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Home/ Materials/ Nickel-Based Alloys — Inconel 625 / 718 · Hastelloy C-276 · Monel 400
Nickel-Based Alloy CNC Machining

Nickel Alloy
CNC Machining

Inconel 625 Inconel 718 Hastelloy C-276 Monel 400 Aerospace · Chemical · Marine

Precision CNC machining of nickel-based superalloys for aerospace, chemical processing, oil & gas, and marine applications demanding extreme temperature resistance, corrosion resistance, and high-strength performance where stainless steel is insufficient.

Nickel Alloy Inconel Hastelloy Monel CNC Machined Parts
Max Service Temp
982 °C
4 Grades
In625 / In718 / C-276 / Monel
982°C
Max Service Temperature
1380MPa
Inconel 718 Tensile Strength
24hr
Quote Turnaround
Inconel 625 Inconel 718 Aerospace Hastelloy C-276 Chemical Monel 400 Marine High-Pressure Coolant Machining Ceramic & PCBN Tooling Turbine Components Subsea & Offshore Parts Valve Seats · Nozzles · Flanges Inconel 625 Inconel 718 Aerospace Hastelloy C-276 Chemical Monel 400 Marine High-Pressure Coolant Machining Ceramic & PCBN Tooling Turbine Components Subsea & Offshore Parts Valve Seats · Nozzles · Flanges
Material Grades

