CARBON STEEL & ALLOY STEEL · MATERIAL EXPERTISE

Machined Carbon Steel and Alloy Steel Parts for Load-Bearing Work

Carbon Steel is what most mechanical structures are actually made of, and C45 is the grade that carries the load. XS Precision machines both sides of that choice — plain carbon steel where the section is thin enough to harden through, Alloy steel such as 42CrMo4 where it is not.

The properties that put steel on the drawing are High strength, a Cost-effective bar price and Good machinability in the annealed and normalised conditions. The property that decides whether you get all three is hardenability, and that is a question about diameter, not about the grade name.

Bundles of hot-rolled carbon steel round bar in warehouse racks, dark blue-grey mill scale surfaces, sawn circular ends showing bright cut faces, steel banding and wired paper mill tags

Hot-rolled carbon steel bar, sawn and tagged before it reaches a machine

THROUGH-HARDENED
SOFT CORE
≤20–25 mm · water quench>25 mm · core stays soft50–75 mm · 42CrMo4
C45 BY THE NUMBERS

C45 carbon steel: the six numbers that decide the drawing

C45 (EN 1.0503, AISI/SAE 1045, JIS S45C, GB 45#) is a medium-carbon structural steel with nominally 0.45% carbon. Mills routinely dual-certify the same heat to all four standards, so the grade names are interchangeable in practice. What is not interchangeable is the section size.

0.42–0.50
WT% CARBON
The medium-carbon window. Enough carbon to quench harden, not so much that it cracks on the way.
620
MPa · Rm AS NORMALISED
Tensile strength in the +N condition at sections up to 16 mm.
700–850
MPa · Rm AFTER Q&T
Quenched and tempered C45 reaches this band, with Re ≥490 MPa.
55–60
% MACHINABILITY
Indexed against 1212 free-cutting steel at 100. Carbide tooling, no drama.
≤207
HB · SOFT ANNEALED
The +A ceiling. This is the condition to machine in when tolerances are tight.
20–25
mm · CRITICAL DIAMETER
Water-quench limit. Past it the core never becomes martensite.
GOOD MACHINABILITY, CONDITIONALLY

Good machinability is a property of the heat treatment, not the grade

The handbooks quote one machinability number for C45. The shop sees three, because the same bar behaves differently depending on what the mill or the heat treater did to it before it arrived.

Soft annealed C45 at 160–190 HB is the easiest thing on this page to cut: the chips break, the cutting forces are low, and the surface finish comes out clean in one pass. Normalised C45 at 170–220 HB is a little tougher because the pearlite is finer, but it is still routine on carbide. Quenched and tempered C45 is the one that changes the plan — from roughly 250 HB upward, tool wear and cutting forces both climb, and the feed and speed have to come down to protect the tolerance you are trying to hold.

Turning speeds that work on C45

With coated carbide in the normalised or annealed condition: turning 240–330 m/min, milling 150–205 m/min, parting off 115–155 m/min, grooving 135–185 m/min, drilling 95–130 m/min. In the quenched and tempered state, drop the turning speed by roughly a third and expect to spend tool life instead of cycle time. Above 45 HRC C45 leaves carbide behind and wants ceramic or CBN, which is usually the point at which grinding becomes the cheaper option.

The one process change that pays
Machine in the soft condition, heat treat, then take a light finishing cut. It sounds like an extra operation and it is — but it is cheaper than holding a tight tolerance through a furnace cycle, and it is the only reliable way to reach ±0.01 mm on a hardened feature. At XS Precision the roughing operation leaves 0.25–0.40 mm of stock on every surface that will be finished after hardening; the distortion has to come out of somewhere.
STOCK ALLOWANCE
0.25–0.40 mm on surfaces that will be ground or finish turned after hardening. Add 1.0–1.5 mm per surface on forged or heavily distorted geometry.
WHEN CARBON STEEL IS THE WRONG ANSWER

Past 25 mm, the carbon steel stops being high strength and starts being a case

Use C45 for Load-bearing parts and the single most expensive mistake is specifying it on a section too thick to harden. Water quenching gives a critical diameter of about 20–25 mm for a 50% martensite core. A 60 mm shaft quenched in water has a hard skin and a soft centre, and the fatigue life you designed for belongs to the skin only.

