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Aluminum 2011

Aluminum $$

The screw-machine aluminum. 2011 is an Al-Cu alloy with lead and bismuth inclusions that act as built-in chip breakers, giving the highest machinability rating of any common aluminum (Aluminum Association rating of A — the reference standard). Used almost exclusively for high-volume turned parts: fittings, fasteners, connector bodies, knobs. The trade-offs are real — 2011 has poor corrosion resistance, essentially zero weldability, and the leaded chemistry restricts it from food/medical/potable water applications. Property data below reflects T3 / T8 temper as noted per variant.

Service °C
150°C continuous (T3/T8 overage above this)
Tensile
360–410 MPa (52–59 ksi) — T3 to T8
Density
2.82 g/cm³ (0.102 lb/in³) — slightly denser than 6061 due to Pb/Bi
Cost
$$
$2.50/lb
Trade names: 2011-T32011-T8Free-machining aluminumAlCu6BiPbEN AW-2011

The screw-machine aluminum. 2011 is an Al-Cu alloy with lead and bismuth inclusions that act as built-in chip breakers, giving the highest machinability rating of any common aluminum (Aluminum Association rating of A — the reference standard). Used almost exclusively for high-volume turned parts: fittings, fasteners, connector bodies, knobs. The trade-offs are real — 2011 has poor corrosion resistance, essentially zero weldability, and the leaded chemistry restricts it from food/medical/potable water applications. Property data below reflects T3 / T8 temper as noted per variant.

Properties

Mechanical
Mechanical properties for Aluminum 2011
Tensile360–410 MPa (52–59 ksi) — T3 to T8
Yield280–310 MPa (40–45 ksi) — T3 to T8
Elongation10–15% (lower than 6061 due to Pb/Bi inclusions)
Modulus71 GPa (10,300 ksi)
Hardness95–100 HB / Rockwell B 55
Fatigue strength120 MPa (18 ksi) at 5×10⁸ cycles, rotating beam
Poisson's ratio0.33
Thermal
Thermal properties for Aluminum 2011
Continuous max150°C continuous (T3/T8 overage above this)
Short-term max~190°C short-term
Min serviceCryogenic-capable but rarely used in cold service
Conductivity150–170 W/m·K
CTE23 × 10⁻⁶/°C (12.8 × 10⁻⁶/°F)
Specific heat870 J/kg·K
Metal-specific
UNSA92011
ENEN AW-2011 (AlCu6BiPb)
Magneticnon magnetic
Cond.39% IACS
Composition (% wt)
Al 91.3–94.6 (balance) Cu 5.0–6.0 Pb 0.2–0.6 Bi 0.2–0.6 Fe ≤0.7 Si ≤0.4 Zn ≤0.3 other_each ≤0.05 other_total ≤0.15

Variants (2)

2011-T3 T3 T3 bar

Standard screw-machine bar temper. Property data above represents T3 to T8 range. Solution treated, cold worked, naturally aged. Most distributor stock is T3.

2011-T8 T8 T8 bar

Solution + cold work + artificial age. Higher strength than T3 with slight SCC improvement. Specified for applications requiring ~45 ksi yield without alloy substitution.

Processing

Machinability: excellent
Chip: Best-in-class aluminum chip behavior — the lead and bismuth inclusions act as discrete chip breakers, producing short broken chips ideal for screw machines and bar feeders. This is THE selling point of 2011.
Gumming: Essentially none. The Pb/Bi inclusions prevent the smearing and built-up edge that plague 6061 on aggressive cuts.
Finish: 16 Ra readily; 8 Ra achievable. Surface can show a slight gray cast versus 6061 due to lead-bismuth phase distribution.
Tooling: Standard carbide or HSS. 2011 is forgiving on tool selection — cycle times limited by spindle and chuck, not by metallurgy. Speeds 600–2000 SFM, feeds 0.005–0.025 in/rev. Cutting fluid optional but recommended for finish work. AA machinability rating is "A" (the reference standard at 100% — every other aluminum is rated relative to 2011-T3).
2011 exists because screw machines want short chips. On Swiss-style lathes and multi-spindle bar machines, 2011 runs unattended for hours where 6061 would tangle on long stringy chips within minutes. For any high-volume turned part below ~50 ksi UTS requirement, 2011 is the default choice. Above that strength, designers move to 2017 or 7075 free-machining variants (less common).
Weldability: poor

2011 is essentially unweldable for structural service. The lead and bismuth segregate at grain boundaries during cooling and produce hot cracks and porosity. Design 2011 parts for mechanical fastening, press-fit, or adhesive bonding only. If a joint must be welded, switch alloys for the weldable section and join mechanically.

