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Aerospace CNC

Aviation CNC machining expert: what that actually means on the shop floor

This page is for design and manufacturing engineers who need airframe, engine and satellite hardware cut to print. We explain the process decisions behind tight-tolerance aviation parts: five-axis setup strategy, titanium and Inconel cutting data, fixture design, and how inspection evidence is built. Read it and you can judge whether a shop is set up for your part or just quoting it.

±0.005 mm tolerance16 five-axis centers4,000 mm max size100% inspection
Aerospace CNC Machining Prototype Service Savannah
Scope

Where aviation machining differs from general CNC work

Same machines, different constraints. Tolerance, material, traceability and the cost of a scrap part all shift.

Baseline

What an aviation CNC machining expert has to control

A general machine shop holds ±0.05 mm and calls it tight. Aviation work starts an order of magnitude finer. GreatLight machines to ±0.005 mm, which is ±0.0002 in. At that scale the machine is rarely the limiting factor. The fixture, the thermal state of the part, and the order of operations decide whether the number holds on the last cut.

Material changes the whole plan. Aluminum 6061-T6 and 7075 cut fast and stay put. Ti-6Al-4V (TC4) and Inconel generate heat in the cut zone instead of the chip, so tool life drops and the surface can work-harden if the feed is too light. Magnesium AZ31B cuts easily but demands chip control because fine magnesium swarf ignites. Each of these needs its own speeds, feeds and coolant strategy, not one generic program.

Traceability is the other split. A bracket for ground equipment can ship with a dimensional report. A flight part usually needs raw material certs, a process route, inspection records and a first article report. We build that paperwork alongside the chips, not after the fact. When a part fails a check, the record tells you which operation drifted.

  • 1
    ToleranceAviation parts commonly land at ±0.005 mm; general work sits near ±0.05 mm.
  • 2
    MaterialTitanium and Inconel need heat-aware cutting data, not aluminum recipes.
  • 3
    EvidenceMaterial certs, in-process checks and final reports shipped with the parts.
Setup

Why five-axis setup dominates tight-tolerance aviation work

Five-axis means the tool and the part move together on five axes at once: X, Y, Z plus two rotary axes. The payoff is not speed. It is that a complex contour, a pocket floor and a bolt-hole pattern can come off in one setup. Every extra setup adds a re-fixturing error and a new datum stack. Removing setups removes error sources.

For aerodynamic surfaces and turbine hardware, the tool can stay normal to the surface through the pass. That keeps the effective cutting radius constant, which holds surface finish (Ra 0.8–1.6 μm on a machined profile) and avoids the witness lines a three-axis raster leaves on a curved face. On thin-wall parts, the same motion lets us approach at an angle so the cutter pushes into the wall instead of lifting it.

GreatLight runs 16 simultaneous five-axis machining centers, with a Ø400 mm rotary table and travels up to 4,000 × 400 × 150 mm. Larger prismatic parts go on the 4,000 mm capacity machines. Five-axis is not automatic for every job. A simple flat plate with holes is faster and cheaper on a three-axis mill, and we will say so.

The cost of five-axis is programming time and a stiffer setup. When a part has one sculpted face and ten flat features, the honest answer may be a hybrid: five-axis for the contour, three-axis for the drilling. We quote the routing that holds the print, not the one that sounds most advanced.

  • 1
    Good fitSculpted contours, thin walls, angled hole patterns, one-setup datums.
  • 2
    Poor fitFlat plates with simple holes; a three-axis mill is faster and cheaper.
Process

Fixtures, workholding and the order of operations

On a thin airframe rib, the fixture is the process. Clamp force bends a 2 mm wall before the cutter touches it. We use vacuum plates, low-melt fixturing or sacrificial tabs so the part is supported without being crushed. For parts that move after stress relief, we plan a semi-finish, a stress-relief cycle, then a finish pass that takes the last 0.2 mm.

Datum strategy matters as much as the machine. On a five-axis part we try to establish one primary datum and machine as many features from it as possible. When a print calls for a datum that only exists after a secondary operation, we flag it during DFM review instead of discovering it at inspection.

Tool selection follows the geometry. Long reach tools deflect, so we keep the length-to-diameter ratio as low as the pocket allows and use a smaller stepover on deep walls. For Inconel and titanium, high-pressure coolant and coated carbide keep the heat in the chip. We do not run a finishing pass on a work-hardened skin left by a dull tool.

Free DFM analysis comes back within 12 hours with the quote. If a radius is too small for the tool that reaches the floor, or a tolerance is tighter than the feature needs, that is where we say it. Fixing it in the model is cheaper than scrapping a titanium part.

Selection

Material and routing guide for common aviation parts

Starting points only. Final cutting data depends on geometry, wall thickness and finish callout.

