Most custom sheet metal fabrication quotes come back wrong for one of three reasons: the flat pattern was unfolded with the wrong K-factor, a hole sits closer to a bend than the process can tolerate, or a critical feature was left as-formed when it should have been machined after forming. None of those are pricing problems. They are specification problems, and they are fixable before you send the RFQ.
This guide gives you the numbers. It covers what custom sheet metal fabrication can actually hold across cutting, bending, joining and finishing, where the tolerance stack-up really accumulates, and the decision rule for moving a feature off the press brake and onto a machining centre. It is written for engineers and buyers sourcing precision sheet metal fabrication from a contract manufacturer, so the emphasis is on what you write on the drawing rather than what a machine datasheet claims.
In one line: custom sheet metal fabrication is the set of cutting, forming, joining and finishing operations that turn flat metal sheet into constant-thickness parts. Typical capability is ±0.10–0.20 mm on cut profiles, ±0.25–0.50 mm on formed flange lengths and ±0.5–1.0 degrees on bend angles, at material thicknesses from 0.2 mm to roughly 6 mm.
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What custom sheet metal fabrication covers, and where it stops
The five process families
The sheet metal fabrication process converts flat stock into a formed part through a fixed sequence of operations. A typical custom sheet metal fabrication job uses some subset of five families, and each one adds its own variation to the final dimension:
- Cutting — fiber laser, CNC punching, waterjet or plasma. Creates the flat profile, holes and slots.
- Forming — press brake bending, rolling, coining, embossing. Turns the flat pattern into a three-dimensional part.
- Joining — TIG, MIG, spot or laser welding, riveting, clinching, hardware insertion.
- Finishing — anodizing, powder coating, electroplating, brushing, sandblasting, screen printing, laser marking.
- Inspection — first article, in-process checks, CMM verification, coating thickness and adhesion testing.
The ordering matters more than most drawings admit. A hole cut in the flat blank holds laser accuracy. The same hole, once its position depends on a bend, inherits the press brake's accuracy instead. That single fact explains most "the parts don't fit" complaints, and it drives the design rules in the rest of this guide.
Where fabrication ends and CNC machining begins
Custom sheet metal fabrication is the right process when your part is essentially a constant-thickness shell: brackets, panels, chassis, mounting plates, covers, frames, busbars, shields. If a part is largely a formed blank with holes and a few bends, fabrication wins on cost and lead time every time.
CNC machining takes over when a feature needs three-dimensional geometry, a tight fit, or a surface relationship that forming cannot control. Bores for bearings, press-fit pin holes, sealing faces, O-ring grooves, coaxial bores across a welded joint, and anything calling for tighter than roughly ±0.05 mm belong to machining. We cover the comparison in more detail in our guide to sheet metal fabrication versus CNC machining.
In practice, a large share of real production parts need both. That hybrid route — a fabricated blank with machined critical features — is the single most under-specified decision in sheet metal procurement, and section 5 gives you the rule for making it.
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Cutting: laser, punch or waterjet
Process selection by thickness and volume
| Process | Practical thickness | Typical profile tolerance | Best for | Setup cost | Volume sweet spot |
|---|---|---|---|---|---|
| Fiber laser cutting | 0.5–8 mm carbon steel, 0.5–6 mm stainless, 0.5–4 mm aluminium | ±0.10–0.20 mm | Complex outlines, slots, tabs, one-off and low-volume work | Low | 1–500 pcs, and beyond |
| CO2 laser cutting | 0.5–12 mm, slower | ±0.15 mm | Legacy parts, non-metals | Low | 1–200 pcs |
| CNC turret punching | 0.5–6 mm steel, stainless, aluminium | ±0.13–0.25 mm | High-quantity repetitive holes, louvers, vent patterns | Medium (tooling) | 500+ pcs with repeated features |
| Waterjet | 1–50 mm and beyond | ±0.08–0.13 mm | Heat-sensitive alloys, very thick stock, no heat-affected zone | Low | 1–100 pcs, thick material |
| Plasma | 1–25 mm carbon steel | ±0.38–0.76 mm | Thick plate where edge quality is secondary | Low | 1–50 pcs, thick |
The cutting process fixes the accuracy of every one of your laser cut sheet metal parts, so it is the right place to start rather than the press brake.
