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Aluminum 2618 · temper

Aluminum 2618-O

Properties of the O condition, compared with the other 2618 tempers.

Choose for deep forming, straightening or heavy machining before solution treating and ageing.

CNC machiningSheet metalPremium cost $$$

What is 2618-O?

2618-O is 2618 in the O temper — choose for deep forming, straightening or heavy machining before solution treating and ageing. 2618-O has a yield strength of 125 MPa (18.1 ksi) and a tensile strength of 215 MPa (31.2 ksi) — weaker than 75% of aluminum grades. Elongation at break is 18% and the elastic modulus is 74.5 GPa (10.8 Msi). 2618-O has a density of 2.76 g/cm³ (0.0997 lb/in³), heavier than 69% of aluminum grades. It melts at 549°C (1,020 °F).

Advantages

  • Ductile — tolerates forming and impact — 18%, better than 86% of aluminum grades
  • Forms and bends easily — 70/100, better than 83% of aluminum grades
  • High electrical conductivity — 41 % IACS, better than 78% of aluminum grades
  • Conducts heat well — 160 W/m·K (92.4 BTU/hr·ft·°F), better than 75% of aluminum grades

Limitations

  • Needs corrosion protection — 32/100, worse than 94% of aluminum grades
  • Difficult to weld — 22/100, worse than 83% of aluminum grades
  • Difficult to machine — 40/100, worse than 80% of aluminum grades
  • Low strength — 125 MPa (18.1 ksi), worse than 75% of aluminum grades

2618-O properties

Typical room-temperature values for 2618-O — 11 properties are specific to this condition; the rest are grade-level values shared by every 2618 temper. Each bar shows where the value sits among the aluminum grades in FabDigit's library — further right is higher.

Physical3

2618-O has a density of 2.76 g/cm³ (0.0997 lb/in³), heavier than 69% of aluminum grades. It melts at 549°C (1,020 °F).

Density2.76 g/cm³0.1 lb/in³
Melting Point (Solidus)549°C1,020 °F
Liquidus Temperature638°C1,180 °F

Mechanical15

2618-O has a yield strength of 125 MPa (18.1 ksi) and a tensile strength of 215 MPa (31.2 ksi) — weaker than 75% of aluminum grades. Elongation at break is 18% and the elastic modulus is 74.5 GPa (10.8 Msi).

Elastic (Young's) Modulus74.5 GPa10.8 Msi
Shear Modulus28 GPa4.1 Msi
Bulk Modulus76 GPa11 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)215 MPa31.2 ksi
Yield Strength (0.2% offset)125 MPa18.1 ksi
Elongation at Break18%
Reduction in Area20%
Compressive Strength380 MPa55.1 ksi
Shear Strength145 MPa21 ksi
Fatigue Strength (Endurance Limit)90 MPa13.1 ksi
Fracture Toughness (K_IC)28 MPa·√m25.5 ksi·√in
Hardness, Brinell65 HB
Hardness, Rockwell B70 HRB
Hardness, Vickers125 HV

Thermal6

2618-O is rated for continuous service to 150°C (302 °F). It conducts heat at 160 W/m·K (92.4 BTU/hr·ft·°F), better than 75% 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 Fusion389 J/g167 BTU/lb
Max Service Temperature (continuous)150°C302 °F
Min Service Temperature-196°C-321 °F

Electrical3

2618-O conducts electricity at 41 % IACS, better than 78% of aluminum grades.

Electrical Conductivity41 % IACS
Electrical Resistivity4.66×10⁻⁸ Ω·m1.83 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is poor (32/100), worse than 94% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.7 V
Corrosion ResistancePoor32/100
Chemical Resistance SummaryGood in dry air and neutral organics/oils; poor in chlorides, seawater and acids/alkalis due to Cu and Fe-Ni intermetallics driving galvanic pitting — protect by anodizing, cladding or paint; avoid direct contact with steel or carbon composites.

Sustainability4

Producing a kilogram of 2618-O takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 75% of aluminum grades. Typical recycled content is 5%.

