What the Process Does
5-axis CNC milling combines three linear axes with two rotational axes. The additional motion provides more flexible cutter access for compound angles, contoured surfaces, deep cavities, and features that are difficult to reach from a fixed vertical direction. It is used when a part benefits from machining several faces or sculpted forms with fewer re-fixturing operations.
Process Flow
The machining sequence should be planned around the part's functional datums, feature access, material behavior, and the required inspection method. The detailed route is ultimately governed by the actual machine configuration, workholding, tool availability, and production quantity.
|
Process Stage |
Purpose |
|
1. Input review |
Confirm the 3D model, drawing, material, critical dimensions, datums, quantity, and finish requirements. |
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2. Setup plan |
Select workholding, datum strategy, cutting tools, machining order, and access to all functional features. |
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3. Machining |
The machining plan begins with a 3D model review, identification of critical datums, and tool-access analysis. CAM programming then defines the roughing, semi-finishing, and finishing paths while considering collision avoidance, workholding, tool length, and the direction of the cutter relative to the surface. |
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4. Verification |
Quality planning commonly emphasizes the relationship between complex surfaces, locations of angled features, wall thickness, profile tolerance, and the datums used to inspect the finished part. Functional dimensions should be clearly called out instead of applying extremely tight tolerances everywhere. |
Design Intent
Five-axis work should be designed with manufacturability in mind: identify critical surfaces, leave sensible radii for cutter access, avoid unnecessarily deep narrow pockets, and discuss any thin-wall or vibration-sensitive areas early in the review.
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ENGINEERING INPUT Β Provide a 3D CAD model, a drawing with critical tolerances and datums, the material grade, requested quantity, surface finish, and any inspection or packaging requirements. |
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Part Geometry and Materials

Features and Typical Components
Typical features include compound-angle holes, blended surfaces, deep pockets, undercut-adjacent areas, thin walls, multi-face locating features, freeform contours, and complex curved channels.
Typical components Β Representative components include impellers, aerospace brackets, contoured mold inserts, orthopedic or surgical-device components, turbine-like forms, complex manifolds, and high-value prototype parts.
Material Selection
The process can be applied to aluminum, steels, stainless steels, brass, copper, titanium, and engineering plastics. Material choice affects spindle load, tool selection, heat management, part support, and the finishing strategy.
|
Material group |
What to consider |
Typical reason for selection |
|
Aluminum |
Machinability, thermal movement, cosmetic finish. |
Lightweight housings, brackets, fixtures, heat-management parts. |
|
Steel & stainless |
Strength, corrosion resistance, heat, chip control. |
Industrial, structural, fluid-system, precision mechanical parts. |
|
Brass, copper & titanium |
Conductivity, corrosion, strength-to-weight, cost. |
Fittings, electrical parts, high-performance or specialized components. |
|
Engineering plastics |
Stiffness, temperature, chemical environment, burr control. |
Insulating, lightweight, prototype, wear or fluid-contact parts. |
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MATERIAL NOTE Β The material must be selected against functional needs first. Machinability, heat, corrosion, weight, cost, and the desired surface treatment should then be reviewed together. |
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Technical Planning and Quality

Manufacturing Considerations
Five-axis work should be designed with manufacturability in mind: identify critical surfaces, leave sensible radii for cutter access, avoid unnecessarily deep narrow pockets, and discuss any thin-wall or vibration-sensitive areas early in the review.
Quality and Inspection
Quality planning commonly emphasizes the relationship between complex surfaces, locations of angled features, wall thickness, profile tolerance, and the datums used to inspect the finished part. Functional dimensions should be clearly called out instead of applying extremely tight tolerances everywhere.
Surface Finish and Part Protection

Finishing can include anodizing, blasting, polishing, plating, passivation, painting, or laser marking. Cosmetic requirements and contact surfaces should be distinguished from functional surfaces in the drawing.
Before Production
A manufacturability review should confirm that the tolerance scheme is functional, the specified material is available, the workholding leaves access to critical faces, and the measurement plan can verify all requirements without ambiguity. Where an assembly interface is critical, provide the mating-part information or fit requirement.