The crossover between laser and punching is worth knowing because it is the most common place a buyer overpays. Above roughly 500 pieces with a repeated hole pattern, a turret punch beats a fiber laser on unit cost because the tooling is amortised across volume and the punch cycle is faster than a laser traverse for simple geometry — typically under two seconds for a 50 mm slot in 16-gauge steel. Below about 200 pieces, laser wins outright because there is no tooling to pay for.
Feature-size rules that decide your price
Fiber lasers cut a kerf of roughly 0.1–0.2 mm, and the molten metal has to clear the cut. That sets hard limits:
| Feature | Minimum | Recommended | Why |
|---|---|---|---|
| Hole diameter | 1.0 × material thickness | 1.5 × thickness | Below 1×T the beam cannot clear dross cleanly; hole roundness suffers |
| Slot width | 0.8 × thickness | 1.2 × thickness | Narrow slots force slow feed and heat build-up |
| Bridge between holes | 1.0 × thickness | 2.0 × thickness | Thin webs warp from laser heat and distort adjacent holes |
| Distance from hole to part edge | 1.0 × thickness | 2.0 × thickness | Edge collapse and burr formation |
| Corner radius (internal) | 0.5 × thickness | 1.0 × thickness | Avoids stress concentration and reduces laser dwell at the corner |
For holes smaller than the material thickness, do not force the laser. Drill or ream them as a secondary operation, or specify the hole after forming. A 2 mm hole in 3 mm stainless is a drilling job, not a cutting job, and treating it that way usually removes cost rather than adding it. If you need guidance on which features to move to secondary operations across a whole part family, that is the core of a DFM analysis before quoting.
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Bending: where most dimensional error is born
Press brake bending tolerance decides the accuracy of every formed feature, and bending introduces more variation than any other step in custom sheet metal parts. Laser cutting is repeatable to a tenth of a millimetre; bending involves springback, material thickness variation, grain direction and tooling wear, and every one of those shows up in the finished flange. This is the section worth reading before you select a sheet metal bending service.
Bend allowance, K-factor and drifting flat patterns
When a sheet bends, the outer surface stretches, the inner surface compresses, and somewhere inside the material a neutral axis neither stretches nor compresses. Bend allowance is the arc length of that neutral layer through the bend zone — the material consumed by the bend:
BA = θ × (R + K × T)
where θ is the bend angle in radians, R is the inside bend radius, T is material thickness, and K is the K-factor locating the neutral axis as a fraction of thickness.
CAD software calculates this automatically using whatever K-factor is set in its defaults — and those defaults are frequently wrong for your material and tooling. A K-factor error of 0.05 on a 90-degree bend in 2 mm steel shifts the flat pattern by roughly 0.3–0.5 mm. Multiply that by six bends and you have 2–3 mm of cumulative error, which is more than enough to fail an assembly.
| Material | Typical K-factor (air bend) | Typical K-factor (coined) |
|---|---|---|
| Cold-rolled mild steel (SPCC) | 0.30–0.41 | 0.42–0.44 |
| Aluminium 5052-H32 | 0.33–0.45 | 0.44–0.46 |
| Aluminium 6061-T6 | 0.38–0.45 | 0.44–0.46 |
| Stainless steel 304 | 0.35–0.45 | 0.44–0.50 |
| Copper and brass alloys | 0.33–0.40 | 0.42–0.45 |
The only reliable way to fix K-factor for a given material and tool set is to bend a test coupon, measure the actual consumed length on a CMM, and correct the flat pattern before releasing production. For a one-off bracket, the default is fine. For a 5,000-piece run where two parts bolt together, it is worth the day.
