FabDigit

Aluminum 7178-T62

Temper

AA 7178 · UNS A97178 · EN AW-7178, AW 7178

T62 = t6, heat treated by the user

7178 re-solution-treated from O/F temper and artificially aged by the fabricator; strength essentially equals T6 with no stretch stress relief.

CNC machiningSheet metalPremium cost $$$

Values for the T62 condition

Other 7178 tempers and conditions

7178 is listed in 8 conditions; see the grade overview at 7178.

Compare all 8 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Soft annealed stock for severe forming or machining before solution heat treatment and aging.1032281560 HB38 % IACS
Overaged for exfoliation-corrosion resistance
Choose when exfoliation-corrosion resistance matters more than the last 5 % of strength.50557011150 HB38 % IACS
T76, stress relieved by stretching
Over-aged plate with low residual stress — for machined skins needing exfoliation resistance and dimensional stability.51057210150 HB38 % IACS
T62This page
T6, heat treated by the user
7178 re-solution-treated from O/F temper and artificially aged by the fabricator; strength essentially equals T6 with no stretch stress relief.53060010160 HB31 % IACS
T6, stress relieved by stretching
Standard plate temper — same peak strength as T6 but low residual stress for stable machining of thick parts.5306009160 HB31 % IACS
Solution heat treated and artificially aged
Peak-strength condition — pick it for maximum static and compressive strength in sheet, clad sheet and simple sections.53860710160 HB31 % IACS
Solution treated, stretched, aged; extrusion without straightening…
Extruded stringer/section temper with controlled stretch and no subsequent straightening.5706208165 HB31 % IACS
T6, stress relieved by stretching, minor straightening
Most common high-strength extrusion temper — straightness-corrected version of T6510.5706208165 HB31 % IACS

What is 7178-T62?

7178-T62 is 7178 in the T62 temper — 7178 re-solution-treated from O/F temper and artificially aged by the fabricator; strength essentially equals T6 with no stretch stress relief. 7178-T62 has a yield strength of 530 MPa (76.9 ksi) and a tensile strength of 600 MPa (87 ksi) — stronger than 97% of aluminum grades. Elongation at break is 10% and the elastic modulus is 71.7 GPa (10.4 Msi). 7178-T62 has a density of 2.83 g/cm³ (0.102 lb/in³), heavier than 91% of aluminum grades. It melts at 477°C (891 °F).

Advantages

  • High strength — 530 MPa (76.9 ksi), better than 97% of aluminum grades

Limitations

  • Difficult to weld — 15/100, worse than 96% of aluminum grades
  • Limited service temperature — 120°C (248 °F), worse than 79% of aluminum grades
  • Needs corrosion protection — 38/100, worse than 79% of aluminum grades

7178-T62 properties

Typical room-temperature values for 7178-T62; 34 are specific to this condition. Other listed values are 7178 reference data and may not represent this condition. Bars are the position among aluminum grades.

Physical3

7178-T62 has a density of 2.83 g/cm³ (0.102 lb/in³), heavier than 91% of aluminum grades. It melts at 477°C (891 °F).

Density2.83 g/cm³0.1 lb/in³
Melting Point (Solidus)477°C891 °F
Liquidus Temperature629°C1,164 °F

Mechanical13

7178-T62 has a yield strength of 530 MPa (76.9 ksi) and a tensile strength of 600 MPa (87 ksi) — stronger than 97% of aluminum grades. Elongation at break is 10% 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)600 MPa87 ksi
Yield Strength (0.2% offset)530 MPa76.9 ksi
Elongation at Break10%
Compressive Strength545 MPa79 ksi
Shear Strength355 MPa51.5 ksi
Fatigue Strength (Endurance Limit)150 MPa21.8 ksi
Fracture Toughness (K_IC)23 MPa·√m20.9 ksi·√in
Hardness, Brinell160 HB
Hardness, Vickers175 HV

Thermal6

7178-T62 is rated for continuous service to 120°C (248 °F). It conducts heat at 125 W/m·K (72.2 BTU/hr·ft·°F), worse than 72% of aluminum grades. Thermal expansion is 23.4 µm/m·K (13 µin/in·°F).

Thermal Conductivity125 W/m·K72.2 BTU/hr·ft·°F
Specific Heat Capacity860 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

7178-T62 conducts electricity at 31 % IACS, worse than 68% of aluminum grades.