Four Nickel Alloys, Four Different Demands

IN625
UNS N06625 · ASTM B446 / B564 · AMS 5666
Solution-Strengthened Nickel-Chromium-Molybdenum Alloy
The industry-standard nickel alloy for seawater, chemical, and cryogenic service. Niobium additions provide solid-solution strengthening and outstanding corrosion resistance across a wide temperature range — from cryogenic (-196 °C) to 982 °C. Excellent weldability and resistance to stress corrosion cracking in chloride environments. The most widely specified nickel alloy for subsea, marine, and chemical processing components.
930 MPa
Tensile Strength
414 MPa
Yield Strength
−196–982°C
Service Range
HRB 98
Hardness
Subsea ConnectorsChemical ValvesCryogenic PartsMarine FlangesHeat Exchanger Tubes
View Inconel 625 Details
Chemical Composition
Nickel (Ni)58% min (bal.)
Chromium (Cr)20.0–23.0%
Molybdenum (Mo)8.0–10.0%
Niobium + Ta3.15–4.15%
Iron (Fe) max5.0%
Carbon (C) max0.10%
Key Properties
Exceptional resistance to seawater, chloride pitting, and crevice corrosion
Excellent weldability — retains corrosion resistance in the weld HAZ
Cryogenic toughness — suitable down to −196 °C
Not precipitation-hardenable — strength fixed by composition
More machinable than IN718 — carbide tooling standard
IN718
UNS N07718 · AMS 5662 / 5664 · ASTM B637
Precipitation-Hardened Nickel-Chromium-Molybdenum-Niobium Alloy
The most widely used aerospace superalloy — accounting for over 50% of all jet engine superalloy usage. Age-hardened by gamma-prime and gamma-double-prime precipitates, Inconel 718 achieves tensile strength up to 1380 MPa with outstanding fatigue resistance. Maintains mechanical integrity at temperatures up to 650 °C (700 °C for short durations). The most challenging of the four alloys to machine — work-hardening rate is high and ceramic tooling is required for roughing.
1380 MPa
Tensile Strength
1172 MPa
Yield Strength
to 700°C
Service Temp
HRC 36–46
Hardness (aged)
Turbine DiscsJet Engine PartsAerospace FastenersRocket ComponentsDownhole Tools
View Inconel 718 Details
Chemical Composition
Nickel + Cobalt50.0–55.0%
Chromium (Cr)17.0–21.0%
Niobium + Ta4.75–5.50%
Molybdenum (Mo)2.8–3.3%
Titanium (Ti)0.65–1.15%
Aluminum (Al)0.20–0.80%
Key Properties
Highest strength of the four alloys — precipitation-hardened
Outstanding fatigue and creep resistance at elevated temperature
Usually machined in annealed or solution-treated condition, then aged
Ceramic inserts + PCBN for finishing — most difficult nickel alloy to machine
Work-hardening is the primary machining challenge — no dwell at any stage
C-276
UNS N10276 · ASTM B574 / B575 · AMS 5750
Nickel-Molybdenum-Chromium Alloy — Maximum Chemical Resistance
Hastelloy C-276 is engineered for one purpose: superior corrosion resistance in the most aggressive chemical environments on earth. Its high molybdenum content (15–17%) provides exceptional resistance to pitting, crevice corrosion, and stress corrosion cracking in oxidizing and reducing acids simultaneously — a capability no stainless steel or standard Inconel grade can match. The material of choice for chemical reactor internals, scrubbers, and FGD systems where mixed acid and chloride exposure is unavoidable.
790 MPa
Tensile Strength
355 MPa
Yield Strength
to 1040°C
Service Temp
HRB 100
Hardness
Reactor InternalsScrubber ComponentsAcid Pump PartsFGD SystemsChemical Fittings
View Hastelloy C-276 Details
Chemical Composition
Nickel (Ni)Balance (≥57%)
Molybdenum (Mo)15.0–17.0%
Chromium (Cr)14.5–16.5%
Iron (Fe)4.0–7.0%
Tungsten (W)3.0–4.5%
Carbon (C) max0.01%
Key Properties
Resists both oxidizing AND reducing acids — unique dual capability
Ultra-low carbon (0.01% max) — no carbide sensitization after welding
Outstanding chloride pitting and crevice corrosion resistance
Resists hydrochloric, sulfuric, nitric, hydrofluoric, and mixed acids
Harder to machine than IN625 — tungsten/Mo phases accelerate tool wear
M400
UNS N04400 · ASTM B164 / B165 · AMS 4574
Nickel-Copper Alloy — Seawater, Brine & HF Acid Resistance
The simplest and oldest commercial nickel alloy — approximately 67% Ni and 31% Cu. Monel 400 offers excellent corrosion resistance in seawater, brine, hydrofluoric acid, and alkaline environments at a lower cost and with significantly better machinability than Inconel or Hastelloy grades. It is not heat-treatable to high strength levels but is stronger than copper and significantly more corrosion resistant than stainless steel in marine environments. The standard material for marine pump shafts, impellers, propeller shafts, and HF acid handling equipment.
550 MPa
Tensile Strength
240 MPa
Yield Strength
to 480°C
Service Temp
HRB 65–85
Hardness
Marine Pump ShaftsPropeller ShaftsHF Acid ValvesHeat Exchanger TubesBrine Fittings
View Monel 400 Details
Chemical Composition
Nickel + Cobalt≥63% (min)
Copper (Cu)28.0–34.0%
Iron (Fe)2.5% max
Manganese (Mn)2.0% max
Silicon (Si) max0.50%
Carbon (C) max0.30%
Key Properties
Excellent seawater and brine corrosion resistance — outperforms 316 SS
Exceptional HF (hydrofluoric) acid resistance — unique capability
Best machinability of the four alloys — closer to stainless than Inconel
Lower cost than Inconel — economical for large or high-volume parts
Not suitable for high-temperature service above 480 °C
Grade Selection Guide

Choosing the Right Nickel Alloy

🌊
Choose Inconel 625 when…
Seawater, subsea, or offshore environment
Cryogenic service (down to −196 °C)
Weldability is important (piping, overlays)
Chemical process equipment in chloride environments
Moderate temperature service up to 982 °C
Choose Inconel 718 when…
Aerospace, turbine, or jet engine application
Maximum strength (up to 1380 MPa) required
High fatigue and creep resistance at temperature
Downhole oil & gas tooling and wellhead components
Space and rocket propulsion components
Choose Hastelloy C-276 when…
Aggressive mixed acid environments (HCl + H₂SO₄)
Chemical reactor internals and scrubber systems
Both oxidizing AND reducing acid exposure simultaneously
Flue gas desulfurization (FGD) components
When IN625 corrosion resistance is insufficient
Choose Monel 400 when…
Marine pump shafts, impellers, and propeller shafts
HF (hydrofluoric) acid handling equipment
Seawater and brine service at moderate temperatures
Lower cost nickel alloy for larger or high-volume parts
Alkaline and caustic service environments
Material Comparison

