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Aluminum 7175 · precip hard

Aluminum 7175-T66

Properties of the T66 condition, compared with the other 7175 tempers.

Highest-strength registered temper for 7175 die forgings when maximum static strength is needed.

CNC machiningSheet metalPremium cost $$$

What is 7175-T66?

7175-T66 is 7175 in the T66 condition — highest-strength registered temper for 7175 die forgings when maximum static strength is needed. 7175-T66 has a yield strength of 560 MPa (81.2 ksi) and a tensile strength of 620 MPa (89.9 ksi) — stronger than 98% of aluminum grades. Elongation at break is 9% and the elastic modulus is 71.7 GPa (10.4 Msi). 7175-T66 has a density of 2.8 g/cm³ (0.101 lb/in³), heavier than 81% of aluminum grades. It melts at 477°C (891 °F).

Advantages

  • High strength — 560 MPa (81.2 ksi), better than 98% of aluminum grades
  • Easy to machine — 78/100, better than 89% of aluminum grades

Limitations

  • Difficult to weld — 12/100, worse than 98% of aluminum grades
  • Needs corrosion protection — 32/100, worse than 94% of aluminum grades
  • Limited service temperature — 120°C (248 °F), worse than 79% of aluminum grades

7175-T66 properties

Typical room-temperature values for 7175-T66 — 9 properties are specific to this condition; the rest are grade-level values shared by every 7175 temper. Each bar shows where the value sits among the aluminum grades in FabDigit's library — further right is higher.

Physical3

7175-T66 has a density of 2.8 g/cm³ (0.101 lb/in³), heavier than 81% of aluminum grades. It melts at 477°C (891 °F).

Density2.8 g/cm³0.1 lb/in³
Melting Point (Solidus)477°C891 °F
Liquidus Temperature635°C1,175 °F

Mechanical14

7175-T66 has a yield strength of 560 MPa (81.2 ksi) and a tensile strength of 620 MPa (89.9 ksi) — stronger than 98% of aluminum grades. Elongation at break is 9% and the elastic modulus is 71.7 GPa (10.4 Msi).

Elastic (Young's) Modulus71.7 GPa10.4 Msi
Shear Modulus26.9 GPa3.9 Msi
Bulk Modulus70 GPa10.2 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)620 MPa89.9 ksi
Yield Strength (0.2% offset)560 MPa81.2 ksi
Elongation at Break9%
Reduction in Area25%
Compressive Strength470 MPa68.2 ksi
Shear Strength340 MPa49.3 ksi
Fatigue Strength (Endurance Limit)150 MPa21.8 ksi
Fracture Toughness (K_IC)26 MPa·√m23.7 ksi·√in
Hardness, Brinell160 HB
Hardness, Vickers148 HV

Thermal6

7175-T66 is rated for continuous service to 120°C (248 °F). It conducts heat at 155 W/m·K (89.6 BTU/hr·ft·°F), better than 71% of aluminum grades. Thermal expansion is 23.4 µm/m·K (13 µin/in·°F).

Thermal Conductivity155 W/m·K89.6 BTU/hr·ft·°F
Specific Heat Capacity960 J/kg·K0.23 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)23.4 µm/m·K13 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

7175-T66 conducts electricity at 32 % IACS, worse than 63% of aluminum grades.

Electrical Conductivity32 % 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)-0.8 V
Corrosion ResistancePoor32/100
Chemical Resistance SummaryGood in dry atmospheres and neutral organics; attacked by strong acids/alkalis, chlorides and mercury salts; T6 tempers are SCC-sensitive in the short-transverse direction, so T73/T74 overaged tempers are specified for exposed aerospace parts.

Sustainability4

Producing a kilogram of 7175-T66 takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 75% of aluminum grades. Typical recycled content is 8%.