Heat treatments
Solution + cold work + artificial age (T8) (100 HB) — Highest-strength 2011 temper. The cold-work step before aging develops dislocation structure that maximizes precipitate nucleation. Modestly better SCC behavior than T3 in chloride service.
Solution + cold work + natural age (T3) (95 HB) — Standard supply temper for screw-machine bar stock. Most 2011 bar at distributors is T3 unless T8 is explicitly ordered.
Full anneal (O temper) (~45 HB) — Rarely used for 2011 — the entire point of 2011 is the heat- treated machining behavior. Annealed 2011 is softer but machines no better than annealed 6061.
Surface treatments
Sulfuric acid anodize (Type II) (5–25 μm) — 2011 anodizes poorly — the high copper content causes the oxide layer to be dark, non-uniform, and prone to streaking. Copper migrates out of the anodic layer creating cosmetic defects. For decorative anodize, switch to 6061 or 6063. For functional corrosion protection only, anodize is acceptable but visually unappealing.
Chromate conversion coating (0.05–0.5 μm) — Best surface treatment for 2011. Provides corrosion protection and paint adhesion without the cosmetic problems of anodize. Hex-chrome formulations being phased out for trivalent.
Electroless nickel (5–125 μm) — Used when 2011 needs hard, uniform corrosion barrier — common on industrial fluid fittings. More expensive than anodize but better appearance and corrosion behavior on copper-bearing alloys.

Corrosion resistance

general Atmospheric fair Worse than 6061 due to copper content (5–6% Cu vs 0.15–0.4% in 6061). Develops gray oxide and surface pits faster in outdoor exposure. Anodize or paint for service life.
saltwater poor Pitting and exfoliation in marine atmospheres. Do not specify for marine immersion without significant protection.
acids poor Less acid-resistant than 6061. Avoid acid-cleaning or pickling without controlled inhibitors. HCl and HF attack rapidly.
bases poor Aluminum is attacked by NaOH/KOH. 2011's higher copper makes no improvement here.
oxidizing Environments fair Concentrated nitric tolerated; other oxidizers vary.
reducing Environments fair
Corrosion behavior is the second-largest 2011 weakness after regulatory restrictions. For corrosion-prone applications, choose a different alloy or design in protective coating from the start.
⚠ Galvanic risks with
Carbon steel (severe)Stainless steel (severe)Copper and brass (severe)Graphite (severe)Titanium (mild)

Regulatory

FDA grade
NSF 51
NSF 61
USP Class VI
RoHS
REACH
EU 10/2011

Lead content (0.2–0.6%) makes 2011 incompatible with RoHS, REACH, food-contact (FDA 21 CFR 175.300), and drinking water (NSF 61). Many medical-device and consumer-electronics specifications exclude leaded aluminum entirely. RoHS exemption 6(c) covers some industrial machined components but is being phased down. For new designs in regulated markets, specify 6262 (bismuth-tin, lead-free free-machining aluminum) instead — slightly worse machinability, no leaded-aluminum compliance issue.

Notes & applications

Overview

2011 is the screw-machine aluminum. The lead and bismuth inclusions (0.2–0.6% each) act as built-in chip breakers — when the tool reaches an inclusion, the chip cleaves cleanly into a short fragment that falls away from the tool. The result is the highest machinability rating of any aluminum (Aluminum Association rating “A” — every other aluminum’s machinability is reported as a percentage of 2011).

This single property determines everything about 2011’s place in the materials landscape. 2011 is not a general-purpose structural aluminum. It’s a screw-machine grade chosen for production turned parts where cycle time and chip handling dominate the manufacturing economics. Knobs, fittings, connector shells, fasteners, camera hardware — anywhere a CNC lathe runs unattended on a bar feeder.

The price for that machinability is paid in three places:

  • Corrosion — 5–6% copper makes 2011 more anodic and less corrosion- resistant than 6061. Outdoor service requires anodize or paint.
  • Weldability — essentially zero. Pb and Bi segregate and crack on cooling. Design 2011 for mechanical fastening only.
  • Regulatory — lead content disqualifies 2011 from food contact, potable water (NSF 61), and most RoHS/REACH applications.

For new designs in regulated markets, 6262 (bismuth-tin, lead-free free-machining aluminum) has been displacing 2011 for ~20 years. 6262 machines slightly worse than 2011 but cleans up the compliance problem. For unrestricted industrial applications, 2011 remains the cost-per-cycle leader.

Machining notes

2011 exists for machining. The recipe is forgiving:

  • Carbide or HSS (both work well)
  • Speed: 600–2000 SFM
  • Feed: 0.005–0.025 in/rev — feeds can run aggressive without chip control problems
  • Cutting fluid optional but recommended for finish work and tool life
  • Standard chip breakers and inserts; geometry choice less critical than on 6061

The Pb/Bi inclusions break chips into roughly 3–10 mm fragments that clear gravitationally through bar machine workspaces. This is what makes unattended multi-hour runs possible on Swiss-style and multi-spindle machines.

Surface finish on 2011 is excellent when tools are sharp — 16 Ra or better straight off the tool, 8 Ra with a finishing pass. The machined surface has a slight gray cast versus 6061 due to lead- bismuth phase distribution; this is normal and not a defect.

Temper selection guidance

  • T3 — Standard screw-machine bar. ~40 ksi yield. The default unless application requires more strength or SCC resistance.
  • T8 — When 45 ksi yield is needed without alloy substitution. Modest improvement in SCC behavior over T3.
  • O — Rarely used. The point of 2011 is the heat-treated machining behavior; annealed 2011 doesn’t outperform annealed 6061.