Full Property Comparison — All Four Grades

Property Inconel 625 Inconel 718 Hastelloy C-276 Monel 400 316L SS (ref)
Base System Ni-Cr-Mo-Nb Ni-Cr-Mo-Nb (aged) Ni-Mo-Cr-W Ni-Cu Fe-Cr-Ni-Mo
Tensile Strength 930 MPa Up to 1380 MPa 790 MPa 550 MPa ~485–690 MPa
Yield Strength 414 MPa Up to 1172 MPa 355 MPa 240 MPa ~170–310 MPa
Max Service Temp. 982 °C 700 °C (mech.) 1040 °C 480 °C ~870 °C (ox.)
Seawater / Chloride Excellent Good Excellent Excellent Moderate — pits
Mixed Acid Resistance Good Moderate Best in class Moderate Poor in HCl
HF Acid Resistance Good Fair Good Excellent — unique Poor
Precipitation Hardenable No Yes — to 1380 MPa No No No
Machinability (relative) Moderate — 15–20% of 316SS Hardest — 10–15% of 316SS Moderate — 15–20% of 316SS Best — 25–30% of 316SS 100% (reference)
Primary Application Subsea, cryogenic, chemical Aerospace, turbine, downhole Chemical reactors, FGD, acids Marine, HF acid, brine General corrosion resistance
Machining Notes

Machining Nickel Alloys — What Engineers Need to Know

Challenges with Nickel Alloy Machining
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Extreme work-hardening — especially Inconel 718Nickel alloys work-harden rapidly under cutting forces. Any dwell, rubbing, or re-cutting of already machined surfaces creates a hard surface layer that damages the next cutting edge. Inconel 718 in aged condition has work-hardening rates comparable to austenitic stainless steel at its worst — requiring constant chip engagement.
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Heat concentration at the cutting edgeLow thermal conductivity means heat generated at the tool tip cannot conduct away into the workpiece — concentrating it in the insert. This causes diffusion wear, notching, and chemical attack of the tool coating at a fraction of the cutting speeds used on steel.
!
Abrasive hard phases in C-276 and IN718Hastelloy C-276 contains tungsten-rich and molybdenum-rich intermetallic phases significantly harder than the surrounding nickel matrix. Inconel 718 contains gamma-prime and gamma-double-prime precipitates. Both cause accelerated abrasive wear — carbide tools require very conservative cutting speeds and monitored tool life limits.
!
Built-up edge and adhesion on tool rake facesNickel is chemically reactive with most tool coatings at high temperature. At elevated cutting temperatures, nickel diffuses into carbide substrates and forms a built-up edge — degrading surface finish and causing unpredictable breakout. This makes flood coolant and high-pressure coolant mandatory, not optional.
!
Springback and dimensional variation on thin wallsHigh elastic modulus combined with work-hardening causes nickel alloy parts to spring back more than stainless after each cutting pass — thin walls and complex features require confirmation passes and adjusted programs relative to stainless steel toolpaths.
How We Address These Challenges
Grade-specific tooling strategy for each alloyIN625 and C-276: PVD AlTiN-coated carbide (positive rake, sharp edge). IN718 roughing: SiAlON ceramic inserts (aggressive material removal at controlled speed). IN718 finishing: PCBN inserts for precise dimensional control. Monel 400: uncoated carbide or TiN-coated carbide to prevent built-up edge in the copper-rich matrix.
High-pressure coolant at 70–100 bar on every nickel alloy operationFlood coolant is insufficient for nickel alloys. High-pressure coolant (70–100 bar) directed precisely at the cutting zone manages temperature, breaks chips, and flushes away nickel chips that would otherwise re-cut and damage the surface. Dramatically extends tool life and improves surface integrity.
Continuous cutting — no dwell or re-cutting at any stagePrograms are written with full chip engagement at all times. Tool retracts clear the machined surface before any pause. Corner radii and lead angles chosen to prevent notching at depth-of-cut line. No in-cut pauses regardless of program interruption requirements.
Monitored tool life — inserts changed at intervals, not on failureTool life in nickel alloy machining is managed by cutting time and number of passes — not by visual wear assessment. Inserts are changed at defined intervals before built-up edge or thermal damage occurs. This prevents the batch-to-batch surface quality variation caused by running worn tools.
Machine state and age before post-machining heat treatmentFor IN718 aerospace parts: we machine in solution-treated (soft) condition to tolerance, then coordinate with the customer's heat treat facility or our approved sub-contractor for precipitation hardening (aging at 720 °C + 620 °C). Post-age dimensional verification confirms that aging distortion is within tolerance.
Manufacturing Capability