Minimum inside radius and grain direction
Forming beyond a material's ductility cracks the outer surface of the bend. The inside radius is the variable you control:
| Material | Minimum inside radius | Notes |
|---|---|---|
| Cold-rolled steel (SPCC) | 0.5–1.0 × T | 1.0 × T up to 3 mm; 1.5 × T above |
| Aluminium 5052-H32 | 0.5 × T | Most formable common aluminium |
| Aluminium 6061-T6 | 1.0 × T | T6 temper cracks at tighter radii; anneal for R under 1 × T |
| Aluminium 6063-T5 | 1.0 × T | Cosmetic extrusions; grain direction matters |
| Stainless steel 304 / 316 | 0.5–1.0 × T | Higher springback; expects larger radii |
| Brass C260 | 0.5 × T | Excellent formability |
| Phosphor bronze | 1.0–1.5 × T | Spring temper needs generous radii |
Two further rules come free with the radius decision:
- Bend perpendicular to the rolling grain wherever the part is visible or load-bearing. Bending along the grain produces surface tearing on aluminium and reduces fatigue life in steel.
- Keep holes at least 2 × T from the bend line (3 × T plus the radius is safer), and slots at least 3 × T. Inside that distance, the bending force pulls the hole out of round and shifts its position — the classic "oval hole" complaint. If a hole must live near a bend for functional reasons, specify it in the formed state and plan to drill it after bending. A sheet metal fabrication service worth using will flag this during quoting rather than after the first article.
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Joining, welding distortion and inserted hardware
Joining is where a precise custom sheet metal fabrication job most often loses its accuracy, because heat distortion is the one variable no fixture fully controls.
Budgeting for weld distortion
Welding is the loosest process in the sequence. Heat input causes expansion and contraction that no fixture fully suppresses, so welded assemblies typically land at ±0.25–0.50 mm on weldment dimensions, and manual TIG or MIG can drift to ±0.5–1.0 mm. Robotic welding with good fixturing recovers part of that, but never all of it.
Practical consequences for your drawing:
- Move critical dimensions away from weld zones. Locating holes and mating faces near a weld seam inherit the weld's variation.
- Use balanced weld sequencing — alternate sides, stitch rather than run continuous, and allow cooling between passes.
- Add 0.2–0.5 mm clearance at mating surfaces if the assembly will be welded. Trying to hold a ±0.05 mm press fit across a welded joint is a specification error, not a supplier failure.
- Specify a post-weld machining operation on any face that must be flat or any bore that must be round after welding. This is normal, not exceptional, in precision work.
PEM inserts, rivets and the holes they need
Self-clinching hardware is the most cost-effective way to add threads, standoffs and cable mounts to a formed panel — but it needs the right hole and the right side of the sheet. Specify the hardware part number, the insertion side, and the material and thickness of the host sheet. A PEM insert specified as "+0.075/−0.000 mm on the hole diameter" is a press-controlled feature, not a forming-controlled one: the hole must be punched or laser-cut to that window before insertion, and it will close up slightly if you powder coat afterwards. Which brings us to a step most drawings ignore entirely.
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Tolerances you can actually hold
Sheet metal fabrication tolerances come in three groups: those the cutting process controls, those the forming process controls, and those only a secondary machining operation can deliver. Most quoting disputes come from treating all three as a single number. The same discipline applies to machined features, where the CNC machining tolerance guide sets out the equivalent capability limits.
Per-process capability
This table is the reference to design against for custom sheet metal parts. It describes process capability under normal production conditions, not the best result achievable on a good day.
| Feature or process | Typical tolerance | Notes |
|---|---|---|
| Fiber laser cut profile | ±0.10–0.20 mm | Flat-state features only |
| Laser cut hole diameter | ±0.08–0.15 mm | Holes smaller than 1 × T need drilling |
| Feature location (flat state) | ±0.20–0.30 mm | Depends on sheet movement and thermal input |
| Turret punch hole position | ±0.13–0.25 mm | Tool wear dependent |
| Press brake, single bend (linear) | ±0.25–0.50 mm | Flange length measured from a datum |
| Press brake, angular | ±0.5–1.0° | Angle-sensor press brakes hold the tight end |
| Multi-bend cumulative | ±0.76 mm and wider | See stack-up below |
| Hole-to-bend dimension | ±0.25–0.50 mm | Always looser than hole-to-hole |
| Welded assembly | ±0.25–0.50 mm | Robotic, fixtured |
| Manual welded assembly | ±0.5–1.0 mm | Operator dependent |
| Post-weld or post-form machining | ±0.02–0.05 mm | Secondary operation |
| General untoleranced dimensions | ISO 2768-m | Only applies when the standard is invoked on the drawing |
The rule that saves the most money: state your general tolerance as ISO 2768-m and apply tight tolerances only to features that control fit or function. Every extra tight dimension adds setup time, inspection time and scrap risk without improving the part.
