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Aluminum 2017A

AA 2017A · EN AlCu4MgSi, 3.1325 · BS H14 · also Avional

2017A (EN AW-2017A, AlCu4MgSi(A), material 3.1325, historically duralumin/Avional) is a heat-treatable 2000 series Al-Cu alloy usually supplied naturally aged to T4 as bar, profile and sheet.

CNC machiningSheet metalPremium cost $$$

2017A tempers and conditions

2017A is supplied in 10 conditions, soft to hard.

Compare all 10 conditionsHide
Condition · open for datasheetBest forYield MPaTensile MPaElong. %HardnessConductivity
Annealed
Choose for deep forming, bending or cold heading of rivets before solution treatment.751802245 HB50 % IACS
Slightly strain hardened
Soft, near-annealed 2017A with only incidental strain hardening from straightening or forming; used as a workable pre-heat-treatment condition.1002051852 HB50 % IACS
Re-solution heat treated by the user and naturally aged
Applies to parts formed in O temper and then heat treated by the fabricator; slightly lower and more scattered properties than mill T4.23538515103 HB34 % IACS
Solution heat treated, stress-relieved by compression, naturally aged
T4 condition for forgings and hand-forged blocks in which residual stress is removed by cold compression, giving T4-level strength with low distortion on machining.25040014105 HB34 % IACS
Extruded, stretched, no further straightening
Stress-relieved extruded bar/profile supplied without post-stretch straightening; used for long machined parts.25540013108 HB34 % IACS
Extruded, stretched, minor straightening allowed
Same as T4510 but with a light straightening pass for tighter bar straightness tolerances.25540013108 HB34 % IACS
Solution heat treated and naturally aged
The standard commercial condition for 2017A bar, rod and profiles — best all-round strength/toughness for machined fittings, rivets and bolts.26041014110 HB34 % IACS
T4, stress relieved by stretching
T4 with controlled stretch — specify for plate and rolled bar that will be machined asymmetrically.26040514108 HB34 % IACS
T3, stress relieved by stretching
Stress-relieved plate/bar for machined parts that must stay dimensionally stable after heavy stock removal.27542013112 HB34 % IACS
Solution heat treated, cold worked and naturally aged
Cold-worked variant of T4 for sheet and drawn rod where slightly higher strength and straightness are needed.29042512115 HB34 % IACS

What is 2017A?

2017A (EN AW-2017A, AlCu4MgSi(A), material 3.1325, historically duralumin/Avional) is a heat-treatable 2000 series Al-Cu alloy usually supplied naturally aged to T4 as bar, profile and sheet. Strength approaches 2024 while forming and machining behaviour is more forgiving, so it is used for rivets, bolts, gear blanks, structural joints and general machined parts. Corrosion resistance is poor and requires cladding, anodizing or paint; fusion welding is not practical, and continuous service should stay below about 120 °C. 2024 is the nearest higher-strength option. 2017A has a density of 2.79 g/cm³ (0.101 lb/in³), heavier than 77% of aluminum grades. It melts at 512°C (954 °F). 2017A has a yield strength of 260 MPa (37.7 ksi) and a tensile strength of 410 MPa (59.5 ksi) — stronger than 68% of aluminum grades. Elongation at break is 14% and the elastic modulus is 72.5 GPa (10.5 Msi).

What is 2017A used for?

  • Rivets
  • Structural plate
  • Aircraft fittings

Advantages

  • Easy to machine — 75/100, better than 86% of aluminum grades
  • Ductile — tolerates forming and impact — 14%, better than 81% of aluminum grades
  • Tough — resists crack growth — 30 MPa·√m (27.3 ksi·√in), better than 76% of aluminum grades

Limitations

  • Difficult to weld — 20/100, worse than 89% of aluminum grades
  • Needs corrosion protection — 35/100, worse than 85% of aluminum grades
  • Limited service temperature — 120°C (248 °F), worse than 79% of aluminum grades

2017A properties

Typical room-temperature values; bars are the position among aluminum grades.

Physical3

2017A has a density of 2.79 g/cm³ (0.101 lb/in³), heavier than 77% of aluminum grades. It melts at 512°C (954 °F).