How We Machine Nickel Alloy Parts

CNC Turning Inconel 625 718 Nickel Alloy Parts
PROCESS / 01
CNC Turning — Shafts, Flanges & Nozzles
Precision CNC turning of Inconel 625/718, Hastelloy C-276, and Monel 400 shafts, flanges, nozzles, and rotational components. Grade-specific insert geometry and high-pressure coolant. Tolerances to ±0.01 mm on precision sealing diameters and bearing journals.
All 4 GradesShafts & FlangesNozzlesHPCO
CNC Milling Hastelloy Inconel Complex Parts
PROCESS / 02
CNC Milling — Housings, Brackets & Valve Bodies
3-axis and 5-axis milling of complex nickel alloy housings, valve bodies, brackets, and structural components. Climb milling strategy to minimise work-hardening. Rigid setups and short tool stick-out mandatory for dimensional control.
5-AxisValve BodiesHousingsClimb Milling
Nickel Alloy Prototype to Production Parts
PROCESS / 06
Prototype to Production Supply
Single-piece prototypes through repeat production orders. Nickel alloy parts are expensive — we treat every piece as a prototype. Process is documented from first article and maintained through production runs to ensure quality consistency across all deliveries.
1 pc PrototypeFAI ReportsProduction Supply
Application Gallery

Typical Nickel Alloy Parts We Produce

Inconel 625 Subsea Connector Flange Inconel 625
Subsea Connectors & Flanges
MaterialIN625 — ASTM B564, NACE MR0175
ProcessCNC Turning · Boring · Threading
IndustrySubsea · Offshore · Oil & Gas
Inconel 718 Aerospace Turbine Disc Inconel 718
Aerospace Turbine & Engine Parts
MaterialIN718 — AMS 5662/5664, aged
Process5-Axis Milling · PCBN Finish · CMM
IndustryAerospace · Defence · Space
Industries Served

Nickel Alloys for Extreme Environments

Aerospace
Inconel 718
Oil & Gas
IN625 / IN718
Chemical
Hastelloy C-276
Marine
Monel 400 / IN625
🔬
Pharmaceutical
C-276 / IN625
Power Gen.
IN625 / IN718
From Raw Billet to Finished Part

How We Produce Nickel Alloy Parts

STEP 01
Material & Cert Verification
IN625, IN718, C-276, or Monel 400 sourced with full MTR. Heat number, chemical composition, and mechanical properties verified before release. Grade-appropriate stock form selected.
STEP 02
Rough Machining
Grade-specific tooling: ceramic inserts for IN718 roughing, AlTiN carbide for IN625/C-276/Monel. High-pressure coolant (70–100 bar) from first cut. Continuous chip engagement — no dwell.
STEP 03
Finish Machining
PCBN finishing on IN718, fresh carbide on IN625/C-276/Monel. Final dimensions, threads, sealing faces, and critical features completed with tool life monitoring and fresh inserts.
STEP 04
Secondary Ops & Heat Treatment
Threading, drilling, secondary milling. IN718 aerospace parts: precipitation aging per AMS 2774. Pressure testing for fluid-service parts. Surface treatment if specified.
STEP 05
Inspection & Delivery
CMM dimensional verification, surface finish, hardness. MTR, inspection report, pressure test record (where applicable), and heat traceability shipped with every order.
Post-Processing

Surface Treatments for Nickel Alloy Parts

Nickel alloy parts are most commonly supplied as-machined — the alloy's inherent corrosion resistance is the primary functional requirement. When additional surface properties are needed, the following treatments are compatible with nickel-based alloys.

