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Aluminum 2025-F (As fabricated)

Temper

AA 2025 · UNS A92025

As-forged stock with no controlled thermal treatment — bought for subsequent solution treating and aging.

Premium cost $$$

Values for the F condition

Other 2025 tempers and conditions

2025 is listed in 4 conditions; see the grade overview at 2025.

Compare all 4 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Softest condition for maximum workability, straightening or re-forging before heat treatment.952052455 HB47 % IACS
FThis page
As fabricated
As-forged stock with no controlled thermal treatment — bought for subsequent solution treating and aging.1402602070 HB45 % IACS
Solution heat treated and naturally aged
Intermediate temper used when forgings must be straightened, coined or machined before final artificial aging.21537022100 HB34 % IACS
T6Default
Solution heat treated and artificially aged
Standard delivery condition for 2025 forgings — full strength for propeller blades and structural forgings.25540019110 HB40 % IACS

What is 2025-F?

2025-F is 2025 in the F temper — as-forged stock with no controlled thermal treatment — bought for subsequent solution treating and aging. 2025-F has a yield strength of 140 MPa (20.3 ksi) and a tensile strength of 260 MPa (37.7 ksi) — weaker than 70% of aluminum grades. Elongation at break is 20% and the elastic modulus is 72 GPa (10.4 Msi). 2025-F has a density of 2.81 g/cm³ (0.102 lb/in³), heavier than 86% of aluminum grades. It melts at 520°C (968 °F). T6 is the default condition FabDigit quotes; F is available on request or by drawing note.

Advantages

  • Ductile — tolerates forming and impact — 20%, better than 89% of aluminum grades
  • High electrical conductivity — 45 % IACS, better than 86% of aluminum grades
  • Conducts heat well — 170 W/m·K (98.2 BTU/hr·ft·°F), better than 82% of aluminum grades

Limitations

  • Needs corrosion protection — 32/100, worse than 94% of aluminum grades

2025-F properties

Typical room-temperature values for 2025-F; 21 are specific to this condition. Other listed values are 2025 reference data and may not represent this condition. Bars are the position among aluminum grades.

Physical3

2025-F has a density of 2.81 g/cm³ (0.102 lb/in³), heavier than 86% of aluminum grades. It melts at 520°C (968 °F).

Density2.81 g/cm³0.1 lb/in³
Melting Point (Solidus)520°C968 °F
Liquidus Temperature640°C1,184 °F

Mechanical11

2025-F has a yield strength of 140 MPa (20.3 ksi) and a tensile strength of 260 MPa (37.7 ksi) — weaker than 70% of aluminum grades. Elongation at break is 20% and the elastic modulus is 72 GPa (10.4 Msi).

Elastic (Young's) Modulus72 GPa10.4 Msi
Shear Modulus27 GPa3.9 Msi
Bulk Modulus75 GPa10.9 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)260 MPa37.7 ksi
Yield Strength (0.2% offset)140 MPa20.3 ksi
Elongation at Break20%
Shear Strength165 MPa23.9 ksi
Fatigue Strength (Endurance Limit)90 MPa13.1 ksi
Hardness, Brinell70 HB
Hardness, Vickers74 HV

Thermal6

2025-F is rated for continuous service to 150°C (302 °F). It conducts heat at 170 W/m·K (98.2 BTU/hr·ft·°F), better than 82% of aluminum grades. Thermal expansion is 22.7 µm/m·K (12.6 µin/in·°F).

Thermal Conductivity170 W/m·K98.2 BTU/hr·ft·°F
Specific Heat Capacity875 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)150°C302 °F
Min Service Temperature-196°C-321 °F

Electrical3

2025-F conducts electricity at 45 % IACS, better than 86% of aluminum grades.

Electrical Conductivity45 % IACS
Electrical Resistivity3.8×10⁻⁸ Ω·m1.5 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

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

Galvanic Potential (seawater, vs SCE)-0.64 V
Corrosion ResistancePoor32/100
Chemical Resistance SummaryGood in dry air, oils and most organic solvents; attacked by chlorides, seawater spray, strong acids and alkalis; copper content promotes pitting and galvanic attack against steel/stainless fasteners — protect by anodize, cladding or primer.