Electrical Conductivity31 % IACS
Electrical Resistivity5.6×10⁻⁸ Ω·m2.2 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is fair (38/100), worse than 79% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.83 V
Corrosion ResistanceFair38/100
Chemical Resistance SummaryGood in neutral atmospheres and dry environments; poor in chloride-bearing or marine service — sustained short-transverse tensile stress in T6 risks stress-corrosion cracking; attacked by strong acids and alkalis; clad or anodize plus prime for aerospace use.

Sustainability4

Producing a kilogram of 7178-T62 takes about 200 MJ of energy and emits 12.5 kg of CO₂ — less than 60% of aluminum grades. Typical recycled content is 25%.

Embodied Energy (primary production)200 MJ/kg85,985 BTU/lb
Embodied Carbon (primary production)12.5 kg CO₂/kg
Embodied Water1,150 L/kg138 gal/lb
Typical Recycled Content25%

Manufacturability7

7178-T62's machinability is very good (70/100, better than 72% of aluminum grades); weldability poor (15/100); formability poor (22/100).

MachinabilityVery good70/100
Machinability Rating (AISI 1212 = 100 %)70%
WeldabilityPoor15/100
Formability (cold)Poor22/100
Brazeability / SolderabilityNot recommended10/100
PolishabilityGood60/100
Anodizing Responsegood — clear/sulfuric and hard-coat anodizing work well; high Zn/Cu gives a slightly grey-bronze tint and lower clarity than 6061; chromic/sulfuric anodize widely used on aerospace parts

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

Working with 7178-T62

Is 7178 easy to machine?

Machines well in T6/T76 with sharp carbide, high speed and flood coolant; relieve stresses (T651/T7651) before heavy pocket milling to control distortion.

Can 7178 be welded?

Not fusion weldable — hot cracking and severe HAZ SCC; join by riveting, bolting or adhesive bonding (friction-stir only with qualified procedures).

Can 7178 be formed, bent or molded?

Form in O or freshly quenched W temper and age afterwards; T6 sheet tolerates only large-radius bends and is prone to cracking.

What surface finishes work on 7178?

Clad or anodize (chromic/sulfuric) plus chromate conversion and primer for corrosion protection; avoid sustained short-transverse tensile stress and use T76 tempers in exfoliation-prone areas.

7178 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
Si≤ 0.4
Fe≤ 0.5
Cu1.6 – 2.42
Mn≤ 0.3
Mg2.4 – 3.12.7
Cr0.18 – 0.280.23
Zn6.3 – 7.36.8
Ti≤ 0.2
Others (each)each≤ 0.05
Others (total)total≤ 0.15
Albalance

7178-T62 — frequently asked

What is 7178-T62 used for?

7178-T62 is typically used for aircraft upper wing skins, wing stringers, compression-loaded airframe panels, extruded stiffeners and spar caps, alclad aerospace sheet components and legacy airframe replacement parts. In short: compression aerospace alloy.

What is the yield strength of 7178-T62?

7178-T62 has a typical yield strength of 530 MPa (76.9 ksi) and a tensile strength of 600 MPa (87 ksi) — stronger than 97% of aluminum grades. Strength varies by condition: see the 8 listed tempers.

Is 7178-T62 easy to machine?

Yes — machinability is rated very good (70/100, better than 72% of aluminum grades). Machines well in T6/T76 with sharp carbide, high speed and flood coolant; relieve stresses (T651/T7651) before heavy pocket milling to control distortion.

Can 7178-T62 be welded?

Not readily — weldability is rated poor (15/100). Not fusion weldable — hot cracking and severe HAZ SCC; join by riveting, bolting or adhesive bonding (friction-stir only with qualified procedures).

What surface finishes work on 7178-T62?

Clad or anodize (chromic/sulfuric) plus chromate conversion and primer for corrosion protection; avoid sustained short-transverse tensile stress and use T76 tempers in exfoliation-prone areas.

Can 7178-T62 be formed, bent or molded?

Form in O or freshly quenched W temper and age afterwards; T6 sheet tolerates only large-radius bends and is prone to cracking.

What is the maximum service temperature of 7178-T62?

7178-T62 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 7178-T62?

Yes — 7178-T62 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. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys — ASM International (1990)
  3. MMPDS-17 Metallic Materials Properties Development and Standardization — Battelle/FAA (2022)
  4. ASTM B209 / B221 — Aluminum Sheet, Plate and Extruded Products — ASTM International (2021)
  5. ASM Handbook Vol. 13B — Corrosion: Materials — ASM 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.