Electropolishing
Electrochemical material removal producing ultra-smooth (Ra ≤ 0.2 μm), highly passivated surfaces. Used on IN625 and C-276 chemical and pharmaceutical contact parts to eliminate micro-crevices and maximise corrosion resistance at weld HAZ and machined surfaces.
IN625C-276Pharma GradeRa ≤ 0.2 μm
Passivation
Nitric acid or citric acid passivation to remove free iron contamination from the machined surface and restore the native oxide protective layer. Specified for IN625, C-276, and Monel 400 parts after machining to maximize corrosion resistance and meet ASTM A967 or ASTM B912 requirements.
All GradesASTM A967Citric / Nitric
Shot Peening (IN718)
Controlled shot peening introduces compressive residual stress into Inconel 718 aerospace and fatigue-critical parts — increasing fatigue life in cyclic loading applications. Specified per AMS 2430 or AMS 2432 for jet engine and aerospace structural components where fatigue life improvement is required.
IN718 OnlyAMS 2430Fatigue Life
Bead Blasting & Polishing
Controlled glass bead blasting for uniform matte finish and stress relief on machined surfaces. Mechanical polishing (Ra ≤ 0.4 μm) for sealing faces, bearing surfaces, and flow-critical internal bores where surface finish directly affects sealing performance or fluid flow.
All GradesSealing FacesFlow Surfaces
4
Nickel Alloy Grades
1380 MPa
IN718 Tensile Strength
±0.01mm
Precision Tolerance
24hr
Quote Turnaround
Nickel Alloy CNC Machining Workshop Inconel Hastelloy Monel
Why Work With Us

Why Choose Us for Nickel Alloy Machining

NKL
Four-Grade Nickel Alloy Capability — Not Just One
IN625, IN718, Hastelloy C-276, and Monel 400 all machined in-house with grade-specific tooling strategies. We advise on grade selection before quoting — preventing costly material mistakes on expensive billet.
HPQ
High-Pressure Coolant on Every Nickel Alloy Operation
70–100 bar directed coolant is standard on all nickel alloy jobs — not an upgrade. This is the single most important factor in managing tool life, surface integrity, and dimensional consistency in superalloy machining.
718
Inconel 718 Post-Age Dimensional Verification
We machine IN718 in solution-treated condition, coordinate age hardening, and verify post-age dimensions by CMM — confirming that aging distortion does not push features out of tolerance before shipment.
MTR
Full Material Traceability — MTR, CMM Report, Heat Numbers
Every nickel alloy order ships with complete material test report, heat number traceability, CMM dimensional inspection report, and pressure test records where applicable. No document chasing after delivery.
FAQ

Frequently Asked Questions

Common questions about Inconel 625, Inconel 718, Hastelloy C-276, and Monel 400 — grade selection, machining challenges, tolerances, tooling, and material certification.

