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Aluminum 2N01-T73

Temper

GB 2N01 · JIS A2N01

T73 = solution heat treated and overaged for stress-corrosion resistance

Rarely stocked overaged condition used when long-term thermal stability and better SCC/exfoliation resistance outweigh peak strength.

High cost $$$$

Values for the T73 condition

Other 2N01 tempers and conditions

2N01 is listed in 5 conditions; see the grade overview at 2N01.

Compare all 5 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Softest state for deep machining stock removal, cold sizing or re-forging before solution treatment.951852055 HB50 % IACS
Solution heat treated and naturally aged
Choose when some cold forming or straightening is still needed after heat treatment and maximum strength is not required.2053501695 HB33 % IACS
T73This page
Solution heat treated and overaged for stress-corrosion resistance
Rarely stocked overaged condition used when long-term thermal stability and better SCC/exfoliation resistance outweigh peak strength.26035513105 HB44 % IACS
T6Default
Solution heat treated and artificially aged
Standard delivered condition for 2N01 forgings and bar: peak strength plus retained strength at 150–200 °C.28040012115 HB40 % IACS
T6, stress relieved by compression
Hand/die forgings that must be heavily machined — residual stress is knocked down so parts stay dimensionally stable.29040511118 HB40 % IACS

What is 2N01-T73?

2N01-T73 is 2N01 in the T73 temper — rarely stocked overaged condition used when long-term thermal stability and better SCC/exfoliation resistance outweigh peak strength. 2N01-T73 has a yield strength of 260 MPa (37.7 ksi) and a tensile strength of 355 MPa (51.5 ksi) — stronger than 68% of aluminum grades. Elongation at break is 13% and the elastic modulus is 74 GPa (10.7 Msi). 2N01-T73 has a density of 2.82 g/cm³ (0.102 lb/in³), heavier than 89% of aluminum grades. It melts at 505°C (941 °F). T6 is the default condition FabDigit quotes; T73 is available on request or by drawing note.

Advantages

  • High service temperature — 220°C (428 °F), better than 95% of aluminum grades
  • High electrical conductivity — 44 % IACS, better than 85% of aluminum grades
  • Ductile — tolerates forming and impact — 13%, better than 79% of aluminum grades
  • Tough — resists crack growth — 30 MPa·√m (27.3 ksi·√in), better than 76% of aluminum grades
  • Conducts heat well — 160 W/m·K (92.4 BTU/hr·ft·°F), better than 76% of aluminum grades

Limitations

  • Difficult to weld — 22/100, worse than 83% of aluminum grades

2N01-T73 properties

Typical room-temperature values for 2N01-T73; 22 are specific to this condition. Other listed values are 2N01 reference data and may not represent this condition. Bars are the position among aluminum grades.

Physical3

2N01-T73 has a density of 2.82 g/cm³ (0.102 lb/in³), heavier than 89% of aluminum grades. It melts at 505°C (941 °F).

Density2.82 g/cm³0.1 lb/in³
Melting Point (Solidus)505°C941 °F
Liquidus Temperature635°C1,175 °F

Mechanical15

2N01-T73 has a yield strength of 260 MPa (37.7 ksi) and a tensile strength of 355 MPa (51.5 ksi) — stronger than 68% of aluminum grades. Elongation at break is 13% and the elastic modulus is 74 GPa (10.7 Msi).

Elastic (Young's) Modulus74 GPa10.7 Msi
Shear Modulus27.5 GPa4 Msi
Bulk Modulus76 GPa11 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)355 MPa51.5 ksi
Yield Strength (0.2% offset)260 MPa37.7 ksi
Elongation at Break13%
Reduction in Area28%
Compressive Strength265 MPa38.4 ksi
Shear Strength225 MPa32.6 ksi
Fatigue Strength (Endurance Limit)115 MPa16.7 ksi
Fracture Toughness (K_IC)30 MPa·√m27.3 ksi·√in
Charpy V-Notch Impact (RT)13 J9.6 ft·lbf
Hardness, Brinell105 HB
Hardness, Vickers113 HV

Thermal6

2N01-T73 is rated for continuous service to 220°C (428 °F). It conducts heat at 160 W/m·K (92.4 BTU/hr·ft·°F), better than 76% of aluminum grades. Thermal expansion is 22.3 µm/m·K (12.4 µin/in·°F).

Thermal Conductivity160 W/m·K92.4 BTU/hr·ft·°F
Specific Heat Capacity875 J/kg·K0.21 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)22.3 µm/m·K12.4 µin/in·°F
Latent Heat of Fusion390 J/g168 BTU/lb
Max Service Temperature (continuous)220°C428 °F
Min Service Temperature-196°C-321 °F

Electrical3

2N01-T73 conducts electricity at 44 % IACS, better than 85% of aluminum grades.

