FabDigit

Aluminum 7012 · temper

Aluminum 7012-T651

Properties of the T651 condition, compared with the other 7012 tempers.

Choose for thick plate that will be heavily machined — stretch stress-relief minimises distortion of mould and jig plates.

CNC machiningSheet metalPremium cost $$$

What is 7012-T651?

7012-T651 is 7012 in the T651 temper — choose for thick plate that will be heavily machined — stretch stress-relief minimises distortion of mould and jig plates. 7012-T651 has a yield strength of 495 MPa (71.8 ksi) and a tensile strength of 540 MPa (78.3 ksi) — stronger than 96% of aluminum grades. Elongation at break is 9% and the elastic modulus is 71 GPa (10.3 Msi). 7012-T651 has a density of 2.81 g/cm³ (0.102 lb/in³), heavier than 86% of aluminum grades. It melts at 480°C (896 °F).

Advantages

  • High strength — 495 MPa (71.8 ksi), better than 96% of aluminum grades
  • Easy to machine — 75/100, better than 86% of aluminum grades

Limitations

  • Needs corrosion protection — 33/100, worse than 90% of aluminum grades
  • Difficult to weld — 22/100, worse than 83% of aluminum grades
  • Limited service temperature — 120°C (248 °F), worse than 79% of aluminum grades

7012-T651 properties

Typical room-temperature values for 7012-T651 — 8 properties are specific to this condition; the rest are grade-level values shared by every 7012 temper. Each bar shows where the value sits among the aluminum grades in FabDigit's library — further right is higher.

Physical3

7012-T651 has a density of 2.81 g/cm³ (0.102 lb/in³), heavier than 86% of aluminum grades. It melts at 480°C (896 °F).

Density2.81 g/cm³0.1 lb/in³
Melting Point (Solidus)480°C896 °F
Liquidus Temperature635°C1,175 °F

Mechanical13

7012-T651 has a yield strength of 495 MPa (71.8 ksi) and a tensile strength of 540 MPa (78.3 ksi) — stronger than 96% of aluminum grades. Elongation at break is 9% and the elastic modulus is 71 GPa (10.3 Msi).

Elastic (Young's) Modulus71 GPa10.3 Msi
Shear Modulus26.9 GPa3.9 Msi
Bulk Modulus70 GPa10.2 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)540 MPa78.3 ksi
Yield Strength (0.2% offset)495 MPa71.8 ksi
Elongation at Break9%
Compressive Strength520 MPa75.4 ksi
Shear Strength320 MPa46.4 ksi
Fatigue Strength (Endurance Limit)155 MPa22.5 ksi
Fracture Toughness (K_IC)28 MPa·√m25.5 ksi·√in
Hardness, Brinell158 HB
Hardness, Vickers170 HV

Thermal6

7012-T651 is rated for continuous service to 120°C (248 °F). It conducts heat at 135 W/m·K (78 BTU/hr·ft·°F), worse than 58% of aluminum grades. Thermal expansion is 23.4 µm/m·K (13 µin/in·°F).

Thermal Conductivity135 W/m·K78 BTU/hr·ft·°F
Specific Heat Capacity865 J/kg·K0.21 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)23.4 µm/m·K13 µin/in·°F
Latent Heat of Fusion385 J/g166 BTU/lb
Max Service Temperature (continuous)120°C248 °F
Min Service Temperature-196°C-321 °F

Electrical3

7012-T651 conducts electricity at 32 % IACS, worse than 63% of aluminum grades.

Electrical Conductivity32 % IACS
Electrical Resistivity5.4×10⁻⁸ Ω·m2.13 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is poor (33/100), worse than 90% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.84 V
Corrosion ResistancePoor33/100
Chemical Resistance SummaryGood in neutral atmospheres and fresh water; attacked by strong acids/alkalis, marine and chloride exposure causes pitting and (in T6) stress-corrosion cracking — use T73/T76 plus anodizing or cladding.

Sustainability4

Producing a kilogram of 7012-T651 takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 75% of aluminum grades. Typical recycled content is 20%.