Nickel-based superalloys (including Inconel 625, Inconel 718, Hastelloy C-276, and Monel 400) are high-performance alloys based on nickel as the primary element, engineered for extreme heat resistance, corrosion resistance, and mechanical strength at elevated temperatures. They are significantly more difficult to machine than stainless steel or titanium because they work-harden rapidly under cutting forces, have very low thermal conductivity that concentrates heat at the tool tip, and contain hard carbide and intermetallic phases that cause rapid abrasive tool wear. Cutting speeds for nickel alloys are typically 10–30% of those used for stainless steel.
Both are nickel-chromium superalloys but with different strengthening mechanisms and applications. Inconel 625 (UNS N06625) is solution-strengthened with niobium and molybdenum — it has outstanding corrosion resistance, excellent weldability, and good strength at high temperatures, but is not age-hardenable. Inconel 718 (UNS N07718) is precipitation-hardened by niobium and aluminum additions — it has significantly higher tensile strength (up to 1380 MPa in aged condition) and fatigue resistance, making it the dominant aerospace and turbine superalloy. Inconel 718 is harder to machine than 625 due to its higher strength and work-hardening tendency.
Hastelloy C-276 (UNS N10276) is a nickel-molybdenum-chromium alloy engineered specifically for maximum corrosion resistance in aggressive chemical environments. It offers superior resistance to oxidizing acids (nitric, chromic), reducing acids (hydrochloric, sulfuric), and mixed acid conditions — outperforming both Inconel 625 and stainless steel in many chemical service environments. Specify Hastelloy C-276 when the primary requirement is chemical corrosion resistance, especially in chloride-containing, acidic, or mixed oxidizing/reducing environments. For high-temperature aerospace or turbine applications, Inconel 718 is the correct choice.
Monel 400 (UNS N04400) is a nickel-copper alloy (approximately 67% Ni, 31% Cu) — the simplest and oldest commercial nickel alloy. Unlike Inconel (nickel-chromium) and Hastelloy (nickel-molybdenum-chromium), Monel 400 derives its corrosion resistance primarily from the nickel-copper system. It has exceptional resistance to seawater and brine, hydrofluoric acid, and alkaline environments, and is the most machinable of the four alloys. Monel 400 is specified for marine hardware, pump shafts and impellers in seawater service, heat exchanger tubing, and chemical handling equipment — particularly where hydrofluoric acid resistance is required.
Standard tolerance for nickel alloy CNC turning and milling is ±0.02 mm. For precision features (bores, shaft diameters, sealing faces), we hold ±0.010–0.015 mm. Note that nickel alloys spring back more than steel after cutting — particularly Inconel 718 — so final tolerances on tight-fit features require careful process control. CMM inspection reports are provided for all precision nickel alloy components. Tighter tolerances (±0.005 mm) are achievable on selected features with process confirmation — please specify in your drawing.
Nickel alloys require premium cutting tools not used on standard steel or aluminum jobs. We use coated carbide inserts (PVD TiAlN and AlTiN coatings) for general turning and milling, ceramic inserts (SiAlON and whisker-reinforced alumina) for high-speed roughing of Inconel 718, and PCBN (polycrystalline cubic boron nitride) for finishing cuts on hardened Inconel 718. High-pressure coolant (70–100 bar) is directed at the cutting zone on all nickel alloy operations. Tool life is monitored and inserts are changed at defined intervals regardless of visible wear.
Use Inconel 625 for seawater, chemical, and cryogenic applications where corrosion resistance and weldability are primary requirements. Use Inconel 718 for aerospace, turbine, and high-temperature structural applications where maximum strength and fatigue resistance are required. Use Hastelloy C-276 for the most aggressive chemical environments — mixed acids, chloride solutions, and chemical reactors where Inconel 625 would corrode. Use Monel 400 for marine hardware, HF acid service, and applications where a lower-cost, easier-to-machine nickel alloy is acceptable. If unsure, share your operating temperature, fluid or chemical exposure, and mechanical load — we will recommend the correct grade before quoting.
Yes. All nickel alloy orders are supplied with material test reports (MTR) including chemical composition and mechanical properties per the relevant standard: ASTM B446 for Inconel 625, AMS 5662/5664 or ASTM B637 for Inconel 718, ASTM B574 for Hastelloy C-276, and ASTM B164 for Monel 400. Heat number traceability is maintained throughout production. For aerospace and safety-critical applications, full first article inspection (FAI) reports and dimensional CMM reports are available on request.
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Every enquiry includes a DFM review — tolerance feasibility, material confirmation, and process approach confirmed before production starts. MOQ 1 piece.

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Quote Response
MOQ 1
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ISO
9001:2015
📐
DFM Review on Every Enquiry
Tolerance feasibility, fixturing strategy, and material confirmation. Specific, actionable feedback — not generic pushback.
🎯
First Article Inspection — Standard
FAI report on every new run. Material certs and surface treatment certs included with every shipment.
🔄
Same Process: Prototype to Production
Process plan from your prototype applies to production batches. No re-qualification when you scale.
3 / 4 / 5-Axis CNC + Turning
Complex structural parts, shafts, housings, and transmission components. Metals and engineering plastics.
ISO 9001:2015 3/4/5-Axis Milling CNC Turning CMM Inspection Global Delivery