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Aluminum 7475 · temper

Aluminum 7475-T6

Properties of the T6 condition, compared with the other 7475 tempers.

Pick for maximum static strength where SCC exposure is low and part is not stretch-relieved.

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What is 7475-T6?

7475-T6 is 7475 in the T6 temper — pick for maximum static strength where SCC exposure is low and part is not stretch-relieved. 7475-T6 has a yield strength of 496 MPa (71.9 ksi) and a tensile strength of 565 MPa (81.9 ksi) — stronger than 96% of aluminum grades. Elongation at break is 11% and the elastic modulus is 71 GPa (10.3 Msi). 7475-T6 has a density of 2.81 g/cm³ (0.102 lb/in³), heavier than 86% of aluminum grades. It melts at 477°C (891 °F).

Advantages

  • Tough — resists crack growth — 47 MPa·√m (42.8 ksi·√in), better than 100% of aluminum grades
  • High strength — 496 MPa (71.9 ksi), better than 96% of aluminum grades
  • Easy to machine — 75/100, better than 86% of aluminum grades
  • Polishes to a fine finish — 65/100, better than 82% of aluminum grades

Limitations

  • Difficult to weld — 18/100, worse than 94% of aluminum grades
  • Needs corrosion protection — 36/100, worse than 81% of aluminum grades
  • Limited service temperature — 120°C (248 °F), worse than 79% of aluminum grades

7475-T6 properties

Typical room-temperature values for 7475-T6 — 15 properties are specific to this condition; the rest are grade-level values shared by every 7475 temper. Each bar shows where the value sits among the aluminum grades in FabDigit's library — further right is higher.

Physical3

7475-T6 has a density of 2.81 g/cm³ (0.102 lb/in³), heavier than 86% of aluminum grades. It melts at 477°C (891 °F).

Density2.81 g/cm³0.1 lb/in³
Melting Point (Solidus)477°C891 °F
Liquidus Temperature635°C1,175 °F

Mechanical12

7475-T6 has a yield strength of 496 MPa (71.9 ksi) and a tensile strength of 565 MPa (81.9 ksi) — stronger than 96% of aluminum grades. Elongation at break is 11% 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)565 MPa81.9 ksi
Yield Strength (0.2% offset)496 MPa71.9 ksi
Elongation at Break11%
Compressive Strength500 MPa72.5 ksi
Shear Strength331 MPa48 ksi
Fatigue Strength (Endurance Limit)160 MPa23.2 ksi
Fracture Toughness (K_IC)47 MPa·√m42.8 ksi·√in
Hardness, Brinell148 HB

Thermal6

7475-T6 is rated for continuous service to 120°C (248 °F). It conducts heat at 142 W/m·K (82 BTU/hr·ft·°F), better than 51% of aluminum grades. Thermal expansion is 22.7 µm/m·K (12.6 µin/in·°F).

Thermal Conductivity142 W/m·K82 BTU/hr·ft·°F
Specific Heat Capacity864 J/kg·K0.21 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)22.7 µm/m·K12.6 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

7475-T6 conducts electricity at 33 % IACS, worse than 57% of aluminum grades.

Electrical Conductivity33 % IACS
Electrical Resistivity5.22×10⁻⁸ Ω·m2.06 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is fair (36/100), worse than 81% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.82 V
Corrosion ResistanceFair36/100
Chemical Resistance SummaryGood in neutral atmospheres and fresh water; overaged T73/T76 tempers resist stress-corrosion and exfoliation far better than T6. Attacked by strong acids and alkalis, and by chlorides in stagnant seawater; requires anodizing, cladding or primer in marine/aerospace service.

Sustainability4

Producing a kilogram of 7475-T6 takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 75% of aluminum grades. Typical recycled content is 12%.

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 Content12%

Manufacturability8

7475-T6's machinability is very good (75/100, better than 86% of aluminum grades); weldability poor (18/100); formability poor (22/100).

MachinabilityVery good75/100
Machinability Rating (AISI 1212 = 100 %)70%
WeldabilityPoor18/100
Formability (cold)Poor22/100
CastabilityPoor20/100
Brazeability / SolderabilityNot recommended10/100
PolishabilityGood65/100
Anodizing Responsegood — clear and hard (type III) anodize both work well; low Fe/Si content gives cleaner, more uniform films than 7075, though coating stays slightly grey-bronze

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

Other 7475 tempers and conditions

7475 is also supplied in 9 other conditions. The full side-by-side table is on the 7475 overview.

Working with 7475-T6

Is 7475 easy to machine?

Machines well in aged tempers with sharp polished-flute carbide, high speed and flood coolant; T7x plate distorts less than T651 thanks to stretch stress relief.

Can 7475 be welded?

Not fusion weldable in structure (hot cracking, SCC in HAZ) — join by riveting, adhesive bonding or friction-stir welding with post-weld temper control.

Can 7475 be formed, bent or molded?

Form in O or freshly quenched W temper then age; aged T6/T7x sheet needs generous bend radii (typically ≥4–6 t) and often warm forming.

What surface finishes work on 7475?

Responds well to chromate/anodic pretreatments; clear or hard anodize is standard, and aerospace parts are usually clad, chromated and primed for corrosion protection.

7475 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
Zn5.2 – 6.25.7
Mg1.9 – 2.62.25
Cu1.2 – 1.91.6
Crgrain-structure control0.18 – 0.250.21
Fetightly limited for toughness≤ 0.120.07
Sitightly limited for toughness≤ 0.10.06
Mn≤ 0.060.02
Ti≤ 0.060.03
Others (each)≤ 0.05
Others (total)≤ 0.15
Albalance

7475-T6 — frequently asked

What is 7475-T6 used for?

7475-T6 is typically used for wing skins, fuselage skins and stringers. In short: damage-tolerant aerospace plate.

What is the yield strength of 7475-T6?

7475-T6 has a typical yield strength of 496 MPa (71.9 ksi) and a tensile strength of 565 MPa (81.9 ksi) — stronger than 96% of aluminum grades. Strength varies by condition: see the 10 listed tempers.

Is 7475-T6 easy to machine?

Yes — machinability is rated very good (75/100, better than 86% of aluminum grades). Machines well in aged tempers with sharp polished-flute carbide, high speed and flood coolant; T7x plate distorts less than T651 thanks to stretch stress relief.

Can 7475-T6 be welded?

Not readily — weldability is rated poor (18/100). Not fusion weldable in structure (hot cracking, SCC in HAZ) — join by riveting, adhesive bonding or friction-stir welding with post-weld temper control.

What surface finishes work on 7475-T6?

Responds well to chromate/anodic pretreatments; clear or hard anodize is standard, and aerospace parts are usually clad, chromated and primed for corrosion protection.

Can 7475-T6 be formed, bent or molded?

Form in O or freshly quenched W temper then age; aged T6/T7x sheet needs generous bend radii (typically ≥4–6 t) and often warm forming.

What is the maximum service temperature of 7475-T6?

7475-T6 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 7475-T6?

Yes — 7475-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. AMS 4202 / AMS 4084 — 7475 Aluminum Alloy Plate and SheetSAE International (2019)
  3. ASM Handbook Vol. 2: Properties and Selection — Nonferrous AlloysASM International (1990)
  4. ASM Handbook Vol. 19: Fatigue and FractureASM International (1996)
  5. MMPDS-Metallic Materials Properties Development and Standardization (7475 typical values)FAA/Battelle (2023)

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.