Tolerance stack-up, worked
Take a 4-bend mounting bracket with a hole at each end, 50 mm flanges, 2 mm aluminium. Here is where the error goes:
| Contribution | Value |
|---|---|
| Laser cut hole position in the flat blank | ±0.15 mm |
| Bend 1 flange length | ±0.30 mm |
| Bend 2 flange length | ±0.30 mm |
| Bend 3 angle, ±0.5° across a 50 mm flange | ±0.44 mm |
| Bend 4 angle, ±0.5° across a 50 mm flange | ±0.44 mm |
Worst-case linear addition gives 1.63 mm. Root-sum-square, which is closer to observed behaviour for independent random errors, gives about 0.77 mm. Either way, hole-to-hole across four bends is a sub-millimetre-class dimension at best — and nowhere near the ±0.05 mm a designer sometimes writes on it.
On a recent 4-bend bracket, the first article measured 0.9 mm out across the two end holes. That was inside the range calculated above and still outside the ±0.3 mm the assembly needed — which is why the next revision moved both holes onto a post-form machining operation instead of tightening the bends.
Two design answers, both standard practice:
- Datum the bend, not the edge. Dimension flange lengths from a functional datum face rather than from a cut edge, so cutting error does not stack into forming error.
- Relocate the critical pair. If the two holes must be within ±0.05 mm of each other, machine them after forming in a single setup. That removes the bend contributions entirely.
When to machine after forming
This is the hybrid decision. Use it feature by feature:
| Feature | As-formed capability | Post-form machined | Decision rule |
|---|---|---|---|
| Cosmetic or clearance hole (Ø tolerance ≥ ±0.2 mm) | ±0.15–0.30 mm | not required | Leave as-formed |
| Bolt hole for a standard fastener with clearance | ±0.25 mm | not required | Leave as-formed |
| Hole-to-hole across one or two bends | ±0.50–0.80 mm | ±0.05 mm | Leave as-formed if the mating part has clearance |
| Hole-to-hole across three or more bends | ±0.8–1.6 mm | ±0.05 mm | Machine after forming |
| Bearing bore or press-fit pin hole | not achievable | ±0.02–0.05 mm | Always machine after forming |
| Flat sealing face or gasket land | ±0.3 mm flatness per 100 mm | ±0.02 mm | Machine after forming |
| Threaded hole coaxial with a formed flange | not achievable | ±0.05 mm | Machine after forming |
| Slot used as an alignment datum | risky | ±0.05 mm | Machine after forming |
The cost logic is straightforward. A post-form machining operation adds a setup and machine time — realistically a 10–25% uplift on the fabricated part price for a handful of features on a small bracket, and a larger share on a complex chassis that needs a fixture. Weigh that against the cost of a rejected assembly, an on-site fit failure, or a rework loop, and the hybrid route pays for itself the first time the as-formed parts do not assemble. Where the volume is low, this is often cheaper than trying to bend to a tolerance the process cannot hold — the same logic that makes low volume CNC machining economical for prototype and pilot builds. The machining operation itself is ordinary work for a CNC milling service or a CNC turning service; when the critical feature is a contoured face rather than a hole, it moves to five-axis CNC machining instead.
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Finishing changes dimensions
Finishing is the stage of custom sheet metal fabrication that competitors skip, and it causes more surprises than bending does. Every coating adds material to the surface it covers, and added material changes every dimension it touches.