For applications requiring strength above 2011-T8’s ~45 ksi yield in a turned part, consider:

  • 2017-T4 (free-machining, no lead) — modest improvement
  • 7075-T6 with free-machining geometry — much higher strength, worse cycle time
  • 303 stainless — different material class but similar machining economics for higher-strength parts

Welding and joining

Don’t weld 2011 for structural service. Lead and bismuth segregate at the solidification front and produce hot cracks and porosity. Fusion welding (TIG, MIG, stick) is essentially impossible to do reliably. Friction stir welding is theoretically possible but not commercially established for 2011.

In practice, 2011 parts are joined by:

  • Threaded fasteners — the dominant method
  • Press-fits and interference assemblies
  • Adhesive bonding — chromate-converted surface for adhesion
  • Mechanical staking and crimping

If a part design requires welding, switch alloy rather than trying to weld 2011.

Anodize considerations

2011 anodizes poorly. The 5–6% copper content causes:

  • Non-uniform color — anodic layer ranges from dark gray to nearly black depending on local copper distribution
  • Streaking — copper migrates out of the oxide during anodize, creating visible streaks on prominent surfaces
  • Reduced corrosion resistance of the anodic layer itself versus copper-poor alloys

For decorative anodize on visible parts, don’t use 2011. Switch to 6061 (clean anodize, slight copper darkening), 6063 (best anodize uniformity), or 5052 (clean anodize on sheet stock).

For functional corrosion protection where appearance doesn’t matter, 2011 anodize works but is rarely the right choice — chromate conversion (Alodine/Iridite) gives better protection on 2011 without the cosmetic problems.

Corrosion considerations

2011’s high copper content makes it more corrodible than other structural aluminums. In bare condition:

  • Indoor dry service — essentially indefinite (the typical application)
  • Outdoor atmospheric — gray oxide and pitting within months
  • Marine atmosphere — heavy corrosion within a year without protection
  • Saltwater immersion — do not specify

For any non-indoor application:

  • Chromate conversion is the standard protection
  • Electroless nickel for harder corrosion barrier (industrial fittings, hydraulic adapters)
  • Paint over chromate for cosmetic outdoor applications

Galvanic risks are severe — 2011 in mixed-metal assemblies with steel, stainless, or copper will corrode preferentially in moist service. Use dielectric isolation or matched-metal fasteners.

Regulatory considerations

The leaded chemistry creates compliance issues in many markets:

  • RoHS — lead is restricted; 2011 fails by composition. Some industrial-component exemptions exist but are tightening.
  • REACH — lead is on the SVHC candidate list. 2011 parts must be declared in supply-chain reporting.
  • FDA food contact (21 CFR 175.300) — lead-containing aluminum alloys are excluded.
  • NSF 61 (drinking water) — lead-containing aluminum is excluded.
  • California Prop 65 — lead disclosure required for consumer products.
  • EU 10/2011 (food contact) — leaded aluminum excluded.

For applications in any of these regulated spaces, specify 6262 (lead-free free-machining aluminum with bismuth-tin substitution) or move to 6061 / 6063 if machinability is non-critical.

Applications by industry

  • Industrial automation — high-volume CNC-turned fittings, bushings, knobs, levers. The dominant 2011 application.
  • Electronics — connector shells, BNC/SMA bodies, RF connector parts. Most consumer electronics now spec 6262 instead for RoHS compliance.
  • Plumbing and fluid handling — industrial fluid fittings, hose ferrules, compression fittings. Lead-free alternatives required for any drinking-water service.
  • Photography and optics — camera bodies, tripod parts, optical mounting hardware. High-volume turned components.
  • Consumer products — pen barrels, writing instrument components, decorative hardware. Many modern designs have switched to 6262.

Failure modes worth designing around

Specifying 2011 in a regulated application is the most common real-world 2011 failure — not a mechanical failure but a compliance failure caught at audit. If the design will ever ship to consumers, food/water contact applications, EU markets, or California, start with 6262 instead of needing to redesign later.

Galvanic corrosion in mixed-metal assemblies is the second common field failure. Steel fasteners through 2011 parts in moist service corrode the 2011 preferentially. Use isolation washers, anodized surfaces under fastener heads, or compatible-metal fastening.

SCC at high cyclic stress in T3 temper — sustained tensile stress above ~50% of yield in a chloride environment cracks T3 within months. T8 mitigates somewhat. For SCC-prone applications, switch alloy entirely.

Welding attempts — 2011 cracks during fusion welding. Designers unfamiliar with leaded aluminums sometimes try to weld 2011 fittings in field repair; the welds always crack. Train fabricators or mechanical-fasten exclusively.

Sources & standards

Standards: ASTM B211 (rolled or cold-finished bar, rod, wire)ASTM B210 (drawn seamless tubes)AMS 4225 (2011-T3 bar/rod, screw-machine quality)EN AW-2011 / EN AW-AlCu6BiPbISO AlCu6BiPbDIN EN 573-3

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