging. | 290 | 425 | 18 | 105 HB | 34 % IACS |
T4, stress relieved by stretching | Plate/bar version of T4 with low residual stress — for parts that will be machined then artificially aged. | 290 | 425 | 16 | 105 HB | 34 % IACS |
T6, stress relieved by compression | Hand/die forging condition where stretching is impractical; low residual stress for heavily machined forgings. | 400 | 460 | 8 | 130 HB | 40 % IACS |
Solution heat treated and artificially aged | Peak-strength condition for forgings, extrusions and machined fittings where residual stress is not critical. | 414 | 483 | 13 | 135 HB | 40 % IACS |
T6, stress relieved by stretching | Standard aerospace plate/bar condition — full T6 strength with minimal residual stress so machined parts stay flat. | 415 | 470 | 9 | 135 HB | 40 % IACS |
T6511This page T6, stress relieved by stretching, minor straightening | Extruded bar, rod and profile equivalent of T651 for long machined structural members. | 415 | 470 | 8 | 135 HB | 40 % IACS |
What is 2214-T6511?
2214-T6511 is 2214 in the T6511 temper — extruded bar, rod and profile equivalent of T651 for long machined structural members. 2214-T6511 has a yield strength of 415 MPa (60.2 ksi) and a tensile strength of 470 MPa (68.2 ksi) — stronger than 89% of aluminum grades. Elongation at break is 8% and the elastic modulus is 73 GPa (10.6 Msi). 2214-T6511 has a density of 2.8 g/cm³ (0.101 lb/in³), heavier than 81% of aluminum grades. It melts at 507°C (945 °F).
Advantages
- High strength — 415 MPa (60.2 ksi), better than 89% of aluminum grades
- Easy to machine — 78/100, better than 89% of aluminum grades
Limitations
- Needs corrosion protection — 32/100, worse than 94% of aluminum grades
- Difficult to weld — 25/100, worse than 76% of aluminum grades
2214-T6511 properties
Typical room-temperature values for 2214-T6511; 22 are specific to this condition. Other listed values are 2214 reference data and may not represent this condition. Bars are the position among aluminum grades.
Physical3
2214-T6511 has a density of 2.8 g/cm³ (0.101 lb/in³), heavier than 81% of aluminum grades. It melts at 507°C (945 °F).
Mechanical15
2214-T6511 has a yield strength of 415 MPa (60.2 ksi) and a tensile strength of 470 MPa (68.2 ksi) — stronger than 89% of aluminum grades. Elongation at break is 8% and the elastic modulus is 73 GPa (10.6 Msi).
Thermal6
2214-T6511 is rated for continuous service to 150°C (302 °F). It conducts heat at 155 W/m·K (89.6 BTU/hr·ft·°F), better than 71% of aluminum grades. Thermal expansion is 22.5 µm/m·K (12.5 µin/in·°F).
Electrical3
2214-T6511 conducts electricity at 40 % IACS, better than 72% of aluminum grades.
Chemical & Environmental3
Corrosion resistance is poor (32/100), worse than 94% of aluminum grades.
Sustainability4
Producing a kilogram of 2214-T6511 takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 76% of aluminum grades. Typical recycled content is 10%.
Manufacturability8
2214-T6511's machinability is very good (78/100, better than 89% of aluminum grades); weldability poor (25/100); formability poor (33/100).
Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.
Working with 2214-T6511
Is 2214 easy to machine?
Excellent chip control in T6/T651 — use polished-flute carbide, high speeds with flood or MQL; avoid re-introducing residual stress in thin machined webs.
Can 2214 be welded?
Not recommended for fusion welding (hot cracking with Cu-rich melt); join by rivets, bolts, adhesive or friction-stir; if arc welded, use 4145/4043 filler and re-heat-treat.
Can 2214 be formed, bent or molded?
Form in O or fresh T4 (within a few hours of quench, or hold sub-zero); T6/T651 has limited bend ductility and springback is high.
What surface finishes work on 2214?
Chromic-acid anodize, chemical conversion coat or alclad plus epoxy primer for corrosion protection; sulfuric anodize gives dark, non-uniform color due to CuAl2 phases.
2214 chemical composition (wt %)
Limits by weight percent from the governing specification, written the way the spec states them — a single maximum for impurities, a range for alloying elements, and the base element as balance. Nominal is the typical mid-range value.
| Element | Spec limit (wt %) | Nominal |
|---|---|---|
| Si | 0.5 – 1.2 | 0.8 |
| FeLower Fe than 2014 — the defining difference of 2214 | ≤ 0.3 | 0.15 |
| Cu | 3.9 – 5 | 4.4 |
| Mn | 0.4 – 1.2 | 0.8 |
| Mg | 0.2 – 0.8 | 0.5 |
| Cr | ≤ 0.1 | — |
| Zn | ≤ 0.25 | — |
| Ti | ≤ 0.15 | — |
| Zr+Ticombined limit where applicable | ≤ 0.2 | — |
| Others (each) | ≤ 0.05 | — |
| Others (total) | ≤ 0.15 | — |
| Al | balance | — |
2214-T6511 — frequently asked
What is 2214-T6511 used for?
2214-T6511 is typically used for aerospace structural forgings, wheel hubs, machined airframe fittings, thick-plate machined components, high-stress tooling and dies and extruded structural sections. In short: high-strength forging; 2014 variant.
What is the yield strength of 2214-T6511?
2214-T6511 has a typical yield strength of 415 MPa (60.2 ksi) and a tensile strength of 470 MPa (68.2 ksi) — stronger than 89% of aluminum grades. Strength varies by condition: see the 7 listed tempers.
Is 2214-T6511 easy to machine?
Yes — machinability is rated very good (78/100, better than 89% of aluminum grades). Excellent chip control in T6/T651 — use polished-flute carbide, high speeds with flood or MQL; avoid re-introducing residual stress in thin machined webs.
Can 2214-T6511 be welded?
Not readily — weldability is rated poor (25/100). Not recommended for fusion welding (hot cracking with Cu-rich melt); join by rivets, bolts, adhesive or friction-stir; if arc welded, use 4145/4043 filler and re-heat-treat.
What surface finishes work on 2214-T6511?
Chromic-acid anodize, chemical conversion coat or alclad plus epoxy primer for corrosion protection; sulfuric anodize gives dark, non-uniform color due to CuAl2 phases.
Can 2214-T6511 be formed, bent or molded?
Form in O or fresh T4 (within a few hours of quench, or hold sub-zero); T6/T651 has limited bend ductility and springback is high.
What is the maximum service temperature of 2214-T6511?
2214-T6511 is rated for continuous use to about 150°C (302 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.
Can FabDigit make parts in 2214-T6511?
Yes — 2214-T6511 is available for CNC machining and sheet metal; every part is priced by an engineer rather than instantly. Upload a STEP file to get a price and a DFM check.
Sources
- International Alloy Designations and Chemical Composition Limits for Wrought Aluminum (Teal Sheets) — The Aluminum Association (2018)
- EN 573-3 Aluminium and aluminium alloys — Chemical composition — CEN (2019)
- ASTM B209 / B211 / B247 (aluminum plate, bar, forgings) — ASTM International (2021)
- ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys — ASM International (1990)
- MMPDS-17 Metallic Materials Properties Development and Standardization — Battelle/FAA (2022)
- ASM Handbook Vol. 13B — Corrosion: Materials — ASM International (2005)
Property data is compiled from published supplier and standards handbooks and normalised for comparison. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.