LA CNC Aluminum: How Aluminum Machining Actually Works
This page explains what happens between your CAD file and a finished aluminum component: alloy behavior, spindle and fixture choices, tolerance limits, and surface finish. Written for engineers and buyers who need to judge whether a supplier can hold a drawing, not for people shopping on price alone.

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Why LA CNC aluminum parts behave differently on a machine
Aluminum cuts fast. That is the obvious part. The less obvious part is that it moves. A 6061-T6 block relieved on one side will bend toward the heavier remaining section as the internal stress releases. The cutter did its job; the part still ends up out of flat.
Thermal drift matters too. Aluminum expands about twice as fast as steel for the same temperature rise. A spindle running for six hours warms the casting, the fixture and the workpiece. If the machine has no thermal compensation, dimensions taken at 8 a.m. and 3 p.m. will not match.
Chip evacuation decides your surface finish more often than spindle speed does. Aluminum chips are soft and sticky. They weld to the cutting edge, then drag across the finished wall and leave a torn smear. High-pressure coolant or through-spindle air clears the pocket; a deeper radial cut with fewer passes often finishes cleaner than a light finishing pass.
So the first question is not which alloy is strongest. It is how much stock you are removing, from which side, and how the part will be held while you do it.
Alloy choice: 6061, 7075, 2024 and cast grades
6061-T6 is the default for a reason. It welds, anodizes cleanly, machines at 300–600 m/min surface speed with carbide, and holds ±0.005 mm on a stable setup. Brackets, housings, manifolds, fixture plates and most enclosures start here.
7075-T6 gives roughly twice the yield strength of 6061 and machines to a sharper edge. It also costs more, anodizes to a slightly darker tone, and shows stress cracking at sharp internal corners. Use it for high-load airframe fittings, racing suspension links and molds. Radius your internal corners to at least 0.5 mm.
2024-T4 is the fatigue choice in aerospace work. It has better damage tolerance than 7075 but poor corrosion resistance, so it usually gets Alclad sheet or a protective coating. 5052 and 5083 are for formed sheet and welded tanks, not for tight-tolerance milling.
Cast grades such as ADC12 come in when the geometry is better poured than cut. If wall thickness drops below 2 mm or the part needs pressure tightness, die casting plus a light CNC skim on the sealing faces is often cheaper than machining the whole shape.
Three-axis, five-axis or mill-turn: picking the right setup
A three-axis mill cuts from one direction. Every new face needs a new fixture and a new datum. Two setups on a simple bracket are fine. Six setups on a manifold mean six chances to stack error, and the tolerance budget disappears before the part is finished.
Five-axis machining tilts the tool or the table so the cutter reaches five faces in one setup. The real gain is not speed; it is datum continuity. One setup means one origin, so bores that must stay coaxial actually stay coaxial. On our 16 simultaneous five-axis centers we hold Ø400 mm rotary work and travel up to 4,000 × 400 × 150 mm.
Mill-turn centers handle parts that are mostly round with milled features: valve bodies, actuator housings, sensor housings. Turning and milling in one program removes the concentricity error you get from re-chucking.
Complexity has a cost. Five-axis programming and setup take longer, and a badly designed part can be slower on five axes than on three. If the part is a flat plate with holes, use three-axis and spend the money on inspection instead.
What ±0.005 mm really requires
±0.005 mm is achievable on aluminum, but only when the whole chain supports it: rigid fixturing, sharp tooling, temperature control and a metrology plan. A tolerance printed on a drawing does not create the capability by itself.
Watch where you place tight tolerances. A bore diameter of 20 ±0.005 mm is routine on a good mill. A 300 mm overall length at the same tolerance is a different problem, because thermal expansion over that length is larger than the tolerance band.
Surface finish and tolerance interact. Ra 0.8–1.6 μm is a normal machined finish for aluminum. Ra 0.2–0.8 μm needs a dedicated finishing pass, a sharp edge and often a different tool path. Specify the finish only on the faces that seal, slide or mate; cosmetic Ra everywhere triples cycle time for no function.
Inspectors need the same datum you machined to. If the drawing calls out a datum that cannot be reached in the fixture, the CMM report and the machine will disagree. Fix that in DFM, not in a rework loop.