That is the boundary where Alloy steel earns its price. Adding chromium and molybdenum — 42CrMo4 in EN, 4140 in AISI, SCM440 in JIS — pushes the through-hardening diameter from about 20 mm to somewhere between 50 and 75 mm, lifts the quenched and tempered strength to 900–1100 MPa, and improves toughness at the same hardness. The bar costs roughly 1.5 times as much as C45 and welds less willingly, which is exactly the trade you are making.

C45
EN 1.0503 · AISI 1045 · S45C
⌀ 20–25 mm
700–850 MPa
The default carbon steel for shafts, pins, sprockets and structural parts up to about 60 mm, and the cheapest route to High strength. Induction or flame hardening the surface reaches 55–58 HRC over 1.5–5 mm while the core stays tough.
C45E
EN 1.0503 · cleaner phosphorus
⌀ 20–25 mm
700–850 MPa
The same steel with phosphorus held to 0.030% instead of 0.045% and guaranteed impact energy. Mills charge a 5–8% premium for the tighter chemistry and the impact test. Specify it when the part sees shock or when the end user asks for a guaranteed Charpy value.
42CrMo4
EN 1.7225 · AISI 4140 · SCM440
⌀ 50–75 mm
900–1,100 MPa
Chromium 0.90–1.20% with molybdenum 0.15–0.30%. This is the step that lets a large section harden through, and the reason 4140 in the pre-hardened 28–32 HRC condition is the standard bar for mould bases and fixture plates. Nitriding takes the surface to 600–800 HV with almost no distortion.
40CrNiMoA
AISI 4340 · 34CrNiMo6
⌀ 80–100 mm
1,100–1,300 MPa
Nickel added for toughness at high strength. Reserved for sections the Cr-Mo grades still cannot carry, or where a part has to survive impact at 1,000 MPa and above. Cost and machining time both jump, so it needs a functional reason rather than a habit.
WHERE IT GOES

Mechanical structures and Load-bearing parts, in carbon and alloy steel

Mechanical structures and Load-bearing parts are what this page is for: the frames, plates, brackets, housings and shafts that hold a machine together and take the force. With Alloy steel kept in reserve for the sections that need it, three groups cover almost every drawing that arrives.

Machined carbon steel mechanical structures on a fabrication bench: mounting plates with a large central bore and a ring of bolt holes, gusseted L brackets and a pillow block bearing housing
01
STRUCTURAL / STATIC
Frames, plates and machined structures
Mounting plates with a bored centre and a bolt circle, gusseted corner brackets, base plates, tie bars and machine frames. These are the parts where Cost-effective matters most and where flatness, hole position and thread quality carry the function. Welded assemblies are normalised after welding so the machining does not release locked-in stress.
Typical gradesC45 · S355 · 42CrMo4
Delivery condition+N or +A
Hole position±0.05 mm
FinishingBlack oxide · primer
Finished machined C45 carbon steel stepped shafts on a workshop bench, each with shoulder fillet radii, milled keyways, centre-drilled ends and threaded sections
02
ROTATING / FATIGUE-LIMITED
Shafts, spindles and axles
The parts where the material choice and the geometry fight each other. A shoulder, a keyway or a press fit each concentrate stress by a factor of 1.4 to 3, and every one of them is a place a fatigue crack can start. Diameter steps get a real fillet radius, keyways get an end radius, and the journals that will be ground keep their stock allowance through heat treatment.
Typical gradesC45 · C45E · 42CrMo4
Delivery condition+QT · 210–250 HB
Runout on journals0.01–0.02 mm
SurfaceGround · induction hardened
Steel turned parts in three trays showing black oxide, nitrided and untreated machined surface finishes side by side for comparison
03
WEAR-FACING / PRECISION
Pins, bushings, gear blanks and collars
Smaller Load-bearing parts that need a hard surface and a tough core. Induction hardened journals, nitrided gear flanks, black-oxided pins and chrome-plated hydraulic rods. Nitriding is the one to reach for when the part is already finished to size: it runs at 500–550 °C, so it hardens the surface to 600–800 HV without the dimensional movement a quench would introduce.
Typical gradesC45 · 42CrMo4
Surface hardness55–58 HRC · 600–800 HV
Case depth0.2–0.6 mm
FinishingNitride · hard chrome · black oxide
WHERE LOAD-BEARING PARTS ACTUALLY BREAK

Four features cause most fatigue failures in steel shafts

Rotating parts fail from fatigue, not from being overloaded once. The bending stress reverses every revolution, the crack starts at the surface, and it starts wherever the geometry interrupts the load path. The stress concentration factor Kt tells you how much worse than nominal the local stress is. The circle on each card is drawn to scale against that number. These four features account for most of the fatigue failures XS Precision sees on returned steel shafts.