Sustainability4

Producing a kilogram of 2025-F takes about 205 MJ of energy and emits 12.5 kg of CO₂ — more than 76% of aluminum grades. Typical recycled content is 10%.

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 Content10%

Manufacturability7

2025-F's machinability is fair (45/100, worse than 72% of aluminum grades); weldability poor (30/100); formability good (55/100).

MachinabilityFair45/100
Machinability Rating (AISI 1212 = 100 %)105%
WeldabilityPoor30/100
Formability (cold)Good55/100
Brazeability / SolderabilityPoor20/100
PolishabilityGood60/100
Anodizing Responsefair — protective/hardcoat anodizing works, but Cu and Si content gives a dull yellow-grey film and reduced coating corrosion protection; chromate or sulfuric anodize plus primer is typical for aerospace parts.

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

Working with 2025-F

Is 2025 easy to machine?

Machines cleanly in T6 with sharp carbide tooling, high speeds and flood coolant; annealed/F material is gummy and needs positive-rake tools.

Can 2025 be welded?

Not recommended for arc welding (hot-cracking, loss of T6 properties) — join by riveting or bolting; resistance spot welding possible with qualified schedules.

Can 2025 be formed, bent or molded?

Excellent hot forgeability at roughly 420–460 °C, which is the alloy's reason for existence; cold forming should be done in O or T4 and followed by heat treatment.

What surface finishes work on 2025?

Anodize or chromate-convert plus prime for corrosion protection; shot peening improves fatigue life of forged blade sections.

2025 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 limit≤ 1—
Cuprincipal strengthening element3.9 – 54.5
Mn0.4 – 1.20.8
Mg≤ 0.05—
Cr≤ 0.1—
Zn≤ 0.25—
Others (each)≤ 0.05—
Others (total)≤ 0.15—
Albalance—

2025-F — frequently asked

What is 2025-F used for?

2025-F is typically used for propeller blades, forged aircraft components, forged airframe fittings, rotating forged blade sections, legacy aero-engine accessory forgings and machined-from-forging structural parts. In short: easy-forging 2000-series alloy; propeller-blade legacy grade; moderate strength, good ductility.

What is the yield strength of 2025-F?

2025-F has a typical yield strength of 140 MPa (20.3 ksi) and a tensile strength of 260 MPa (37.7 ksi) — weaker than 70% of aluminum grades. Strength varies by condition: see the 4 listed tempers.

Is 2025-F easy to machine?

Reasonably — machinability is rated fair (45/100, worse than 72% of aluminum grades). Machines cleanly in T6 with sharp carbide tooling, high speeds and flood coolant; annealed/F material is gummy and needs positive-rake tools.

Can 2025-F be welded?

Not readily — weldability is rated poor (30/100). Not recommended for arc welding (hot-cracking, loss of T6 properties) — join by riveting or bolting; resistance spot welding possible with qualified schedules.

What surface finishes work on 2025-F?

Anodize or chromate-convert plus prime for corrosion protection; shot peening improves fatigue life of forged blade sections.

Can 2025-F be formed, bent or molded?

Excellent hot forgeability at roughly 420–460 °C, which is the alloy's reason for existence; cold forming should be done in O or T4 and followed by heat treatment.

What is the maximum service temperature of 2025-F?

2025-F 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.

What is the difference between 2025-T6 and 2025-O?

T6 is the default condition — standard delivery condition for 2025 forgings — full strength for propeller blades and structural forgings. O: softest condition for maximum workability, straightening or re-forging before heat treatment. Yield strength is 255 MPa in T6 versus 95 MPa in O.

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 Materials — ASM International (1990)
  3. Aluminum Standards and Data — The Aluminum Association (2017)
  4. Properties and Physical Metallurgy of Aluminum Alloys (J.E. Hatch, ed.) — ASM International (1984)

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.