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Aluminum 2214 · temper

Aluminum 2214-T6

Properties of the T6 condition, compared with the other 2214 tempers.

Peak-strength condition for forgings, extrusions and machined fittings where residual stress is not critical.

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What is 2214-T6?

2214-T6 is 2214 in the T6 temper — peak-strength condition for forgings, extrusions and machined fittings where residual stress is not critical. 2214-T6 has a yield strength of 414 MPa (60 ksi) and a tensile strength of 483 MPa (70.1 ksi) — stronger than 88% of aluminum grades. Elongation at break is 13% and the elastic modulus is 73 GPa (10.6 Msi). 2214-T6 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

  • Easy to machine — 78/100, better than 89% of aluminum grades
  • High strength — 414 MPa (60 ksi), better than 88% of aluminum grades
  • Ductile — tolerates forming and impact — 13%, better than 79% 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-T6 properties

Typical room-temperature values for 2214-T6 — 17 properties are specific to this condition; the rest are grade-level values shared by every 2214 temper. Each bar shows where the value sits among the aluminum grades in FabDigit's library — further right is higher.

Physical3

2214-T6 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).

Density2.8 g/cm³0.1 lb/in³
Melting Point (Solidus)507°C945 °F
Liquidus Temperature638°C1,180 °F

Mechanical15

2214-T6 has a yield strength of 414 MPa (60 ksi) and a tensile strength of 483 MPa (70.1 ksi) — stronger than 88% of aluminum grades. Elongation at break is 13% and the elastic modulus is 73 GPa (10.6 Msi).

Elastic (Young's) Modulus73 GPa10.6 Msi
Shear Modulus27.5 GPa4 Msi
Bulk Modulus75 GPa10.9 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)483 MPa70.1 ksi
Yield Strength (0.2% offset)414 MPa60 ksi
Elongation at Break13%
Reduction in Area25%
Compressive Strength425 MPa61.6 ksi
Shear Strength290 MPa42.1 ksi
Fatigue Strength (Endurance Limit)124 MPa18 ksi
Fracture Toughness (K_IC)25 MPa·√m22.8 ksi·√in
Hardness, Brinell135 HB
Hardness, Rockwell B82 HRB
Hardness, Vickers145 HV

Thermal6

2214-T6 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).

Thermal Conductivity155 W/m·K89.6 BTU/hr·ft·°F
Specific Heat Capacity864 J/kg·K0.21 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)22.5 µm/m·K12.5 µin/in·°F
Latent Heat of Fusion390 J/g168 BTU/lb
Max Service Temperature (continuous)150°C302 °F
Min Service Temperature-196°C-321 °F

Electrical3

2214-T6 conducts electricity at 40 % IACS, better than 72% of aluminum grades.

Electrical Conductivity40 % IACS
Electrical Resistivity4.3×10⁻⁸ Ω·m1.69 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is poor (32/100), worse than 94% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.78 V
Corrosion ResistancePoor32/100
Chemical Resistance SummaryGood in dry air and neutral organics; poor in chloride-bearing water, seawater and acids/alkalis — Cu-rich phases drive pitting and intergranular attack; requires alclad, anodize or primer, and isolation from steel/CFRP.

Sustainability4

Producing a kilogram of 2214-T6 takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 75% of aluminum grades. Typical recycled content is 10%.

Embodied Energy (primary production)205 MJ/kg88,134 BTU/lb
Embodied Carbon (primary production)12.5 kg CO₂/kg
Embodied Water1,150 L/kg138 gal/lb
Typical Recycled Content10%

Manufacturability8

2214-T6's machinability is very good (78/100, better than 89% of aluminum grades); weldability poor (25/100); formability poor (32/100).

MachinabilityVery good78/100
Machinability Rating (AISI 1212 = 100 %)160%
WeldabilityPoor25/100
Formability (cold)Poor32/100
CastabilityPoor30/100
Brazeability / SolderabilityPoor15/100
PolishabilityGood55/100
Anodizing Responsefair — high Cu gives dark, patchy and less protective sulfuric films; hard-coat is possible but thinner and more brittle; chromic acid anodize or alclad preferred for aerospace parts.

Values are nominal handbook figures for design screening. Certified mill or lot data ships with every FabDigit order on request.

Other 2214 tempers and conditions

2214 is also supplied in 6 other conditions. The full side-by-side table is on the 2214 overview.

Working with 2214-T6

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.

ElementSpec limit (wt %)Nominal
Si0.5 – 1.20.8
FeLower Fe than 2014 — the defining difference of 2214≤ 0.30.15
Cu3.9 – 54.4
Mn0.4 – 1.20.8
Mg0.2 – 0.80.5
Cr≤ 0.1
Zn≤ 0.25
Ti≤ 0.15
Zr+Ticombined limit where applicable≤ 0.2
Others (each)≤ 0.05
Others (total)≤ 0.15
Albalance

2214-T6 — frequently asked

What is 2214-T6 used for?

2214-T6 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-T6?

2214-T6 has a typical yield strength of 414 MPa (60 ksi) and a tensile strength of 483 MPa (70.1 ksi) — stronger than 88% of aluminum grades. Strength varies by condition: see the 7 listed tempers.

Is 2214-T6 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-T6 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-T6?

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-T6 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-T6?

2214-T6 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-T6?

Yes — 2214-T6 is available for CNC machining and sheet metal with instant online pricing. Upload a STEP file to get a price and a DFM check.

Sources

  1. International Alloy Designations and Chemical Composition Limits for Wrought Aluminum (Teal Sheets)The Aluminum Association (2018)
  2. EN 573-3 Aluminium and aluminium alloys — Chemical compositionCEN (2019)
  3. ASTM B209 / B211 / B247 (aluminum plate, bar, forgings)ASTM International (2021)
  4. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous AlloysASM International (1990)
  5. MMPDS-17 Metallic Materials Properties Development and StandardizationBattelle/FAA (2022)
  6. ASM Handbook Vol. 13B — Corrosion: MaterialsASM 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.