2.5–3.0
01Kt shaft shoulder, sharp corner
Diameter step with no fillet
A sharp 90° corner at a diameter change is the single most common fracture origin. Kt falls towards 1.5 as the radius grows, so the cheapest fatigue improvement available on any drawing is a larger fillet. Aim for r/d ≥ 0.1 — on a 30 mm shaft that means R3 minimum — and keep the large-to-small diameter ratio at or below 1.5.
1.6–3.0
02Kt keyway, end-milled corner
Keyway cut into a rotating shaft
A keyway removes cross-section and adds a sharp internal corner in the same place. The semicircular end reaches roughly 2.5 times the nominal shear stress at about 50° to the axis, which is exactly where shafts are found broken. ASME deals with it bluntly: reduce the allowable shear stress by 25% wherever the shaft is keyed, and use an end radius of at least half the keyway width.
1.3–1.8
03Kt press fit, bearing seat
Interference fit edge and bearing shoulder
A press fit creates a fretting-fatigue hotspot at the edge of the fit even with no geometric notch at all. Two rules keep it under control: break the edge at the start of the fit zone so the bearing does not scrape its way on, and keep the shaft fillet radius smaller than the bearing bore chamfer so the bearing seats against the shoulder rather than the radius. Shoulder height of 3–5% of the bore diameter is the working range.
1.2–2.0
04Kt groove, undercut, oil hole
Retaining-ring grooves and thread reliefs
Every groove is a notch. Circlip grooves, thread relief undercuts and cross-drilled oil holes all concentrate stress, and they are usually placed wherever the assembly needed them rather than wherever the moment is lowest. Radius the groove flanks, move it away from the high-moment section if the assembly allows, and treat the last thread run-out as a notch rather than as a detail.
Finished machined C45 carbon steel stepped shafts on a workshop bench, each with shoulder fillet radii, milled keyways, centre-drilled ends and threaded sections

Machined C45 shafts: shoulder fillets, milled keyways and centre-drilled ends — the three features that decide fatigue life

HEAT TREATMENT, IN ORDER

The route matters more than the temperature on the ticket

A heat treatment specification that names only a hardness number leaves the shop to invent the sequence, and the sequence is what determines whether the part comes out on size. Quenching does three things at once: it sets the structure, it sets the residual stress, and it moves the geometry. Only the first of those is on the drawing.

Why the shaft was straight on the lathe and is not straight now

Machining removes material and redistributes internal stress; heat treatment changes the structure of what is left. A slender shaft can come out of the quench with 0.1–0.3 mm of bow per metre, and a part with shoulders, keyways and uneven section thickness will move more than a plain cylinder because it does not heat and cool evenly.

The answer is not to try to quench it straight. It is to plan the distortion: leave grinding stock on the controlled diameters, specify the straightness requirement against a stated datum and a stated length, and put straightening between hardening and final grinding where it can be measured and proved. Cold straightening of hardened steel is limited — past roughly 0.020 inch per foot of bow the part is more likely to fracture than to come back — and it has to be done below the tempering temperature or the martensite is locally re-tempered.

150°C
~64 HRC
250°C
~56 HRC
350°C
~48 HRC
450°C
~38 HRC
550°C
~30 HRC
650°C
~24 HRC
STEP 1
Rough machine
leave 0.25–0.40 mm
Remove the bulk with the steel soft. Keep the stock on every surface that will be finished after hardening.
STEP 2
Heat treat
820–860 °C
Quench in water for simple thin sections, oil for complex or thick ones. Temper at 550–660 °C for quenched and tempered properties.
STEP 3
Straighten
measure, press, re-measure
Only if the part moved. Done cold and below the tempering temperature, against the drawing datum.
STEP 4
Finish machine
±0.01 mm available
Light cuts with carbide on the hardened skin, or cylindrical grinding where the tolerance and finish demand it.
STEP 5
Inspect
report at a stated temperature
Dimensions, runout, hardness and the heat number all recorded against the same part.
A wire mesh basket of glowing red-hot steel shafts, rings and gear blanks being lowered on a crane hook towards an open oil quench tank in a heat treatment shop