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DRAWING PRACTICE Β Call out the dimensions that matter to function. Avoid applying an unnecessarily tight general tolerance where only a limited number of features control the fit, motion, sealing, or alignment of the final assembly. |
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Advantages and Applications
Why Select This Process
The main benefit is improved access to complex geometry. In the right part family, fewer setups can reduce datum transfer, improve feature-to-feature alignment, and prevent repeated handling of sensitive surfaces.
Application Context
Aerospace, medical, robotics, energy, electronics, advanced tooling, and high-performance product development are common five-axis application areas.
|
Application family |
Where the process adds value |
|
Prototype and product development |
Useful where a functional part, review sample, or process route must be validated before a larger production decision. |
|
Industrial and automation equipment |
Supports durable custom hardware, fixtures, housings, interfaces, shafts, passages, and assembly features. |
|
Precision and regulated equipment |
Supports geometry that must be documented through clear datums, material specifications, inspection requirements, and controlled finishing. |
When to Choose Another Process
Use 5-axis machining when the tool must approach from many directions or when several complex faces must remain closely related. Simpler prismatic parts may be more economical on 3-axis or 4-axis equipment.
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QUOTE CHECKLIST Β Include model and drawing files, material grade, order quantity, material certification needs, finishing requirements, critical features, and target delivery date with the RFQ. |
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Key Process Parameters
The values below describe the typical operating envelope of our 5-axis machining cells. Tool length, stick-out, and workholding are planned into the toolpath so that critical surfaces can be reached without re-fixturing.
Parameter |
Typical Value |
|---|---|
Axis configuration |
3 linear (X / Y / Z) + 2 rotary (typically A + C or B + C) |
Trunnion table diameter |
200 β 630 mm, depending on machine |
Rotary axis accuracy |
Β±0.005Β° β Β±0.01Β° indexing on calibrated direct-drive axes |
Standard linear tolerance |
Β±0.05 mm; Β±0.025 mm on critical features; Β±0.01 mm by review |
Surface finish (as-machined) |
Ra 0.8 β 3.2 Β΅m, depending on cutter and material |
Maximum part envelope |
Up to 1,000 Γ 800 Γ 600 mm, machine dependent |
Batch range |
1 to 1,000+ pieces; engineering-driven production runs |
Lead time |
Prototypes 5β10 business days; production 15β25 business days |
Accepted CAD formats |
STEP, IGES, X_T, SLDPRT, CATIA, NX native files welcome |
Machine platforms |
Simultaneous 5-axis VMC / HMC with high-rpm spindle (12,000β30,000 rpm) |
Materials We Machine
5-axis work spans the full material range. The cutter, holder, and toolpath are matched to each material family to keep cycle time and tool wear predictable.
- Aluminum alloys β 6061, 7075, 2024, 5052, 6063, A201 cast plate
- Stainless steel β 304, 316, 17-4 PH, 15-5 PH, 2205 duplex, 321
- Carbon & alloy steel β 1018, 1045, 4140, 4340 pre-hardened, A36
- Titanium β Grade 2, Grade 5 (Ti-6Al-4V), Grade 5 ELI
- Nickel & high-temp alloys β Inconel 625, Inconel 718, Monel 400, Hastelloy C276
- Brass, copper & bronze β C360 brass, C110 copper, C954 aluminum bronze
- Magnesium β AZ31, AZ91 (with dust-control protocols)
- Engineering plastics β PEEK, PEI (Ultem), Delrin, PTFE, polycarbonate
- Tooling materials β H13, D2, A2, S7 hardened steels for mold inserts
Standard Tolerances & Achievable Precision
5-axis work is typically specified to GD&T callouts. ISO 2768-m is the default tolerance scheme, but most 5-axis parts require per-feature callouts, so the real limit is the drawing.