Density2.79 g/cm³0.1 lb/in³
Melting Point (Solidus)512°C954 °F
Liquidus Temperature641°C1,186 °F

Mechanical14

2017A has a yield strength of 260 MPa (37.7 ksi) and a tensile strength of 410 MPa (59.5 ksi) — stronger than 68% of aluminum grades. Elongation at break is 14% and the elastic modulus is 72.5 GPa (10.5 Msi).

Elastic (Young's) Modulus72.5 GPa10.5 Msi
Shear Modulus27 GPa3.9 Msi
Bulk Modulus75 GPa10.9 Msi
Poisson's Ratio0.33
Tensile Strength (Ultimate)410 MPa59.5 ksi
Yield Strength (0.2% offset)260 MPa37.7 ksi
Elongation at Break14%
Compressive Strength260 MPa37.7 ksi
Shear Strength260 MPa37.7 ksi
Fatigue Strength (Endurance Limit)125 MPa18.1 ksi
Fracture Toughness (K_IC)30 MPa·√m27.3 ksi·√in
Hardness, Brinell110 HB
Hardness, Rockwell B62 HRB
Hardness, Vickers118 HV

Thermal6

2017A is rated for continuous service to 120°C (248 °F). It conducts heat at 134 W/m·K (77.4 BTU/hr·ft·°F), worse than 60% of aluminum grades. Thermal expansion is 23 µm/m·K (12.8 µin/in·°F).

Thermal Conductivity134 W/m·K77.4 BTU/hr·ft·°F
Specific Heat Capacity873 J/kg·K0.21 BTU/lb·°F
Thermal Expansion (CTE, 20–100 °C)23 µm/m·K12.8 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

2017A conducts electricity at 34 % IACS, worse than 52% of aluminum grades.

Electrical Conductivity34 % IACS
Electrical Resistivity5.07×10⁻⁸ Ω·m2 µΩ·in
Magnetic Responsenon-magnetic

Chemical & Environmental3

Corrosion resistance is fair (35/100), worse than 85% of aluminum grades.

Galvanic Potential (seawater, vs SCE)-0.69 V
Corrosion ResistanceFair35/100
Chemical Resistance SummaryFair in neutral atmospheres when painted or anodized; poor in chlorides, seawater and acids/alkalis; susceptible to intergranular and exfoliation attack in T4 and to galvanic coupling with steel or copper.

Sustainability4

Producing a kilogram of 2017A 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 Water1,100 L/kg132 gal/lb
Typical Recycled Content25%

Manufacturability8

2017A's machinability is very good (75/100, better than 86% of aluminum grades); weldability poor (20/100); formability fair (45/100).

MachinabilityVery good75/100
Machinability Rating (AISI 1212 = 100 %)75%
WeldabilityPoor20/100
Formability (cold)Fair45/100
CastabilityPoor25/100
Brazeability / SolderabilityPoor15/100
PolishabilityGood55/100
Anodizing Responsefair — protective and hard anodizing possible but the coating is grey/mottled and lower quality than 6000 series; not suitable for bright decorative anodize because of the ~4% Cu.

Common Calculations5

Specific Strength (UTS / density)calculated147 kN·m/kg
Specific Stiffness (E / density)calculated26 MN·m/kg
Modulus of Resiliencecalculated466 kJ/m³
Thermal Diffusivitycalculated55 mm²/s
Thermal Shock Resistance Indexcalculated33

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

Strength versus weight in the aluminum family

Yield strength against density for every aluminum grade FabDigit runs. 2017A is highlighted; hover a dot for its name, or open the interactive family chart.

20501002005002.22.42.62.83Density (g/cm³)Yield strength (MPa) — log scale2017A

Working with 2017A

Is 2017A easy to machine?

Excellent free-cutting behaviour in T4/T351 with short chips; use sharp polished-flute carbide tools, high speed and flood emulsion to avoid built-up edge.

Can 2017A be welded?

Not suited to fusion (MIG/TIG) welding due to hot cracking and loss of temper — join by riveting, bolting, adhesive or friction stir welding.

Can 2017A be formed, bent or molded?

Form in O temper or within a few hours of solution treatment (refrigerate to delay natural ageing); T4 tolerates only mild bends with generous radii.

Manufacturability

The process limits FabDigit applies to 2017A. Every 2017A part is priced by an engineer; design inside these and the quote comes back without a redesign loop.