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 Content20%

Manufacturability7

7012-T651's machinability is very good (75/100, better than 86% of aluminum grades); weldability poor (22/100); formability poor (22/100).

MachinabilityVery good75/100
Machinability Rating (AISI 1212 = 100 %)90%
WeldabilityPoor22/100
Formability (cold)Poor22/100
Brazeability / SolderabilityNot recommended10/100
PolishabilityGood60/100
Anodizing Responsegood — hard and clear/sulphuric anodizing both work; Zn+Cu content gives a slightly grey/yellow tint, so decorative colour matching is less consistent than 6xxx.

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

Other 7012 tempers and conditions

7012 is also supplied in 5 other conditions. The full side-by-side table is on the 7012 overview.

Working with 7012-T651

Is 7012 easy to machine?

Machines very freely in T6/T651 with sharp polished PCD or uncoated carbide, high speed and generous coolant; chips are short and finishes excellent.

Can 7012 be welded?

Not recommended for fusion welding (hot cracking, large HAZ strength loss) — join by bolting, bonding or friction-stir welding with post-weld ageing.

Can 7012 be formed, bent or molded?

Form in F/T4 only; T6 material has low ductility and bend radii must be generous — cold bending of aged plate risks cracking.

What surface finishes work on 7012?

Takes clear and hard anodizing well (slightly grey tone), chromate/Ti-Zr conversion coatings and primers; avoid direct contact with steel/CFRP without insulation.

7012 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
Siimpurity limit≤ 0.150.06
Feimpurity limit≤ 0.250.12
Cu0.8 – 1.21
Mn≤ 0.10.03
Mg1.8 – 2.22
Cr≤ 0.050.02
Znprincipal hardening addition5.8 – 6.56.1
Zrgrain-structure control (dispersoids)0.08 – 0.20.14
Ti≤ 0.050.02
Other, each≤ 0.05
Other, total≤ 0.15
Albalance

7012-T651 — frequently asked

What is 7012-T651 used for?

7012-T651 is typically used for aerospace forgings, helicopter rotor parts, high-strength structural extrusions, mould and tooling plate, machined structural fittings from thick plate and sporting goods frames. In short: european aero forging alloy.

What is the yield strength of 7012-T651?

7012-T651 has a typical yield strength of 495 MPa (71.8 ksi) and a tensile strength of 540 MPa (78.3 ksi) — stronger than 96% of aluminum grades. Strength varies by condition: see the 6 listed tempers.

Is 7012-T651 easy to machine?

Yes — machinability is rated very good (75/100, better than 86% of aluminum grades). Machines very freely in T6/T651 with sharp polished PCD or uncoated carbide, high speed and generous coolant; chips are short and finishes excellent.

Can 7012-T651 be welded?

Not readily — weldability is rated poor (22/100). Not recommended for fusion welding (hot cracking, large HAZ strength loss) — join by bolting, bonding or friction-stir welding with post-weld ageing.

What surface finishes work on 7012-T651?

Takes clear and hard anodizing well (slightly grey tone), chromate/Ti-Zr conversion coatings and primers; avoid direct contact with steel/CFRP without insulation.

Can 7012-T651 be formed, bent or molded?

Form in F/T4 only; T6 material has low ductility and bend radii must be generous — cold bending of aged plate risks cracking.

What is the maximum service temperature of 7012-T651?

7012-T651 is rated for continuous use to about 120°C (248 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

Can FabDigit make parts in 7012-T651?

Yes — 7012-T651 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. EN 755-2 Aluminium alloy extruded rod/bar, tube and profiles — Mechanical propertiesCEN (2016)
  4. ASM Handbook Vol. 2: Properties and Selection — Nonferrous AlloysASM International (1990)
  5. ASM Handbook Vol. 13B: Corrosion — Materials (aluminium alloys)ASM International (2005)
  6. High-strength 7xxx extrusion and plate alloy datasheets (Al-Zn-Mg-Cu-Zr)Constellium / Alcoa (2021)

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.