- Standard linear tolerance β Β±0.05 mm
- Precision tolerance β Β±0.025 mm on critical features
- Tight tolerance β Β±0.01 mm by review, dependent on material, feature size, and tool access
- Profile tolerance β 0.05 mm on complex contours is typical; 0.02 mm achievable on aluminum
- Angular positioning β Β±0.02Β° typical on calibrated direct-drive rotary axes
- GD&T support β ASME Y14.5-2018 and ISO 5459 datum schemes
Surface Finish Options
- As-machined β Ra 0.8 β 3.2 Β΅m, depending on cutter and step-over
- Bead blast β glass bead or aluminum oxide for uniform matte finish
- Anodize Type II β clear, black, or dyed, 5β25 Β΅m
- Hard anodize Type III β 25β75 Β΅m, PTFE / Teflon impregnation optional
- Powder coat β polyester, epoxy, hybrid, custom color
- Liquid painting β primer + topcoat, custom color matching
- Electroplating β nickel, tin, zinc, gold, silver, electroless nickel
- Passivation β ASTM A967 / AMS 2700 for stainless steel
- Black oxide & phosphate coating β mild corrosion protection on steel
- Polishing & electropolishing β mirror or sanitary finishes
- Laser marking & engraving β part numbers, logos, UID / 2D Data Matrix
Quality Control & Inspection
5-axis parts usually have critical relationships between features on different faces, so inspection is built around CMM-based GD&T verification rather than simple hand-gauge checks.
- First-article inspection (FAI) β 100 % dimensional report, AS9102 format available
- CMM inspection β Zeiss or equivalent, with CAD-comparison and full GD&T verification
- 3D scanning β optional optical scanning for complex freeform surfaces, especially medical and aerospace
- Surface roughness tester β Mitutoyo SJ-210 or equivalent
- Hardness tester β Rockwell / Vickers / Brinell for material condition and heat-treat verification
- In-process checks β at critical operations, with calibrated hand tools
- Final inspection report β full dimensional record, material certificate, finish records, and photos on request
Design Considerations (DFM Tips)
- Reach the surface before specifying a tight tolerance β 5-axis lets the tool approach from many angles, but tool length, holder clearance, and collision avoidance must be planned together.
- Keep internal corner radii β₯ end-mill radius β minimum R 1.0 mm preferred; smaller radii require micro tooling and slower feeds.
- Use a true 3D model β send the native or neutral file so the CAM team can check tool access against the actual geometry, not a 2D approximation.
- Avoid deep narrow pockets β depth-to-width ratios above 4:1 dramatically increase cycle time and tool deflection.
- Identify the critical surface β call out which surface is the priority for orientation and surface finish; cosmetic and functional faces should be distinguished on the drawing.
- Wall thickness & thin walls β maintain β₯ 1.0 mm in aluminum and β₯ 0.8 mm in plastics; thinner walls need special fixturing and slower cuts.
- Datum strategy β define 3β2β1 datums that match the workholding plan; mismatched datums force a separate inspection setup.
- Undercuts & back-facing features β flag them in the model; some features can only be reached with a 5-axis head and may need a custom tool.
- Tolerance discipline β apply tight tolerances only on functional features; loose tolerances elsewhere keep the part economical.
Industries & Applications
- Aerospace & defense β structural brackets, impellers, engine components, prototype airframe parts, satellite hardware
- Medical & dental β surgical instruments, implant prototypes, orthopedic devices, imaging-system components
- Automotive & motorsport β intake manifolds, turbo housings, prototype engine components, EV battery hardware
- Tooling & molds β mold inserts, contoured electrodes, EDM tooling, injection mold cores
- Energy β turbine components, fuel-cell plates, oil & gas sub-assembly hardware, prototype reactor parts
- Robotics & automation β multi-angle gripper components, sensor mounts, machine-tool bodies
- Semiconductor β vacuum-chamber parts, gas-delivery components, wafer-handling fixtures
Frequently Asked Questions
When does 5-axis make sense over 3 + 2 indexed?
5-axis simultaneous is justified when the tool needs to stay normal to a sculpted surface, when compound-angle features must be cut in a single setup, or when a feature is hidden behind a wall that a 3-axis tool cannot reach. For flat angled faces, 3 + 2 is often more efficient.
What file format do you need for a complex 5-axis part?
A clean 3D model in STEP, IGES, or native CAD (SolidWorks, NX, CATIA, Creo) plus a 2D drawing with GD&T callouts. The native file is preferred because it preserves sketches, surfaces, and construction history used for toolpath planning.
