Nickel superalloy parts held to 0.005 mm and Ra 0.4 μm — 5-axis on Mazak VARIAXIS centers, five-face gantry to 6 m, deep holes production-proven to 10,000 mm. Inconel 718 runs on our floor every week, not once a year. Upload your drawing via the RFQ form — an engineer replies within 24 hours.

Inconel 718 is a precipitation-hardened nickel superalloy that keeps its strength where most steels have already given up — which is exactly why your part is made from it, and exactly why many shops fail at it.
The failure mechanism is work-hardening. The austenitic nickel matrix hardens the instant it is deformed. Cut it with a dull tool or a timid feed and the edge rubs instead of shears; the surface layer hardens mid-cut, pass after pass, until the tool is machining something far harder than the bar that arrived. Add two more traits — thermal conductivity so low that cutting heat concentrates in the tool edge instead of the chip, and hard abrasive carbide particles in the matrix — and you have an alloy that punishes hesitation and rewards decisive, rigid, well-cooled cuts.
Every one of these behaviors is learned in scrapped parts and worn tooling, over years. We have already paid that tuition.

| Process | Envelope / range in Inconel 718 | Notes |
|---|---|---|
| 5-axis CNC machining | Mazak VARIAXIS i-800 (Ø800 class) & C-600 (Ø630 class); meter-to-12 m parts on self-built FWG-M1260 five-face gantry (travels 6/8/12 m) | True simultaneous 5-axis; A-axis 360° / B-axis ±120°; in-house CAM |
| CNC turning & mill-turn | Turning to Ø800 × 8,000 mm (FWT-80800); shop envelope Ø1,000 × 10,000 mm; mill-turn in one clamping (Mazak INTEGREX i-500S / i-400S) | ±0.01 mm at the machine; slender shafts to 4,500 mm as routine |
| Deep-hole drilling (BTA) | Ø20–360 mm; machine envelope 12,000 mm; production-proven Ø20–300 × 10,000 mm | Straightness 0.5 mm/m; eccentric bores, multi-step seal bores in one setup |
| Gun drilling | Ø2–40 mm, depths to 6,000 mm; hole tolerance ±0.02 mm, bore finish Ra 1.6 μm | 13 machines, all designed and built in-house |
| Precision grinding | Cylindrical to φ500 × 3,000 mm (MQ1350B), φ125 × 500 mm (MGB1412); internal φ200 × 250 mm (×2, Swedish); to 0.005 mm & Ra 0.4 μm | Inconel ground as routine |
| Welding & hardfacing | TIG and laser welding of Inconel 718; narrow-gap welding of superalloys to 60 mm depth | In-house, no subcontracting |
| Heat treatment & surface | Vacuum hardening, stress-relief, hard chrome / electroless nickel / PTFE coating | Coating allowance engineered into the machining program |
Commercial aviation — a national civil aircraft program. Semi-finish and precision machining of nickel-superalloy structural parts, on Mazak VARIAXIS 5-axis centers and our self-built FWG-M1260 five-face gantry, with final operations completed by a certified member of our group. In production today:
Air ducts →Seal-ring shields →Valve mounting seats →
We support commercial aviation programs only.
Oil & gas drilling. Inconel 718 MWD & LWD housings → in production for offshore downhole tools rated at 180 °C / 180 MPa, proven in sustained field operation.
Incoloy 925 — the companion grade on this page — runs as high-strength, corrosion-resistant shafts and housings for oilfield service, machined with the same superalloy discipline.


We do not publish speeds and feeds — those are earned per part, per feature, and frozen into the routing once proven. What we can tell you is the doctrine:
Tool life in 718 is managed, not gambled; a worn edge is a work-hardening generator
No dwelling, no rubbing; the cut stays below the hardened layer of the previous pass
Short overhangs, supported workpieces, and machines built heavy enough that the alloy does not get to chatter
High-pressure coolant delivery aimed at the shear zone, because in nickel alloys the heat goes into the tool, not the chip
Machining allowance, heat-treat sequencing, and final grinding planned as one chain, so the aged condition arrives at the finishing pass with stock left to correct distortion

Difficult alloys demand proof at both ends — what the mill delivered, and what we shipped:
The alloy’s mill origin follows your part through every operation to the inspection report
Incoming verification on our optical emission spectrometer (50+ elements, including C/P/S/N); no certificate is taken at face value
Tensile and impact testing on incoming material, in our own lab
Mill certs plus our dimensional inspection reports; FAI packages prepared to your format on request. A recent order shipped with 59 pages of documentation — that is what “documented” means here

Yes — and we plan for it. Where the print requires it, roughing is sequenced around heat treatment so finishing stock remains after aging, and final dimensions are closed by grinding. Tell us the specified condition and we will propose the routing.
From small seal-ring guards to meter-class 5-axis parts on Mazak VARIAXIS centers and 12 m five-face gantry work, turned parts to Ø800 × 8,000 mm, and deep bores production-proven to 10,000 mm. Single prototypes through batch production — from 1 piece, no minimum order.
Yes. Incoloy 925 runs in production as high-strength, corrosion-resistant shafts and housings for oilfield service, with the same traceability and inspection discipline as 718.
We support commercial aviation programs only — semi-finish and precision machining of nickel-superalloy structural parts for a national civil aircraft program, with final operations completed by a certified member of our group.
Every incoming lot is verified by optical emission spectrometry before it enters production, chemistry and mechanical properties are checked in-house, and the mill heat number follows your part to the inspection report. Certificates ship with every order.
Upload your drawing with the alloy condition — aged, annealed, or as-rolled. Within 24 hours, an engineer who runs these alloys weekly responds with a routing and a date.
Related: Materials Hub|Aerospace|Oil & Gas|5-Axis Machining

Trademark notice: INCONEL and INCOLOY are registered trademarks of Special Metals Corporation (PCC). They are used on this page solely to describe the alloys we machine (UNS N07718 / N09925); no affiliation or endorsement is implied.