Coating thickness versus hole and thread allowance
| Finish | Typical thickness per surface | Diameter change on a Ø6.00 mm hole | Effect on threads | Mitigation |
|---|---|---|---|---|
| Anodizing Type II (decorative, dyed) | 5–15 µm | 6.01–6.03 mm | Minor; usually still gauges | None normally needed |
| Anodizing Type III (hard) | 25–50 µm | 6.05–6.10 mm | M6 may fail a go gauge | Mask threads, or tap after anodizing |
| Powder coating | 60–120 µm | 5.76–5.88 mm | Threads unusable if coated | Mask or plug all threads and bores; specify thread masking on the drawing |
| Zinc plating | 5–15 µm | 6.01–6.03 mm | Fine | None normally needed |
| Electroless nickel | 5–25 µm | 6.01–6.05 mm | Tight tolerance threads may need pre-tap allowance | Add allowance before plating |
| Brushing or sandblasting | Material removal only | 0 to −0.02 mm | None | Control flatness, not size |
| Laser marking | None | None | None | See note on anodized surfaces below |
Three rules follow from that table:
- State the inspection state. "Ø6.00 ±0.05 mm" is ambiguous on a powder-coated part. Write "Ø6.00 ±0.05 mm after coating" or "before coating, minimum material condition" and the ambiguity disappears. This one sentence prevents a large share of coating-related rejections.
- Mask before you coat, not after. Tapping a powder-coated hole removes coating at the edge, creates a chip ring, and looks wrong on a visible face. Masking is far cheaper.
- Allow for hard anodizing growth in press fits. A 40 µm hard anodize grows a bore by 80 µm on diameter — the difference between a light press fit and a part that will not go together.
Cosmetic faces: brush grain, anodize colour and flatness
For visible panels — audio front panels, mixer chassis, amplifier faceplates, instrument enclosures — the finish specification carries as much weight as the dimensional one. Three things determine whether a batch looks like one product or five:
- Brush grain direction. Specify grain orientation relative to the part's longest visible edge, and keep it consistent across every part in the assembly. Grain runs in the coil direction by default; if your part is bent, the visible face may show the grain running across a seam instead of along it. A wrong grain direction will pass every dimensional check on the drawing and still get the entire batch rejected on sight.
- Anodize colour consistency. Anodized colour varies with alloy lot, surface preparation and bath conditions. For a multi-part assembly, specify that all parts come from one anodizing batch, and give a physical or photographic master for the target tone.
- Flatness on large panels. Forming stresses and finishing heat both move a large flat panel. Panels over roughly 300 mm should carry an explicit flatness callout per unit length rather than relying on general tolerances.
Serial numbers, batch codes, Data Matrix and QR marks are the fourth cosmetic-face decision, because on an anodized panel the mark has to be legible without breaking the coating. Marking before anodizing lets dye fill an engraved mark; marking after anodizing uses low-power annealing to darken the surface without removing material. We cover the trade-off, along with UDI and traceability requirements, in our guide to laser marking service for metal parts.
Ruijin runs adjacent anodizing capacity and has delivered exactly this class of work — for example a compact control-unit enclosure in aluminium with a horizontal brushed finish and black anodizing, laser-marked panel graphics, produced as a small-batch retail SKU. That combination of fabrication, machining and finishing under one roof is where a hybrid supplier earns its margin on cosmetic products. Our brushed aluminum audio panel guide covers the surface side in depth, and anodizing aluminum covers the process window.
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Material selection for precision sheet metal
Material choice drives formability, finish cost and how much custom sheet metal fabrication the part will tolerate before it needs a secondary operation.
| Material | Formability | Corrosion | Finish compatibility | Typical fabricated parts |
|---|---|---|---|---|
| SPCC cold-rolled steel | Excellent | Poor without coating | Powder coat, zinc plating, painting | Brackets, chassis, mounting plates, covers |
| Galvanised steel | Good | Good | Powder coat (pre-treat required) | Outdoor panels, HVAC, electrical enclosures |
| Stainless 304 / 316 | Moderate; high springback | Excellent | Passivation, brushing, electropolishing | Medical chassis, food equipment, marine brackets |
| Stainless 430 | Moderate | Good | Brushing, passivation | Appliance panels, decorative trims |
| Aluminium 5052 | Excellent | Good | Anodizing, powder coat, brushing | Lightweight covers, transport panels, brackets |
| Aluminium 6061-T6 | Moderate; cracks at tight radii | Good | Anodizing (Type II/III) | Structural brackets, machined-and-formed hybrids |
| Aluminium 6063-T5 | Good | Good | Excellent anodizing response | Audio panels, cosmetic extrusions, knobs |
| Aluminium 3003 | Excellent | Good | Anodizing, painting | Deep-drawn parts, cosmetic covers |
| Brass C260 / H62 | Excellent | Good | Polishing, plating, brushing | Contacts, terminals, decorative plates |
| Phosphor bronze | Moderate | Good | Plating, passivation | Spring contacts, connectors |
| Copper T1 / T2 | Excellent | Moderate; tarnishes | Plating, passivation | Busbars, shielding, heat paths |
Thickness range matters too. Our production stamping runs 0.2–3.0 mm, and precision sheet metal fabrication in the same facility covers the adjacent range comfortably; beyond that, process selection and tooling change materially. If your part mixes a formed shell with turned or milled features, brass CNC machining and aluminum CNC machining cover the machining side of the same materials list. For stamped brass contacts, terminals and shielding plates, brass stamping parts is the more relevant route.