Heat treatment of C45 parts at the quench: structure, residual stress and geometry are all set in the same operation

THE THREE THINGS THAT GO WRONG

Quench cracking, soft cores and a certificate that does not travel

01
Quench cracking and distortion
Water quenching C45 gets the highest hardness and the highest risk in the same operation. Cracks start at sharp corners, at abrupt section changes and where a heavy section meets a thin one, because those are the places where the surface transforms and the core does not. Sharper quench media make it worse — water is riskier than oil, salt bath is the mildest of the three. The design-side fixes are a generous fillet on every corner, symmetric geometry, and wall sections that do not step from thick to thin in one move. The process-side fix is the right medium for the geometry in front of you rather than one setting for the whole shop.
02
A core that never hardened
Hardness measured at the surface says nothing about the middle. Under-austenitising, too short a soak, too slow a quench, too large a section, decarburisation or a quench medium chosen without regard to the part’s shape all produce a part that looks hardened and is not. Section thickness is the one that catches people out, because it is invisible on the inspection report. Below the critical diameter C45 hardens through; above it you have a case and a soft core, and no amount of hardness testing at the surface will show you.
03
A certificate that does not reach the part
The material risk when sourcing steel is rarely outright fraud and usually near-equivalent substitution: 1045 in place of C45E, a Q235 heat certified against a Q355 order, 4140 chemistry that did not get the heat treatment the drawing asked for. An EN 10204 3.1 certificate with the heat number matched to the stamp on the bar, a positive material identification check on receipt, and a hardness test on the finished part are three cheap independent checks, and each one catches a different failure. What none of them catches is a genuine certificate attached to the wrong bundle.
Long continuous steel turning chips tangled in the chip tray of a CNC lathe, temper colours from straw to blue, with the tool holder and carbide insert at the edge

The swarth from turning C45: long continuous chips with temper colours from straw to blue, the same colours the temper scale above is drawn from

SURFACE, WHERE STEEL LOSES FIRST

Carbon steel has no corrosion resistance, so the finish is a specification

Carbon steel and Alloy steel are both structural materials, not corrosion materials. Left bare in a damp workshop or a coastal installation, C45 will rust, and a rusted bearing seat is a tolerance that no longer exists. Every drawing that leaves the shop needs either a finish on it or a stated reason why it can be left bare.

The finishes differ mainly in what they do to the dimension. Black oxide builds a conversion layer of 1–2 µm and changes nothing — it is the default for tooling, fasteners and parts that are already at final size, and it carries no hydrogen embrittlement risk. Hard chrome builds 10–30 µm of 800–1000 HV material and is what keeps a hydraulic rod from wearing out, but high-strength steel must be baked at 190–220 °C for at least four hours after plating to drive out the hydrogen. Nitriding changes no dimension of consequence either, at the cost of a matte grey surface that cannot be machined afterwards.

DO NOT WELD A HARDENED SURFACE
C45 with a carbon equivalent of 0.55–0.65% hardens in the heat-affected zone and cracks without precautions. Preheat 200–300 °C, use low-hydrogen electrodes, control interpass temperature, and stress relieve at 550–650 °C afterwards. Weld in the normalised condition rather than the quenched and tempered one — and never weld a surface that has already been induction or flame hardened.
Steel turned parts in three trays showing black oxide, nitrided and untreated machined surface finishes side by side for comparison

Black oxide, nitrided and untreated machined steel parts, compared side by side

WHAT YOU ARE ACTUALLY PAYING FOR

Cost-effective does not mean the cheapest bar per kilogram

Hot-rolled 45# round bar out of a Chinese mill was trading around US$550–680 per tonne FOB through 2026, with C45E carrying a 5–8% premium for the tighter phosphorus limit and the guaranteed impact test. US-produced 1045 sits at US$850–1,100 per tonne and 42CrMo4 at roughly US$750–760.

Those numbers are real and they are also only part of the story. On a finished machined part, the bar is usually less than half the cost. The rest is cutting time, tool life, fixturing and inspection — which is why a material with a 55–60 machinability index and a predictable heat treatment is often cheaper than a cheaper bar that machines badly or moves in the furnace. Reading a quote means reading the process, not just the material line.