Anodizing, plating and the finishes that change dimensions
Anodizing builds an oxide layer into the surface. Type II clear adds roughly 5–15 μm per side depending on bath time. Hardcoat runs thicker. If a bore must stay at 10.000 mm, mask it or machine it undersize before coating.
Color anodizing is not paint. The dye sits in the porous oxide, so the base alloy changes the final shade. 6061 and 7075 will not match each other in the same bath. If two mating parts must look identical, cut them from the same heat and coat them in the same run.
Electroless nickel gives a uniform deposit on complex geometry and holds tight on internal features. Zinc plating and black oxide are cheaper but thinner. Bead blasting before anodizing hides tool marks and produces a matte surface; polished surfaces need a separate step.
Laser marking is limited by character height. We mark down to 1.5 mm character height; below that, legibility drops and the marking may not survive hardcoat. Put the marking callout on the drawing with the exact text and location.
Matching alloy and process to the part
Pick the row that matches your geometry and load case.
| Part type | Typical alloy | Best process | Why |
|---|---|---|---|
| Flat bracket, holes, slots | 6061-T6 | 3-axis mill, 2 setups | Cheapest path; flatness is easy to hold |
| Manifold with angled ports | 6061-T6 | 5-axis, 1 setup | Datum continuity across five faces |
| High-load fitting | 7075-T6 | 5-axis or mill-turn | Strength per gram; radius internal corners |
| Airframe fatigue part | 2024-T4 | 3-axis plus coating | Damage tolerance; needs corrosion protection |
| Round housing with ports | 6061-T6 | Mill-turn center | Concentricity held in one chucking |
| Thin-wall enclosure | ADC12 then skim | Die cast plus CNC | Walls under 2 mm are cheaper poured |
| Welded tank or panel | 5052 / 5083 | Sheet metal plus CNC | Formability and weldability beat machinability |
The short version
For flat, hole-heavy parts, choose three-axis and put the budget into inspection. For parts with multiple angled faces or coaxial bores, choose five-axis and accept the higher setup cost, because datum continuity is cheaper than rework.
Questions engineers ask before releasing a drawing
How do I know if my part should be cast instead of machined?
Wall thickness is the first test. Below about 2 mm, machining aluminum gets expensive because the part deflects under cutting force.
The second test is volume. If the same geometry repeats thousands of times, a die casting tool plus a skim pass on the sealing faces usually beats cutting the whole shape from solid. Prototypes still go to CNC because the tool does not exist yet.
Does the alloy affect the achievable surface finish?
Yes. 6061-T6 and 6082 machine to a consistent Ra 0.8–1.6 μm with carbide tooling. 7075 can go finer but tends to show faint tool marks on large faces.
Cast aluminum is the opposite. Porosity and hard silicon particles tear the surface, so castings usually get a skim cut and then a coating instead of a fine finish spec.
What causes a part to warp after machining?
Released internal stress is the usual cause. Plate and extruded bar carry residual stress from rolling or extrusion. When one side is removed, the balance changes and the part bends.
Symmetric material removal, stress-relieved stock and a rough-then-finish sequence reduce it. For very flat parts, a light finishing cut after a rest period helps more than a slower spindle.
Can aluminum parts hold tight tolerances after anodizing?
The coating grows on the surface, so tight features change size. Type II clear anodizing adds roughly 5–15 μm per side depending on bath time.
The fix is decided at the drawing stage: mask critical bores, machine them undersize by the expected growth, or finish them after coating. Decide before the first cut, not after the parts come back.
How do I read a CMM report for a first article?
Start with the datum callouts. If the report uses different datums than the drawing, the numbers are not comparable and the report is meaningless.
Then check the tightest tolerances first and the cosmetic callouts last. Ask for the raw measurement values, not only pass or fail, so you can see how much margin the process actually has.
Which features drive the price of aluminum CNC parts most?
Setup count, not material cost. Each additional face that needs its own fixture adds time, risk and inspection work.
After that come tight tolerances on large dimensions, fine surface finish over large areas, and secondary operations such as anodizing or laser marking.
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