Can you hold tight profile tolerances on freeform surfaces?
Yes. Profile tolerance of 0.05 mm is routine on aluminum; 0.02 mm is achievable on selected features with fine finishing, smaller cutters, and CMM verification. Tight profile tolerance on steel or titanium adds cycle time and cost.
What about exotic alloys like Inconel or titanium?
Both are supported. Tooling, feeds, speeds, and cutter engagement are planned against the material; coolant strategy and chip evacuation are reviewed to keep tool life and surface finish consistent.
Do you handle finishing in-house or outsource it?
As-machined finishing, deburring, and light polishing are in-house. Anodize, plating, powder coat, painting, passivation, and black oxide are routed to qualified partners under our quality system; we remain responsible for the result.
Is a CMM inspection report included?
Yes. For 5-axis parts, a CMM report is normally included because hand-gauge checks cannot verify the critical relationships. A CAD-comparison overlay is provided on request for complex surfaces.
How to Get a Quote
Send a 3D model (STEP / IGES or native CAD), a 2D drawing (PDF / DWG) with GD&T callouts, the material grade, requested quantity, finish or coating specification, inspection requirements, and target delivery date. Within one business day we return DFM feedback, lead time, and a unit / total price. For complex geometry we can sign an NDA before any file exchange.
Process Flow & Manufacturing Sequence
5-axis simultaneous machining lets the cutting tool reach a feature from almost any angle in a single setup. The workflow below reflects how we plan and execute these parts, from CAM simulation through final inspection.
- Design intake & DFM review β the 3D model is reviewed for tool access, collision-free tool paths, and datum strategy. Features that cannot be reached with a 5-axis head are flagged up front.
- Material receiving & verification β incoming bar, plate, billet, forging, or near-net preform is checked against the purchase order and MTC, with full heat-lot traceability.
- Stock cutting β band saw or abrasive saw cuts stock to a near-net blank, leaving a controlled machining allowance on every face that will be touched.
- Workholding selection & fixture build β vacuum fixtures, custom soft-jaw arrangements, modular clamping systems, or trunnion chucks are chosen from the print and the model. A 3-2-1 datum is established on the chosen reference face.
- CAM programming & simulation β tool paths are programmed in Mastercam, Fusion 360, or NX, then verified in full machine simulation. Tool length, holder clearance, and rotary-axis limits are checked against the part envelope.
- Datum probing & work offset β on-machine probe establishes part zero, the trunnion centerline, and the rotary axes zero, with verified accuracy before the first cut.
- Roughing (3 + 2 indexed) β heavy material removal is done with the part indexed to working angles, using high-efficiency roughing, trochoidal paths, or plunge roughing strategies.
- Semi-finish inspection β pilot dimensions, datum alignment, and the most critical features are checked before the finishing pass.
- Semi-finishing β walls and floors are brought to within 0.1 β 0.2 mm of nominal using the same indexing scheme as roughing, leaving a uniform stock for the simultaneous finishing pass.
- Drilling & tapping (indexed or simultaneous) β holes are produced with rigid tapping, thread milling, or boring cycles. Off-angle holes are drilled with the head tilted to keep the tool normal to the surface.
- Simultaneous 5-axis finishing β the tool stays normal (or at a controlled lead / tilt angle) to a sculpted surface while the part rotates around two axes. This achieves profile tolerance, surface finish, and consistent scallop height.
- Edge break & chamfer β sharp edges are broken with a 0.2 β 0.5 mm chamfer, applied per the print with a chamfer mill or by hand on cosmetic features.
- Deburring & cleaning β hand deburring, tumble, or brush deburr, followed by aqueous wash. For complex internal passages, an air-blow or solvent rinse verifies chip removal.
- Final inspection on CMM β full GD&T verification with the rotary datum aligned to machine coordinates, including profile tolerance and 3D-feature callouts. CAD-comparison overlay on request.
- Outsourced surface treatment (if applicable) β anodize, plating, powder coat, passivation, or specialty coating routed to qualified partners under our quality system.
- Packaging & shipping β parts are wrapped, bagged, and packed per customer specification, with full documentation enclosed.