Electrical Conductivity44 % IACS
Electrical Resistivity3.9×10⁻⁸ Ω·m1.54 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is fair (42/100), worse than 69% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.69 V
Corrosion ResistanceFair42/100
Chemical Resistance SummaryResists dry atmospheres, oils, fuels and most organic solvents; attacked by chlorides, seawater spray, strong acids and all alkalis. Cu+Ni content makes it markedly less corrosion resistant than 5000/6000 series — clad, anodize or prime for service.

Sustainability4

Producing a kilogram of 2N01-T73 takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 76% 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

2N01-T73's machinability is very good (70/100, better than 72% of aluminum grades); weldability poor (22/100); formability fair (40/100).

MachinabilityVery good70/100
Machinability Rating (AISI 1212 = 100 %)58%
WeldabilityPoor22/100
Formability (cold)Fair40/100
CastabilityPoor25/100
Brazeability / SolderabilityPoor15/100
PolishabilityGood55/100
Anodizing Responsefair — sulfuric anodizing gives a grey/yellowish, somewhat non-uniform film because of Cu and Ni intermetallics; hard anodizing works for wear but colour matching is poor. Chromic anodize or chromate/organic coatings are common for corrosion protection.

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

Working with 2N01-T73

Is 2N01 easy to machine?

Machines well in T6 with sharp carbide tools, high speed and flood coolant; Ni/Fe intermetallics are abrasive so expect faster edge wear than 6061.

Can 2N01 be welded?

Not recommended for fusion welding (hot cracking, loss of T6 properties) — use riveting, bolting, friction stir or friction welding, and re-heat-treat where possible.

Can 2N01 be formed, bent or molded?

Excellent hot forging/upsetting at roughly 400–450 °C; cold forming only in O or T4 with generous bend radii, then solution treat and age.

What surface finishes work on 2N01?

Chromic or sulfuric anodize gives a dull grey film; for corrosion service use cladding, conversion coating plus primer, or hard anodize for wear surfaces.

2N01 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
Si0.5 – 1.20.8
Feimpurity/intentional Fe-Ni phase former≤ 10.6
Cumain strengthening element3.5 – 4.54
Mn≤ 0.20.1
Mg0.4 – 0.80.6
Nigives elevated-temperature stability1.7 – 2.32
Cr≤ 0.1—
Zn≤ 0.25—
Tigrain refiner≤ 0.2—
Others (each)≤ 0.05—
Others (total)≤ 0.15—
Albalance—

2N01-T73 — frequently asked

What is 2N01-T73 used for?

2N01-T73 is typically used for aircraft structural forgings, airframe fittings and brackets, elevated-temperature forged components to 200 °C, machined structural parts from forged bar, engine-adjacent forged hardware and JIS-specified aerospace replacement parts. In short: JIS aerospace forging alloy; 200 °C service capability; 2017/2024 strength class.

What is the yield strength of 2N01-T73?

2N01-T73 has a typical yield strength of 260 MPa (37.7 ksi) and a tensile strength of 355 MPa (51.5 ksi) — stronger than 68% of aluminum grades. Strength varies by condition: see the 5 listed tempers.

Is 2N01-T73 easy to machine?

Yes — machinability is rated very good (70/100, better than 72% of aluminum grades). Machines well in T6 with sharp carbide tools, high speed and flood coolant; Ni/Fe intermetallics are abrasive so expect faster edge wear than 6061.

Can 2N01-T73 be welded?

Not readily — weldability is rated poor (22/100). Not recommended for fusion welding (hot cracking, loss of T6 properties) — use riveting, bolting, friction stir or friction welding, and re-heat-treat where possible.

What surface finishes work on 2N01-T73?

Chromic or sulfuric anodize gives a dull grey film; for corrosion service use cladding, conversion coating plus primer, or hard anodize for wear surfaces.

Can 2N01-T73 be formed, bent or molded?

Excellent hot forging/upsetting at roughly 400–450 °C; cold forming only in O or T4 with generous bend radii, then solution treat and age.

What is the maximum service temperature of 2N01-T73?

2N01-T73 is rated for continuous use to about 220°C (428 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

What is the difference between 2N01-T6 and 2N01-O?

T6 is the default condition — standard delivered condition for 2N01 forgings and bar: peak strength plus retained strength at 150–200 °C. O: softest state for deep machining stock removal, cold sizing or re-forging before solution treatment. Yield strength is 280 MPa in T6 versus 95 MPa in O.

Sources

  1. JIS H 4140 Aluminium and aluminium alloy forgings — JSA (2020)
  2. JIS H 4040 Aluminium and aluminium alloy rods, bars and wires — JSA (2015)
  3. ASM Handbook Vol.2 — Properties and Selection: Nonferrous Alloys — ASM International (1990)
  4. ASM Handbook Vol.13B — Corrosion: Materials — ASM International (2005)
  5. Aluminum Association Teal Sheets — International Alloy Designations — The Aluminum Association (2018)

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.