Embodied Energy (primary production)205 MJ/kg88,134 BTU/lb
Embodied Carbon (primary production)12.5 kg CO₂/kg
Embodied Water1,200 L/kg144 gal/lb
Typical Recycled Content8%

Manufacturability7

7175-T66's machinability is very good (78/100, better than 89% of aluminum grades); weldability not recommended (12/100); formability poor (25/100).

MachinabilityVery good78/100
Machinability Rating (AISI 1212 = 100 %)90%
WeldabilityNot recommended12/100
Formability (cold)Poor25/100
Brazeability / SolderabilityNot recommended8/100
PolishabilityGood60/100
Anodizing Responsegood — chromic/sulfuric and Type III hardcoat all work; clear coatings take a grey-tan tint from Zn/Cu, so dyed or hardcoat finishes are preferred

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

Other 7175 tempers and conditions

7175 is also supplied in 12 other conditions. The full side-by-side table is on the 7175 overview.

Working with 7175-T66

Is 7175 easy to machine?

Machines very well in T7x tempers with sharp polished carbide, high speed and flood coolant; expect long chips and use chip-breaking geometry.

Can 7175 be welded?

Not arc weldable for structure (hot-cracking, SCC in HAZ); join by riveting, bolting, adhesive bonding or friction stir welding with process qualification.

Can 7175 be formed, bent or molded?

Forge/hot work at ~380–440 °C; cold forming in T-tempers is very limited — form in O or W temper and re-heat-treat.

What surface finishes work on 7175?

Chromic/sulfuric anodize, Type III hardcoat, chemical conversion coating (Alodine) plus primer; avoid caustic etch overexposure on close-tolerance machined parts.

7175 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
Zn5.1 – 6.15.6
Mg2.1 – 2.92.5
Cu1.2 – 21.6
Crgrain-structure control0.18 – 0.280.23
Ferestricted vs 7075 for toughness≤ 0.20.12
Sirestricted vs 7075≤ 0.150.08
Mn≤ 0.10.03
Ti≤ 0.10.03
Others (each)≤ 0.05
Others (total)≤ 0.15
Albalance

7175-T66 — frequently asked

What is 7175-T66 used for?

7175-T66 is typically used for aircraft structural fittings, helicopter rotor hubs, fuselage frames and bulkheads, landing gear components, wing and spar forgings and highly loaded machined brackets. In short: premium aerospace forging.

What is the yield strength of 7175-T66?

7175-T66 has a typical yield strength of 560 MPa (81.2 ksi) and a tensile strength of 620 MPa (89.9 ksi) — stronger than 98% of aluminum grades. Strength varies by condition: see the 13 listed tempers.

Is 7175-T66 easy to machine?

Yes — machinability is rated very good (78/100, better than 89% of aluminum grades). Machines very well in T7x tempers with sharp polished carbide, high speed and flood coolant; expect long chips and use chip-breaking geometry.

Can 7175-T66 be welded?

Not readily — weldability is rated not recommended (12/100). Not arc weldable for structure (hot-cracking, SCC in HAZ); join by riveting, bolting, adhesive bonding or friction stir welding with process qualification.

What surface finishes work on 7175-T66?

Chromic/sulfuric anodize, Type III hardcoat, chemical conversion coating (Alodine) plus primer; avoid caustic etch overexposure on close-tolerance machined parts.

Can 7175-T66 be formed, bent or molded?

Forge/hot work at ~380–440 °C; cold forming in T-tempers is very limited — form in O or W temper and re-heat-treat.

What is the maximum service temperature of 7175-T66?

7175-T66 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 7175-T66?

Yes — 7175-T66 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. AMS 4149 — Aluminum Alloy 7175 Die Forgings and Rolled Rings, T74SAE International (2018)
  3. ASTM B247 — Aluminum-Alloy Die, Hand and Rolled Ring ForgingsASTM International (2020)
  4. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous AlloysASM International (1990)
  5. MMPDS — Metallic Materials Properties Development and StandardizationBattelle/FAA (2019)
  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.