One lever that drawings forget: bar diameter. C45 is stocked in a wide range of sizes, so choosing a nominal diameter that matches the stock rather than forcing a special size removes roughing time and swarf from the job before it starts. XS Precision runs that comparison at the quotation stage rather than after the first article.

$550–680
US / TONNE FOB
Hot-rolled 45# round bar, Chinese mill, standard rolled lengths, 2026.
+5–8%
C45E PREMIUM
For phosphorus held at 0.030% and a guaranteed Charpy value.
×1.5
42CrMo4 vs C45
The price of being able to harden a section larger than 25 mm.
≈50%
OF PART COST IN THE BAR
The other half is cutting time, tooling and inspection.
MATERIAL$550–680 / t
PROCESSCutting · tooling · heat treat · inspection
Indicative split on a machined C45 part in low-volume production. The material line is the one that is easy to compare between suppliers and the one that matters least to the final price. Ask what condition the bar arrives in, how many operations the part takes, and whether heat treatment and straightening are inside the quoted route — two suppliers can price the same drawing very differently and both be honest about it.
WHAT TRAVELS WITH THE PARTS

Certificates, traceability and the check that is worth the money

EN 10204 defines four inspection document types, and the difference between them is who did the testing and whether the paperwork can be tied to the piece in your hand. Naming the type on the purchase order rather than asking for a general material certificate is the difference between documentary comfort and traceability.

2.1BASIC
Declaration of compliance
A statement that the material meets the order. No test results, no heat number. Fine for non-critical commercial work and nothing else.
2.2BASIC
Mill test report
Non-specific inspection with the mill’s own test results. Common on general industrial stock, but it does not tie the results to a particular heat.
3.1REQUIRED
Inspection certificate 3.1
Issued by the mill with the heat number and the actual chemistry and mechanical results. This is the type to put on the purchase order for any load-bearing part.
3.2REQUIRED
Inspection certificate 3.2
As 3.1, plus independent verification by a nominated third party. Required for aerospace, nuclear and pressure-equipment supply chains.

A 3.1 certificate is worth exactly as much as its link to the delivered part. The heat number on the certificate has to match the stamp on the bar, and the bar has to be the one the part was cut from. If those three do not line up, the lot is mixed and the honest answer is to sort it before shipment rather than to explain it afterwards.

Two checks catch most of what goes wrong. Positive material identification with a handheld analyser takes about thirty seconds per sample and catches the near-equivalent substitution that paperwork cannot. A hardness test on the finished part is the cheapest way to prove that the heat treatment named on the drawing actually happened, because a C45 part that should read 250 HB and reads 170 HB did not get quenched and tempered, whatever the route sheet says. XS Precision records the heat number against every part in the lot rather than against the shipment as a whole.

A stepped steel shaft supported in V-blocks on a granite surface plate while a dial indicator measures a journal, with a vernier caliper and a blank inspection form

Dimensional inspection of a stepped steel shaft in V-blocks, with the heat number recorded against the part

CHOOSING BETWEEN THEM

Carbon Steel or Alloy steel: the questions that decide it

Four questions settle most of these decisions before the drawing goes out. Answer them in order and the grade usually chooses itself.

IF THE PART…THEN
Loads a section under 25 mm and needs strength after heat treatmentC45 quenched and tempered. You will get 700–850 MPa and a core that actually hardened.
Loads a section over 25 mmMove to 42CrMo4. C45 will only harden the skin, and you will be paying for strength the core does not have.
Needs a hard surface on a finished sizeNitride a 42CrMo4 part at 500–550 °C, or induction harden C45 before the final grind where the geometry allows it.
Sees shock or impact at high strengthEither C45E with its guaranteed impact energy, or a nickel-bearing Alloy steel such as 40CrNiMoA if the section is also large.
Has to be weldedWeld before hardening, preheat 200–300 °C, use low-hydrogen consumables and stress relieve afterwards. If welding is central, a low-carbon steel is the better structural answer.
Faces chlorides or a wet environmentNeither grade is a corrosion material. Specify a coating, or move the part to stainless steel and accept the machining cost.
THREE MISTAKES TO AVOID