MaterialTypical aviation useMachining note
Aluminum 7075-T6Structural brackets, fittingsFast, stable; watch residual stress on thin webs
Aluminum 6061-T6Housings, panels, prototypesEasy to cut; good for first articles
Ti-6Al-4V (TC4)Engine mounts, airframe nodesLow speed, high feed; heat stays in the cut
InconelHot-section and exhaust hardwareRigid setup required; tool wear is the limit
17-4PH (SUS630)Actuators, shafts, fastenersMachines well in condition A, then age
Magnesium AZ31BLightweight housingsChip control and fire-safe handling required
Verification

Inspection and how tolerance is proven

A ±0.005 mm callout is a claim until it is measured. We inspect 100% of parts before shipment and keep three checkpoints: incoming raw material, in-process monitoring, and a final inspection. Reports are available on request. For first articles, the report maps each checked feature back to the drawing.

In-process checks catch drift early. If a boring tool wears and the bore grows, the operator sees it at the next check, not after the run. That is why a 99.99% qualification rate is a process result, not a promise about any single part.

CMM work needs a stable thermal state. A titanium part pulled hot from the machine reads differently from one that has settled. We let parts rest before final measurement on tight features, and we record the temperature when it matters. This is the part of aviation work that does not show up on a quote but shows up in the yield.

Surface finish is checked against the callout: Ra 0.2–0.8 μm for fine finishes, Ra 0.8–1.6 μm for high-finish surfaces, Ra 1.6–3.2 μm as-machined. Finishing options include anodizing, electroless nickel, plating, powder coating, black oxide, bead blasting, brushing and laser marking with a minimum character height of 1.5 mm.

Capacity

What the shop needs to look like for this work

Aviation work needs a machine mix, not one big machine. GreatLight runs 127 high-precision CNC machines across three plants in 7,600 m²: 16 five-axis centers, 12 four-axis mills, 27 three-axis machines, and 16 mill-turn centers. The mix lets us route a part to the machine that holds it best instead of forcing every job onto the most expensive spindle.

Size range matters too. Travels cover 4,000 × 400 × 150 mm for long parts, 750 × 1,150 × 550 mm and 600 × 600 × 600 mm for mid-size housings, and compact envelopes down to 500 × 310 × 200 mm for small precision details.

Quality systems hold the process in place. GreatLight is certified to ISO 9001:2015, IATF 16949:2016, ISO 13485:2016 and ISO 27001:2022. The information-security cert matters when a customer sends controlled drawings. Uploads are handled as confidential, and an NDA is available on request.

Volume runs from one prototype to 10,000+ parts with no minimum order quantity. Production can start within 24 hours of a released order, and parts typically ship in 3–5 days. Historical late-delivery probability is below 2%.

FAQs

Common questions about aviation CNC machining

How is aviation machining different from standard precision CNC work?

Tolerances are tighter, usually an order of magnitude finer. Geometries are more complex, with thin walls and tight radii. Materials like titanium and Inconel are harder to cut and less forgiving of a light feed.

Documentation is heavier. Raw material certs, in-process records and final inspection reports ship with the parts, and the cost of a failed part is far higher than in general industry.

When is five-axis machining the right choice, and when is it not?

Five-axis pays off when a part has sculpted surfaces, angled holes, or features that would need three or more setups on a three-axis mill. Cutting them in one setup removes re-fixturing error and holds the datum stack together.

It is the wrong choice for flat plates with simple holes. Those run faster and cheaper on a three-axis machine, and we will route them there.

Which materials do you machine for aerospace parts?

Aluminum 6061, 6061-T6, 2024, 5052, 5083, 6063, 6082, 7075 and ADC12; titanium TA1, TA2 and TC4 (Ti-6Al-4V); Inconel; magnesium AZ31B and AZ91D.

Stainless grades include 303, 304, 316, 316L, 420, 430, 431, 440C and 17-4PH (SUS630). Steels cover 1018, 1045, 4130, 4140, 4340, A36 and tool steel.

How do you hold ±0.005 mm on a thin-wall part?

Support the part without crushing it. Vacuum plates, low-melt fixturing or sacrificial tabs replace hard clamps on thin walls. The cut is split into semi-finish, stress relief, then a light finish pass.

Tool reach is kept short to limit deflection, and the part is allowed to settle before final measurement.

What inspection evidence comes with an order?

Incoming material check, in-process monitoring and 100% final inspection before shipment. Reports are available on request, and first articles map each checked feature back to the drawing.

Surface finish is verified against the callout, from Ra 0.2–0.8 μm for fine finishes up to Ra 1.6–3.2 μm as-machined.

Can you start from a prototype and scale to production?

Yes. There is no minimum order quantity, so a single prototype and a 10,000+ part run use the same process and inspection standard.

Quotation and free DFM analysis come back within 12 hours, production can start within 24 hours, and parts typically ship in 3–5 days.

Send the drawing, get a routing and a number

Upload a STEP file and tolerance callouts. An engineer reviews manufacturability and returns a quotation with free DFM notes within 12 hours.

12-hour quote100% inspectionNDA on requestNo MOQ

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