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DFM checklist before you release the RFQ
Run this against every part before you send it. In our experience it removes most quote revisions and rework loops.
| # | Check | Pass criterion |
|---|---|---|
| 1 | Inside bend radius meets minimum for material and temper | R ≥ value from the minimum radius table |
| 2 | Bend radii are uniform across the part where possible | Fewer tool changes, lower cost |
| 3 | Hole diameter ≥ material thickness | Otherwise specify drilling or reaming |
| 4 | Holes at least 2 × T from a bend line | 3 × T + R recommended |
| 5 | Slots at least 3 × T from a bend line | 4 × T + R recommended |
| 6 | Flange length at least 4 × T | Shorter flanges cannot be formed reliably |
| 7 | K-factor matches material and bend method | Validate with a coupon on high-volume work |
| 8 | Bend direction stated for every bend | Up or down relative to the flat pattern |
| 9 | Critical features dimensioned from a functional datum | Not from a cut edge |
| 10 | Tight tolerances applied only where function requires | Everything else ISO 2768-m |
| 11 | Coating allowance applied to holes and threads | Consistent with the finishing table above |
| 12 | Inspection state stated for every tight dimension | Before or after coating, explicitly |
| 13 | Hardware specified with part number and insertion side | Not just "M6 insert" |
| 14 | Flat pattern supplied or explicitly waived | If supplied, confirm the K-factor used |
If steps 9 to 12 are correct, you will have removed the four most common causes of fabricated-parts disputes. Everything else is normal production variation. When a supplier pushes back on an item in this list, treat it as information about how well they understand their own process — that instinct is worth applying across the whole vendor evaluation, and it is the same lens we describe in choosing a CNC supplier. Before accepting a quote, check what the supplier actually runs in-house — our about page lists the equipment, certifications and associated plants behind Ruijin Fenghui.
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Cost drivers and lead time
Pricing custom sheet metal fabrication means pricing five operations, and the cost structure of a fabricated assembly looks nothing like a machined one. Here is where the money actually goes on custom sheet metal parts, and which levers move each line.
| Cost element | Share of a typical fabricated part price | What moves it |
|---|---|---|
| Material | 40–55% | Alloy and thickness; aluminium and stainless swing more than steel; scrap nesting efficiency |
| Cutting | 10–15% | Outline complexity, hole count, material thickness, whether punching is viable |
| Bending | 8–12% | Number of bends, bend sequence, tooling changes, part size |
| Welding and assembly | 8–15% | Weld length, fixturing, hardware insertion count |
| Finishing | 10–20% | Coating type, masking complexity, cosmetic requirements, batch colour matching |
| Inspection and overhead | 5–10% | Documentation level, FAI, PPAP, traceability |
The levers that move price most, in order of impact:
- Volume and tooling route. Above ~500 pieces with repeated holes, moving from laser to turret punching can cut cutting cost substantially. Above ~5,000 pieces with a stable design, converting sheet metal parts to progressive die stamping changes the economics completely, at the cost of tooling — we compare the routes in stamping or CNC for your part.
- Bend count and tooling consistency. Four bends with one radius is cheaper than four bends with four radii.
- Cosmetic requirements. A brushed, anodized, colour-matched visible face can cost more than the fabrication itself.
- Tolerance discipline. Tightening tolerances beyond process capability adds inspection cost without adding function.