Material Property Reference
The table below covers the materials most often run on our 5-axis cells, including aerospace and medical grades. Lot-specific values are confirmed by the mill certificate (MTC).
Material |
Density (g/cmΒ³) |
Tensile Strength (MPa) |
Yield Strength (MPa) |
Hardness (HB) |
Machinability (%) |
|---|---|---|---|---|---|
Aluminum 6061-T6 |
2.70 |
310 |
276 |
95 |
180 |
Aluminum 7075-T6 |
2.81 |
572 |
503 |
150 |
170 |
Stainless 304 |
8.00 |
515 |
205 |
170 |
45 |
Stainless 316L |
7.99 |
485 |
170 |
160 |
40 |
17-4 PH (H1025) |
7.78 |
1,070 |
1,000 |
330 |
30 |
15-5 PH (H1025) |
7.80 |
1,090 |
1,030 |
330 |
30 |
Titanium Grade 5 |
4.43 |
950 |
880 |
340 |
22 |
Inconel 718 |
8.19 |
1,275 |
1,050 |
360 |
12 |
Inconel 625 |
8.44 |
965 |
490 |
200 |
15 |
Hastelloy C276 |
8.89 |
790 |
360 |
200 |
15 |
Magnesium AZ31 |
1.77 |
260 |
200 |
49 |
500 |
PEEK |
1.32 |
100 |
90 |
85 (R) |
90 |
Machinability ratings are relative to AISI 1212 steel = 100%. HB values in (R) for plastics denote Rockwell, not Brinell.
Cost Drivers & Lead Time Factors
5-axis work carries higher programming and cycle cost than 3 / 4-axis, but it can also eliminate multiple setups. Understanding the cost drivers helps decide when 5-axis is the right investment.
What drives cost
- Material β exotic alloys (titanium, Inconel, Hastelloy) are expensive per kilogram and machine slowly. Aerospace-grade aluminum with certs carries a premium.
- Programming & simulation β 5-axis CAM programming and full machine simulation is typically 4 β 12 hours of engineering per part, more for complex freeform geometry.
- Tooling β ball nose, bull nose, and tapered tools are common. Long-reach holders, shrink-fit or hydraulic chucks add cost per setup.
- Tolerance β profile tolerance of 0.05 mm is routine; 0.02 mm adds cycle time and CMM inspection cost.
- Batch size β programming is amortized; long production runs dilute the engineering cost across the batch.
- Geometry complexity β compound angles, deep pockets, thin walls, and freeform surfaces all extend cycle time and require careful tool-path planning.
- Inspection & documentation β CMM verification with full GD&T, plus AS9102 or PPAP documentation, adds inspection hours.
- Surface treatment β anodize, plating, powder coat, and specialty coatings are outsourced and may add days to lead time.
What drives lead time
- Material sourcing β common bar / plate 2 β 5 days; certified aerospace plate 1 β 3 weeks; titanium and Inconel billet 2 β 6 weeks.
- CAM programming & simulation β typically 1 β 3 days for new parts, less for repeats or library parts.
- Fixture design & build β custom fixtures add 1 β 5 days depending on complexity.
- CNC cycle time β long tool engagements on freeform surfaces; roughing + finishing + drilling typically 2 β 8 hours of spindle time per part.
- Outsourced processes β anodize, plating, heat-treat 2 β 7 business days at qualified partners.
- Inspection & documentation β full FAI, AS9102, PPAP, and CMM programs add 1 β 3 days.
- Shipping β DHL / FedEx 3 β 5 days international; air freight 5 β 10 days; ocean freight 20 β 35 days.
Typical lead times by scenario
Scenario |
Prototype (1 β 5 pcs) |
Low-volume (10 β 100 pcs) |
Production (100+ pcs) |
|---|---|---|---|
Stock material on hand |
5 β 10 business days |
10 β 15 business days |
15 β 25 business days |
Material to be sourced (incl. aerospace cert) |
10 β 18 business days |
15 β 25 business days |
25 β 40 business days |
With outsourced finish (anodize, plating, coating) |
12 β 20 business days |
15 β 25 business days |
25 β 40 business days |
With full FAI / AS9102 / PPAP documentation |
+ 3 β 5 business days |
+ 2 β 3 business days |
+ 1 β 2 business days |
Common Defects & Prevention
5-axis defects typically come from tool access, holder clearance, or interaction between the linear and rotary axes. The list below covers the most common failure modes and the prevention we apply.