CNC machining

MachinabilityExcellent75 / 100
ISO material groupN.2
Cutting speed (rough / finish)280 / 340 m/min
Minimum wall0.8 mm
Minimum internal radius1 mm
Drill depth limit6× diameter
Best surface (machined / polished)Ra 0.8 / —
Hardenable after machiningNo

Sheet metal

FormabilityFair45 / 100
WeldabilityPoor20 / 100

2017A 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
Si0.2 – 0.80.5
Feimpurity≤ 0.70.35
Cuprincipal strengthening element3.5 – 4.54
Mn0.4 – 10.7
Mg0.4 – 10.7
Cr≤ 0.1
Zn≤ 0.25
Ti+Zrcombined limit per EN 573-3≤ 0.25
Others (each)≤ 0.05
Others (total)≤ 0.15
Albalance

What surface finishes work on 2017A?

Requires protection: chromate/chrome-free conversion coating plus paint, or hard anodizing; decorative bright anodizing gives a dull grey, Cu-mottled finish, and cladding or Alclad-type sheet is used for corrosive service.

Surface treatments FabDigit runs on aluminum parts — pick them in the quote configurator or call them out on the drawing. Each links to its datasheet in the surface-finish library (thickness, specs, call-out, material verdicts).

Equivalent designations

Standards and trade names that resolve to Aluminum 2017A in FabDigit's catalog. Equivalence is nominal — check the exact specification when certification matters.

EN / DIN / Werkstoff-Nr.
AlCu4MgSi3.1325
BS
H14
Trade names
Avional

How much does 2017A cost?

2017A is a premium-cost aluminum ($$$), cheaper than about 60% of the materials FabDigit quotes. Part price depends far more on geometry, tolerance and quantity than on the raw stock — upload a CAD file for a live quote.

2017A — frequently asked

What is 2017A used for?

2017A is typically used for rivets, structural plate and aircraft fittings. In short: european 2017 variant; rivet stock.

What is the yield strength of 2017A?

2017A has a typical yield strength of 260 MPa (37.7 ksi) and a tensile strength of 410 MPa (59.5 ksi) — stronger than 68% of aluminum grades. Strength varies by condition: see the 10 listed tempers.

Is 2017A easy to machine?

Yes — machinability is rated very good (75/100, better than 86% of aluminum grades). Excellent free-cutting behaviour in T4/T351 with short chips; use sharp polished-flute carbide tools, high speed and flood emulsion to avoid built-up edge.

Can 2017A be welded?

Not readily — weldability is rated poor (20/100). Not suited to fusion (MIG/TIG) welding due to hot cracking and loss of temper — join by riveting, bolting, adhesive or friction stir welding.

What surface finishes work on 2017A?

Requires protection: chromate/chrome-free conversion coating plus paint, or hard anodizing; decorative bright anodizing gives a dull grey, Cu-mottled finish, and cladding or Alclad-type sheet is used for corrosive service.

Can 2017A be formed, bent or molded?

Form in O temper or within a few hours of solution treatment (refrigerate to delay natural ageing); T4 tolerates only mild bends with generous radii.

What is the maximum service temperature of 2017A?

2017A 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.

How much does 2017A cost?

2017A is a premium-cost aluminum ($$$), cheaper than about 60% of the materials FabDigit quotes. Part price depends far more on geometry, tolerance and quantity than on the raw stock — upload a CAD file for a live quote.

Can FabDigit make parts in 2017A?

Yes — 2017A 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. EN 573-3 Aluminium and aluminium alloys — chemical composition — CEN (2019)
  2. EN 755-2 Aluminium extruded rod/bar, tube and profiles — mechanical properties — CEN (2016)
  3. ASM Handbook Vol. 2: Properties and Selection — Nonferrous Alloys — ASM International (1990)
  4. International Alloy Designations and Chemical Composition Limits (Teal Sheets) — The Aluminum Association (2018)
  5. DIN 1725 / Werkstoff 3.1325 AlCuMgSi — DIN (1986)

Property data is compiled from published supplier and standards handbooks and normalised for comparison; hardness values on non-Brinell scales are converted approximately for charting only. Manufacturability limits are FabDigit quote-engine defaults and may be relaxed by engineering review. Nothing on this page is a certification — request mill certs, CoC or material test reports with your order.