On lead time: the dominant variables are tooling (none for laser and press brake), finishing batch scheduling, and documentation level. A fabrication-only part with no exotic finish is a matter of days. Prototype work in our facility runs on a 3–7 day sample cycle when the RFQ includes a usable model, a dimensioned drawing and the finish specification — the same door-to-door expectation our CNC prototyping customers work to.
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Documentation and compliance
The paperwork level is a design input, not an afterthought. Decide it before you quote, because it changes both price and lead time.
| Requirement | When it applies | What you should receive |
|---|---|---|
| Material certificate | Almost always for regulated industries | Mill certificate to EN 10204 3.1 |
| First Article Inspection (FAI) | New part, new tooling, or a change to either | Ballooned drawing with measured results on every dimension |
| Dimensional report | Sampling basis, ongoing | CMM or manual report against the ballooned drawing |
| Coating certification | Finished visible or functional parts | Thickness, adhesion and colour verification |
| PPAP | Automotive (IATF 16949 programmes) | Level agreed at award — typically Level 3 for production parts |
| Process validation | Medical (ISO 13485 programmes) | IQ, OQ, PQ documentation and a validated process window |
| Traceability | Regulated or safety-critical parts | Heat lot or coil lot tied to the shipment |
Our quality system is built around IATF 16949 (NQA certificate 1833021), ISO 9001:2015 (certificate 19824QK3217R0S) and ISO 13485, so fabricated parts can be produced under the same controls as machined ones — relevant when a single assembly mixes a formed bracket and a machined interface. If your programme is automotive, our notes on IATF 16949 for machining suppliers describe the documentation structure; for medical work, see ISO 13485 CNC machining.
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Industry playbooks
The same sheet metal fabrication services behave differently depending on what the finished part has to survive. These five routes cover most of what we quote, and they follow the same path work takes through the shop: a process route fixed at quotation, a case history that shows the outcome, and the supplier behind both.
Audio and electroacoustic products
The defining requirement is cosmetic. Front panels, mixer chassis, amplifier faceplates and rack ears are seen by the end customer, so grain direction, anodize tone and hole edge quality all matter as much as the dimensions. Practical rules: keep visible bends to a minimum, orient grain along the longest visible edge, batch-anodize every part of one product together, and put any press-fit or bearing feature onto a post-form machining operation. Our audio equipment capability covers this class of work directly.
Automotive brackets
Brackets and mounting plates are the highest-volume fabricated parts in most automotive programmes. Headline capability is generous — laser tolerance and press-brake tolerance are easily sufficient for mounting holes with clearance — but the trap is the interface. Any bracket that carries a bearing, a bushing or a sensor face needs that feature machined after forming, and the drawing should say so explicitly rather than relying on the supplier to raise it. Automotive bracket CNC machining covers the machined end of this range.
Medical equipment chassis
Medical chassis are usually low volume, cosmetically visible and documentation-heavy. The three things that determine success are a stable cosmetic finish, a validated cleaning-compatible surface, and documentation that matches the device file. Stainless and anodized aluminium are the common choices; passivation or anodizing must be specified with the inspection state because both change hole sizes. See medical device CNC machining.
Consumer electronics and 3C
Thin-wall, tight-cosmetic, high-mix. Fabricated internals — shields, brackets, mid-frames — are common, but the tolerance that matters is usually the relationship between a fabricated part and a machined part in the same stack. Datum strategy across the two processes decides whether the assembly fits, not the tolerance of either part alone. See consumer electronics CNC machining.
Robotics and automation
Frames, covers and cable-management brackets. Load paths matter more than cosmetics. The main design decision is whether a joint should be welded and then machined, or bolted from separate fabricated parts — on low volumes, the bolted route often wins even at a small weight penalty, because it avoids the weld-and-machine sequence entirely. See robotics CNC parts.
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FAQ
What sheet metal fabrication tolerances can I expect?
Standard sheet metal fabrication tolerances are ±0.10–0.20 mm on laser-cut flat features, ±0.25–0.50 mm on formed flange lengths, and ±0.5–1.0 degrees on bend angles. Dimensions spanning multiple bends accumulate to roughly ±0.8–1.6 mm worst case. Anything tighter than ±0.05 mm requires a secondary machining operation after forming. General untoleranced dimensions default to ISO 2768-m when the standard is invoked on the drawing.