Defect |
Cause |
Prevention |
|---|---|---|
Tool / holder collision |
Incomplete simulation, holder not modeled, fixture not loaded into CAM |
Full machine simulation with holder, fixture, and machine limits loaded; verify lead / tilt angles; physical dry-run on critical parts |
Scallop / step-over marks |
Insufficient step-over on finishing, wrong cutter diameter for the scallop height callout |
Calculate step-over from desired scallop; use a smaller tool or a finer pass for tight surface finish callouts |
Profile / form deviation |
Tool deflection, worn cutter, calibration drift on rotary axes, thermal change |
Use shorter / larger cutters, light finishing engagement, calibrate rotary axes, allow thermal stabilization, replace cutters on schedule |
Undercut / back-face damage |
Tool over-travels into a back-facing feature, exit on a back-facing wall |
Lead-in / lead-out lines drawn from safe approach angles; check tool reach against full feature envelope in simulation |
Surface mismatch at face boundaries |
Mismatch between index and simultaneous passes, different tool diameters on adjacent faces |
Use a single finishing tool per surface family, document tool assignments, align datums across passes |
Built-up edge on aluminum / titanium |
Low cutting speed, inadequate coolant, wrong tool coating |
Match speed to material, use coated tools (TiAlN, AlCrN), verify through-spindle coolant, replace cutter at first sign of BUE |
Axis-limit fault / singularity |
Tool path crosses a rotary-axis pole, A / C axes flip |
Plan tool path to avoid poles, use smooth lead-angle transitions, split motion at safe waypoints |
Workholding slip / lift on heavy cuts |
Insufficient clamping force, lifting moment on roughing, fixture deflection |
Match fixture to material, verify torque, use loc-pin + clamp, simulate forces in CAM, run a low-engagement first cut |
Comparison With Related Processes
5-axis simultaneous machining is the most flexible CNC process, but it competes with 3 + 2 indexed work, EDM, and turn-mill for specific geometries. The table below helps pick the right process.
Aspect |
5-Axis Simultaneous Milling (this process) |
3 + 2 Indexed Milling |
EDM (Wire / Sinker) |
|---|---|---|---|
Ideal geometry |
Sculpted freeform surfaces, compound angles, single-setup complex parts, undercuts |
Multi-face prismatic parts, indexed angles, no curved tool-normal surfaces |
Hardened tool steel, sharp internal corners, very deep thin slots, no cutting forces on the part |
Tool access to back-facing features |
Yes, with the head tilted |
Limited; back-facing features usually need a re-clamp or EDM |
Yes, with a properly shaped electrode |
Tightest tolerance |
Β±0.01 mm linear; 0.02 mm profile on aluminum |
Β±0.01 mm linear; profile limited by cutter geometry |
Β±0.005 mm achievable; no mechanical cutting force |
Cost vs. this process |
Baseline (highest programming cost, single-setup saving) |
Lower for parts that don't need simultaneous tool motion |
Higher per part (electrode wear, slow cut); competitive for hard materials and tight internal corners |
When to choose |
Impellers, blisks, sculpted medical / aerospace parts, single-setup complex parts, undercuts |
Multi-face prismatic parts, flat angled features, prototype airframe components |
Hardened tool steel, sharp internal corners, micro-features, no-force cutting on thin walls |
Industry Standards & Certifications
The standards below apply to 5-axis work in particular. Customer-required certifications are referenced in the project scope and documented accordingly.
- ISO 9001:2015 β quality management system baseline.
- AS9100D / AS9102 β aerospace QMS, FAI report format.
- NADCAP AC7110 / AC7119 β aerospace special process accreditation where applicable (heat-treat, surface enhancement).
- ISO 13485:2016 β medical device QMS.
- IATF 16949 β automotive QMS, with PPAP and APQP requirements.
- ISO 2768 β general tolerances (medium / fine / very fine classes).
- ASME Y14.5-2018 β GD&T standard.
