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Aluminum 7076-T61

Temper · default condition

AA 7076 · UNS A97076

T61 = t6 variant, underaged

The historically standard supply condition for 7076 forgings and propeller blades — full strength with slightly improved toughness/consistency over plain T6.

High cost $$$$

Values for the T61 condition

Other 7076 tempers and conditions

7076 is listed in 4 conditions; see the grade overview at 7076.

Compare all 4 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Choose for severe cold forming or straightening before solution treating and ageing to T6/T61.1052301760 HB40 % IACS
As fabricated
Mill/forge delivery condition for stock that will be solution treated and aged by the customer.1803001285 HB40 % IACS
Solution heat treated and artificially aged
Standard peak-strength condition for extrusions and machined parts where SCC exposure is limited.43550011140 HB32 % IACS
T61DefaultThis page
T6 variant, underaged
The historically standard supply condition for 7076 forgings and propeller blades — full strength with slightly improved toughness/consistency over plain T6.44851012142 HB33 % IACS

What is 7076-T61?

7076-T61 is 7076 in the T61 temper — the historically standard supply condition for 7076 forgings and propeller blades — full strength with slightly improved toughness/consistency over plain T6. 7076-T61 has a yield strength of 448 MPa (65 ksi) and a tensile strength of 510 MPa (74 ksi) — stronger than 91% of aluminum grades. Elongation at break is 12% and the elastic modulus is 71 GPa (10.3 Msi). 7076-T61 has a density of 2.8 g/cm³ (0.101 lb/in³), heavier than 81% of aluminum grades. It melts at 475°C (887 °F).

Advantages

  • High strength — 448 MPa (65 ksi), better than 91% of aluminum grades

Limitations

  • Difficult to weld — 20/100, worse than 89% of aluminum grades
  • Needs corrosion protection — 35/100, worse than 85% of aluminum grades
  • Limited service temperature — 120°C (248 °F), worse than 79% of aluminum grades

7076-T61 properties

Typical room-temperature values for 7076-T61; 13 are specific to this condition. Other listed values are 7076 reference data and may not represent this condition. Bars are the position among aluminum grades.

Physical3

7076-T61 has a density of 2.8 g/cm³ (0.101 lb/in³), heavier than 81% of aluminum grades. It melts at 475°C (887 °F).

Density2.8 g/cm³0.1 lb/in³
Melting Point (Solidus)475°C887 °F
Liquidus Temperature635°C1,175 °F

Mechanical12

7076-T61 has a yield strength of 448 MPa (65 ksi) and a tensile strength of 510 MPa (74 ksi) — stronger than 91% of aluminum grades. Elongation at break is 12% and the elastic modulus is 71 GPa (10.3 Msi).

Elastic (Young's) Modulus71 GPa10.3 Msi
Shear Modulus27 GPa3.9 Msi
Bulk Modulus70 GPa10.2 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)510 MPa74 ksi
Yield Strength (0.2% offset)448 MPa65 ksi
Elongation at Break12%
Compressive Strength455 MPa66 ksi
Shear Strength300 MPa43.5 ksi
Fatigue Strength (Endurance Limit)160 MPa23.2 ksi
Fracture Toughness (K_IC)26 MPa·√m23.7 ksi·√in
Hardness, Brinell142 HB

Thermal6

7076-T61 is rated for continuous service to 120°C (248 °F). It conducts heat at 150 W/m·K (86.7 BTU/hr·ft·°F), better than 58% of aluminum grades. Thermal expansion is 23.6 µm/m·K (13.1 µin/in·°F).

Thermal Conductivity150 W/m·K86.7 BTU/hr·ft·°F
Specific Heat Capacity960 J/kg·K0.23 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)23.6 µm/m·K13.1 µin/in·°F
Latent Heat of Fusion390 J/g168 BTU/lb
Max Service Temperature (continuous)120°C248 °F
Min Service Temperature-196°C-321 °F

Electrical3

7076-T61 conducts electricity at 33 % IACS, worse than 57% of aluminum grades.

Electrical Conductivity33 % IACS
Electrical Resistivity5.2×10⁻⁸ Ω·m2.05 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is fair (35/100), worse than 85% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.82 V
Corrosion ResistanceFair35/100
Chemical Resistance SummaryGood in neutral atmospheres and dry environments; poor in strong acids/alkalis and chloride-bearing media, where 7000-series-T6 is prone to pitting, exfoliation and stress-corrosion cracking — clad, anodize or paint for service exposure.

Sustainability4

Producing a kilogram of 7076-T61 takes about 200 MJ of energy and emits 12 kg of CO₂ — less than 60% of aluminum grades. Typical recycled content is 20%.