What is the minimum bend radius for aluminium and stainless?
For aluminium 5052-H32 the minimum inside radius is about 0.5 × thickness. For 6061-T6 it is 1.0 × thickness — T6 cracks at tighter radii unless the material is annealed first. For 6063-T5, 1.0 × thickness. For stainless 304 and 316, 0.5–1.0 × thickness depending on temper, with higher springback than steel. Always specify the inside radius on the drawing; do not leave it to the shop's default tooling.
Why is my flat pattern the wrong size after bending?
Almost always a K-factor error. The K-factor sets the position of the neutral axis, and a wrong value changes the material length consumed by each bend. A K-factor error of 0.05 produces roughly 0.3–0.5 mm of error per 90-degree bend in 2 mm steel, which compounds on multi-bend parts. The fix is to bend a test coupon, measure the actual consumed length on a CMM, and correct the CAD default before releasing production.
When should a feature be machined after forming instead of formed?
In custom sheet metal fabrication, machine after forming whenever the feature carries a bearing or press fit, must be coaxial with a formed flange, must be flat as a sealing face, or needs hole-to-hole accuracy tighter than about ±0.1 mm across three or more bends. Leave features as-formed when they are clearance holes for standard fasteners or cosmetic cut-outs. A post-form machining operation typically adds 10–25% to the fabricated part price for a small bracket — usually less than the cost of one rejected assembly.
Does powder coating or anodizing change part dimensions?
Yes, and it is routinely overlooked. Powder coating at 60–120 µm per surface reduces a Ø6.00 mm hole to roughly 5.76–5.88 mm and renders uncoated threads unusable. Type III hard anodizing at 25–50 µm grows a bore by 50–100 µm on diameter, enough to convert a light press fit into an interference. Type II decorative anodizing at 5–15 µm changes a Ø6 mm hole by only 0.01–0.03 mm. Mask threads and bores before coating, and state the inspection state — before or after coating — on every dimension that matters.
What is the smallest hole a fiber laser can cut?
As a rule, one times the material thickness for a clean cut: 2 mm holes in 2 mm sheet, 3 mm holes in 3 mm sheet. Below that ratio the beam struggles to clear dross and hole roundness suffers, so the practical answer is to drill or ream instead. Narrow slots behave similarly — 0.8 × thickness is the working minimum, 1.2 × thickness is comfortable.
When is sheet metal fabrication cheaper than CNC machining?
Whenever the part is essentially a constant-thickness shell: a bracket, panel, chassis or cover with holes and bends. Fabrication uses far less material, removes far less metal, and needs no long cycle time per part. CNC machining becomes the cheaper route when the part needs significant three-dimensional geometry, very tight tolerances, or features that cannot be formed at all. Many production parts are best served by combining both, and it is worth costing that hybrid route against either process alone — the cost structure differences are covered in our CNC machining cost guide.
Do you provide FAI and PPAP documentation for fabricated parts?
Yes. First Article Inspection with a ballooned drawing and measured results is standard for new parts and for any change in tooling or process. PPAP packages are available for IATF 16949 programmes at the level agreed at award. Medical work is documented to ISO 13485 expectations, including process validation records where the programme requires them. Material certificates to EN 10204 3.1 ship with the parts.
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Getting your next fabricated part quoted
Custom sheet metal fabrication is a predictable process once the drawing describes what the process can actually do, and custom sheet metal parts fail on the drawing far more often than on the shop floor. Three things do most of the work: put tight tolerances only where function needs them, decide feature by feature whether a dimension should be formed or machined, and state the inspection state relative to coating.
If you want a second opinion on a design before you commit tooling or volume, send us the model, the drawing and the volumes. We run production across CNC turning, milling, five-axis machining, precision stamping, sheet metal fabrication and surface treatment in one facility in Dongguan, which means a hybrid part stays in one process chain rather than being split across three suppliers. Most quotes go out within 24 hours when the RFQ includes a 3D model, a dimensioned drawing, the material and finish specification, and the required documentation level — and our sheet metal fabrication service page lists the process envelope in detail.
Request a quote or send your drawings to gongtianbao@xhlmarketing.com.