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Aluminum 7012-T6511

Temper

AA 7012 · EN AW-7012, AW 7012

T6511 = t6, stress relieved by stretching, minor straightening

Standard low-residual-stress temper for 7012 extruded bar and profiles destined for precision machining.

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Values for the T6511 condition

Other 7012 tempers and conditions

7012 is listed in 6 conditions; see the grade overview at 7012.

Compare all 6 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Solution heat treated and naturally aged
Intermediate condition used when some forming or straightening is needed before final artificial ageing.30044015125 HB29 % IACS
Solution heat treated and overaged for stress-corrosion resistance
Pick for humid, marine or sustained-tension service where stress-corrosion cracking must be eliminated, accepting ~12 % lower strength.42048011140 HB39 % IACS
Overaged for exfoliation-corrosion resistance
Compromise temper: most of the T6 strength with much better exfoliation/SCC behaviour for thin plate and profiles.45551010150 HB37 % IACS
T6, stress relieved by stretching
Choose for thick plate that will be heavily machined — stretch stress-relief minimises distortion of mould and jig plates.4955409158 HB32 % IACS
T6511This page
T6, stress relieved by stretching, minor straightening
Standard low-residual-stress temper for 7012 extruded bar and profiles destined for precision machining.5055459160 HB32 % IACS
Solution heat treated and artificially aged
Standard stock condition — maximum strength for structural extrusions, plate and machined parts in dry/protected service.5105509160 HB32 % IACS

What is 7012-T6511?

7012-T6511 is 7012 in the T6511 temper — standard low-residual-stress temper for 7012 extruded bar and profiles destined for precision machining. 7012-T6511 has a yield strength of 505 MPa (73.2 ksi) and a tensile strength of 545 MPa (79 ksi) — stronger than 96% of aluminum grades. Elongation at break is 9% and the elastic modulus is 71 GPa (10.3 Msi). 7012-T6511 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 — 505 MPa (73.2 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 91% 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-T6511 properties

Typical room-temperature values for 7012-T6511; 22 are specific to this condition. Other listed values are 7012 reference data and may not represent this condition. Bars are the position among aluminum grades.

Physical3

7012-T6511 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-T6511 has a yield strength of 505 MPa (73.2 ksi) and a tensile strength of 545 MPa (79 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)545 MPa79 ksi
Yield Strength (0.2% offset)505 MPa73.2 ksi
Elongation at Break9%
Compressive Strength518 MPa75.1 ksi
Shear Strength322 MPa46.7 ksi
Fatigue Strength (Endurance Limit)155 MPa22.5 ksi
Fracture Toughness (K_IC)28 MPa·√m25.5 ksi·√in
Hardness, Brinell160 HB
Hardness, Vickers170 HV

Thermal6

7012-T6511 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-T6511 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 91% 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-T6511 takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 76% 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-T6511's machinability is very good (75/100, better than 86% of aluminum grades); weldability poor (22/100); formability poor (20/100).

MachinabilityVery good75/100
Machinability Rating (AISI 1212 = 100 %)90%
WeldabilityPoor22/100
Formability (cold)Poor20/100
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 6000 series.

Values are nominal handbook figures for design screening. Confirm any required mill or lot documentation when quoting.

Working with 7012-T6511

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-T6511 — frequently asked

What is 7012-T6511 used for?

7012-T6511 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-T6511?

7012-T6511 has a typical yield strength of 505 MPa (73.2 ksi) and a tensile strength of 545 MPa (79 ksi) — stronger than 96% of aluminum grades. Strength varies by condition: see the 6 listed tempers.

Is 7012-T6511 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-T6511 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-T6511?

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-T6511 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-T6511?

7012-T6511 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-T6511?

Yes — 7012-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

  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 composition — CEN (2019)
  3. EN 755-2 Aluminium alloy extruded rod/bar, tube and profiles — Mechanical properties — CEN (2016)
  4. ASM Handbook Vol. 2: Properties and Selection — Nonferrous Alloys — ASM International (1990)
  5. ASM Handbook Vol. 13B: Corrosion — Materials (aluminium alloys) — ASM International (2005)
  6. High-strength 7000-series 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.