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 Content5%

Manufacturability8

2618-O's machinability is fair (40/100, worse than 80% of aluminum grades); weldability poor (22/100); formability very good (70/100).

MachinabilityFair40/100
Machinability Rating (AISI 1212 = 100 %)150%
WeldabilityPoor22/100
Formability (cold)Very good70/100
CastabilityPoor20/100
Brazeability / SolderabilityPoor15/100
PolishabilityGood55/100
Anodizing Responsefair — Cu/Fe/Ni intermetallics give grey, mottled and less protective films; hard-anodize (Type III) is used on pistons but expect dark, non-decorative colour

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

Other 2618 tempers and conditions

2618 is also supplied in 5 other conditions. The full side-by-side table is on the 2618 overview.

Working with 2618-O

Is 2618 easy to machine?

Machines cleanly in T6/T61 with sharp PCD or polished carbide, high speed and flood coolant; hard Fe-Ni intermetallics accelerate edge wear compared with 6061.

Can 2618 be welded?

Not recommended for fusion welding (hot cracking, loss of aged strength); join by mechanical fasteners, friction welding or FSW with post-weld ageing where qualified.

Can 2618 be formed, bent or molded?

Hot forge/extrude at 400–450 °C; cold forming only in O temper — T61 material is essentially non-formable and must be machined to shape.

What surface finishes work on 2618?

Hard anodize (Type III) for piston crowns and wear faces gives a dark grey, non-uniform film; chromate/TCP conversion coat plus primer for corrosion protection, and avoid bare seawater exposure.

2618 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
Si0.1 – 0.250.18
Feforms Al9FeNi dispersoids for creep strength0.9 – 1.31.1
Cu1.9 – 2.72.3
Mg1.3 – 1.81.5
Ni0.9 – 1.21.05
Ti0.04 – 0.10.07
Zn≤ 0.1
Others (each)≤ 0.05
Others (total)≤ 0.15
Albalance

2618-O — frequently asked

What is 2618-O used for?

2618-O is typically used for forged engine pistons, turbocharger compressor wheels, cylinder heads, aero-engine accessory components, high-temperature structural forgings and supersonic aircraft skin panels. In short: concorde alloy; high-temp aerospace.

What is the yield strength of 2618-O?

2618-O has a typical yield strength of 125 MPa (18.1 ksi) and a tensile strength of 215 MPa (31.2 ksi) — weaker than 75% of aluminum grades. Strength varies by condition: see the 6 listed tempers.

Is 2618-O easy to machine?

Not especially — machinability is rated fair (40/100, worse than 80% of aluminum grades). Machines cleanly in T6/T61 with sharp PCD or polished carbide, high speed and flood coolant; hard Fe-Ni intermetallics accelerate edge wear compared with 6061.

Can 2618-O be welded?

Not readily — weldability is rated poor (22/100). Not recommended for fusion welding (hot cracking, loss of aged strength); join by mechanical fasteners, friction welding or FSW with post-weld ageing where qualified.

What surface finishes work on 2618-O?

Hard anodize (Type III) for piston crowns and wear faces gives a dark grey, non-uniform film; chromate/TCP conversion coat plus primer for corrosion protection, and avoid bare seawater exposure.

Can 2618-O be formed, bent or molded?

Hot forge/extrude at 400–450 °C; cold forming only in O temper — T61 material is essentially non-formable and must be machined to shape.

What is the maximum service temperature of 2618-O?

2618-O is rated for continuous use to about 150°C (302 °F). Strength falls off well before that limit — check the elevated-temperature data for load-bearing parts.

Can FabDigit make parts in 2618-O?

Yes — 2618-O 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. ASM Handbook Vol. 2 — Properties and Selection: Nonferrous Alloys and Special-Purpose MaterialsASM International (1990)
  3. MMPDS (Metallic Materials Properties Development and Standardization)FAA/Battelle (2023)
  4. AMS 4132 — Aluminum Alloy Forgings 2618, Solution and Precipitation Heat TreatedSAE International (2019)
  5. EN 573-3 / EN 586 — Aluminium and aluminium alloys, chemical composition and forgingsCEN (2019)

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.