What we would change before the drawing is released

A hardness number with no delivery condition
“C45, HRC 32” tells the shop the destination and nothing about the route. It does not say whether the bar arrives annealed or pre-hardened, whether the part is machined before or after hardening, or where the stock allowance goes. A drawing that names the condition — +A, +N, +QT &mdash and the sequence will get a quote that can be compared with another one, and a part that measures the same twice.
A thick section specified from a thin-section success
A 20 mm pin in C45 that ran for years in one machine is not evidence that a 70 mm shaft will behave the same way. Hardening depth does not scale with the drawing; it scales with the quench and the alloy. Scale the section and the material decision has to be revisited, not carried forward.
Final size specified on a surface that will be hardened
Quenching moves the part, and every tolerance that is already used up cannot absorb the movement. Put the tight tolerances on features that are finished after heat treatment, add the stock allowance on the surfaces that are not, and state the straightness or runout requirement against a datum so it can be measured after the furnace rather than assumed before it.
QUESTIONS WE GET

Carbon steel and alloy steel questions, answered before the quote

For practical purposes, yes. C45 (EN 1.0503) has a carbon window of 0.42–0.50% with manganese 0.50–0.80%; AISI/SAE 1045 is 0.43–0.50% with manganese 0.60–0.90%; JIS S45C sits in the same band with a higher manganese ceiling and tighter impurity control. Mills routinely dual- or triple-certify one heat to all three. C45E is the cleaner European version, with phosphorus held to 0.030% instead of 0.045% and a guaranteed impact value.

Because the material moved, which is normal, and because the route had nowhere to correct it. Slender shafts commonly bow 0.1–0.3 mm per metre through a quench, and parts with shoulders, keyways or uneven section thickness move more than a plain cylinder. The controlled answer is to leave grinding stock on the critical diameters, harden, measure against a stated datum, straighten cold and below the tempering temperature if needed, then grind to size. Finishing every journal before hardening and hoping is the one route that has no way back.

When the load-bearing section is thicker than roughly 25 mm. That is the practical limit of C45’s hardenability in water — below it the part harden through, above it you get a hard case and a soft core. Chromium and molybdenum in 42CrMo4 push the through-hardening diameter to 50–75 mm and lift the quenched and tempered strength to 900–1,100 MPa. You pay about 1.5 times the bar price, a little machinability and a lot more care when welding.

Yes, by taking the tolerance off the hardened condition. Finish features to ±0.01 mm after heat treatment with light carbide cuts, or grind them, and leave 0.25–0.40 mm of stock on those surfaces through the furnace. Above 45 HRC, expect the realistic capability to open up to ±0.02–0.05 mm and grinding to become the cheaper route. What does not work is specifying a tight tolerance on a feature that is already at final size before quenching.

Something, unless there is a stated reason not to. Black oxide is the default where the part is already at final size because it builds 1–2 µm and changes nothing. Hard chrome gives 800–1000 HV and 10–30 µm of wear-resistant material on rod and pin surfaces, with a 190–220 °C bake afterwards to remove hydrogen. Nitriding reaches 600–800 HV with minimal distortion but leaves a matte grey surface that cannot be machined, so it has to be the last operation. XS Precision will name the finish and the thickness on the quotation so the dimension stack can be checked before the parts are cut.

Yes. Every order ships with an EN 10204 3.1 inspection certificate carrying the heat number, with that number matched to the stamp on the bar the parts were cut from, plus a dimensional report at a stated measurement temperature. Positive material identification and hardness verification on finished parts can be added to the route where the application justifies them. If your end user requires 3.2 with independent third-party verification, say so at the RFQ stage rather than at shipment.

WHERE TO GO NEXT

Related capability and material pages to read next

Precision CNC machining

Turning, milling and drilling on carbon and alloy steel, with the speeds, tooling and heat treatment sequence described above.

High-precision components

Bores, threads and ground journals held on hardened steel, with the dimensional report to match.

Brass and copper against steel

The other side of the same decision — where conductivity and machinability beat strength and cost.

Send the drawing. We will tell you which grade fits.

A STEP file, the section thickness at the load-bearing features and the service environment are enough to start. If the section is too thick for C45, or if a coating is the wrong answer for the environment, you will hear that before the quote rather than after the parts arrive.

Or send the drawing to info@xsprecisiontech.com with the grade, the delivery condition and the quantity, and we will come back with the machining route, the heat treatment sequence, the tolerance we can hold and the certificate package.

Request a quote today!