Embodied Energy (primary production)200 MJ/kg85,985 BTU/lb
Embodied Carbon (primary production)12 kg CO₂/kg
Embodied Water1,200 L/kg144 gal/lb
Typical Recycled Content20%

Manufacturability7

7076-T61's machinability is very good (70/100, better than 72% of aluminum grades); weldability poor (20/100); formability poor (25/100).

MachinabilityVery good70/100
Machinability Rating (AISI 1212 = 100 %)90%
WeldabilityPoor20/100
Formability (cold)Poor25/100
Brazeability / SolderabilityNot recommended10/100
PolishabilityGood60/100
Anodizing Responsegood — clear/hard anodize forms readily; coating is slightly grey-toned due to Zn/Cu content, so cosmetic bright anodizing is inferior to 5000/6000 series

Common Calculations5

Specific Strength (UTS / density)calculated182 kN·m/kg
Specific Stiffness (E / density)calculated25.4 MN·m/kg
Modulus of Resiliencecalculated1,413 kJ/m³
Thermal Diffusivitycalculated55.8 mm²/s
Thermal Shock Resistance Indexcalculated46

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

Working with 7076-T61

Is 7076 easy to machine?

Machines freely in T6/T61 with sharp carbide tooling, high speeds and generous coolant; produces clean chips but leaves high residual stress that can distort thin parts.

Can 7076 be welded?

Not recommended for arc welding (hot cracking and severe HAZ SCC due to Zn+Cu); join by riveting, bolting or friction-stir/adhesive methods.

Can 7076 be formed, bent or molded?

Hot forge/extrude at roughly 380–440 °C; do cold forming in the O or freshly quenched W temper, then age — T61 material has little cold formability.

What surface finishes work on 7076?

Takes clear and hard anodizing well (slightly grey tone), chromate/trivalent conversion coating and primer-paint systems; shot peening plus a protective coating is advisable where stress-corrosion exposure is possible.

7076 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≤ 0.4—
Feimpurity limit≤ 0.6—
Cu0.3 – 10.6
Mngrain-structure control in place of Cr0.3 – 0.80.55
Mg1.2 – 21.6
Znprincipal strengthening addition7 – 87.5
Tigrain refiner≤ 0.2—
Others (each)≤ 0.05—
Others (total)≤ 0.15—
Albalance—

7076-T61 — frequently asked

What is 7076-T61 used for?

7076-T61 is typically used for structural extrusions, legacy aerospace components, replacement forgings for older airframes, machined structural fittings, bolted frame and beam sections and repair and MRO spares. In short: legacy 7075 substitute; high-strength extrusion alloy; limited current availability.

What is the yield strength of 7076-T61?

7076-T61 has a typical yield strength of 448 MPa (65 ksi) and a tensile strength of 510 MPa (74 ksi) — stronger than 91% of aluminum grades. Strength varies by condition: see the 4 listed tempers.

Is 7076-T61 easy to machine?

Yes — machinability is rated very good (70/100, better than 72% of aluminum grades). Machines freely in T6/T61 with sharp carbide tooling, high speeds and generous coolant; produces clean chips but leaves high residual stress that can distort thin parts.

Can 7076-T61 be welded?

Not readily — weldability is rated poor (20/100). Not recommended for arc welding (hot cracking and severe HAZ SCC due to Zn+Cu); join by riveting, bolting or friction-stir/adhesive methods.

What surface finishes work on 7076-T61?

Takes clear and hard anodizing well (slightly grey tone), chromate/trivalent conversion coating and primer-paint systems; shot peening plus a protective coating is advisable where stress-corrosion exposure is possible.

Can 7076-T61 be formed, bent or molded?

Hot forge/extrude at roughly 380–440 °C; do cold forming in the O or freshly quenched W temper, then age — T61 material has little cold formability.

What is the maximum service temperature of 7076-T61?

7076-T61 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.

What is the difference between 7076-T61 and 7076-O?

T61 is the default condition — the historically standard supply condition for 7076 forgings and propeller blades — full strength with slightly improved toughness/consistency over plain T6. O: choose for severe cold forming or straightening before solution treating and ageing to T6/T61. Yield strength is 448 MPa in T61 versus 105 MPa in O.

Sources

  1. International Alloy Designations and Chemical Composition Limits for Wrought Aluminum (Teal Sheets) — The Aluminum Association (2018)
  2. ASM Handbook Vol.2 — Properties and Selection: Nonferrous Alloys and Special-Purpose Materials — ASM International (1990)
  3. ASM Handbook Vol.5 — Surface Engineering; Vol.6 — Welding, Brazing and Soldering; Vol.13 — Corrosion — ASM International (1994)
  4. MMPDS-style typical property tables for 7000-series wrought alloys — Battelle/FAA (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.