- ISO 5459 β datums and datum systems.
- ISO 1101 β GPS, including form, orientation, location, and run-out.
- ISO 10360 β CMM acceptance and reverification test for the inspection equipment used to verify 5-axis parts.
- ASTM A967 / AMS 2700 β passivation of stainless steel.
- AMS 2460 / 2470 β chromium plating on aluminum and steel (when specified).
- AMS 2403 / 2404 β electroless nickel plating.
- MIL-A-8625 β anodize Type II / Type III on aluminum.
- RoHS / REACH β substance compliance for European market access.
- Conflict Minerals (CMRT / RMI) β reporting for tin, tantalum, tungsten, and gold sourcing.
- ITAR / EAR β controlled technical data and export compliance for defense parts.
Packaging, Shipping & Documentation
Packaging protects machined features, threads, and freeform surfaces during transit. The level of packaging scales with part size, value, finish, and shipping method; documentation is enclosed per customer requirement.
Standard packaging
- VCI bag β applied to all ferrous parts to prevent oxidation in transit and storage.
- Custom foam inserts β for sculpted or freeform surfaces that would otherwise rest on a single contact point.
- Foam wrap or compartmentalized trays β protects machined surfaces from contact damage; multi-cavity trays for small parts.
- Sealed poly bag β for medical, optical, or cleanroom-delivered parts.
- Cardboard cartons with internal partitions β for medium and small parts.
- Custom plywood / wood crating β for large, heavy, or precision parts above 25 kg, with foam lining and edge protection.
- ESD-safe packaging β for parts that integrate into electronics or semiconductor equipment.
- Labeling β part number, lot / batch, quantity, material, and customer reference on every outer and inner package.
Shipping options
- DHL / FedEx / UPS β international express, 3 β 5 business days door-to-door, full tracking and customs handling.
- Air freight β 5 β 10 business days for heavier or consolidated shipments.
- Ocean freight (FCL / LCL) β 20 β 35 days for non-urgent production runs.
- Customer-arranged courier β parts released to a customer-provided account on request.
- EXW, FOB, CIF, DAP β Incoterms supported per customer preference.
Standard documentation
- Certificate of Conformance (C of C) β confirms parts were manufactured to the print and meet specified requirements.
- Mill Test Certificate (MTC) β material certificate retained for every heat lot.
- First-article inspection report (FAI / AS9102) β 100 % dimensional report on the first part, including GD&T and profile callouts.
- CMM inspection report β recorded measurements against all GD&T callouts, with optional CAD-comparison overlay.
- Surface finish report β Ra measurements where called out.
- Certificate of Origin (CoO) β for customs clearance.
- Commercial invoice & packing list β standard shipping documentation.
- PPAP / APQP package β for automotive customers, including control plan, PFMEA, and capability data.
Related Capabilities & Cross-Services
5-axis work is often one step in a longer workflow. We coordinate the surrounding services so customers get a single point of accountability for the entire part, not a list of subcontractors.
- Post-machining finishing β bead blast, tumble, hand deburr, light polishing, edge-break, and cosmetic buffing in-house.
- Anodizing & plating β Type II / Type III anodize, hard anodize, electroless nickel, zinc, tin, gold, and silver plating through qualified partners.
- Powder coat & wet painting β polyester, epoxy, hybrid systems, RAL / Pantone color matching, primer + topcoat, and clear coat.
- Heat treatment β solution treatment, aging, through-hardening, case hardening, tempering, and stress relief.
- EDM (wire & sinker) β partner service β for sharp internal corners and hardened tool steel features that milling cannot reach.
- Light assembly & kitting β fastener installation, insert pressing, sub-assembly, and kit packaging.
- Laser marking & engraving β part numbers, logos, UID, 2D Data Matrix, and traceability codes on curved surfaces.
- Design for manufacturing (DFM) review β feedback on tool access, datums, undercuts, and freeform tolerances before cutting chips.
- CMM inspection & 3D scanning β full GD&T verification, CAD-comparison overlay, and reverse-engineering scans for legacy parts.
- Subcontracted services coordination β single point of contact for heat-treat, plating, anodize, coating, and EDM partners.
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