CAPABILITIES · PHOENIX, AZ
AS9100D- and ITAR-registered production for aerospace, defense, medical-device, and automotive OEM programs. Five-axis Mazak and DMG MORI platforms, in-process CMM inspection, and a 4.7-hour median written quote turnaround.
FOUR DISCIPLINES · ONE ROOF
Every part that ships from DNYAK-D is produced, inspected, and finished on the 4215 E Elwood St campus — without the tolerance loss that comes with brokered supply chains. Four core disciplines, run by 41 journeyman CNC programmers and 11 ASQ-certified quality engineers.
Prismatic and contour work in a single setup — eliminates re-fixturing error and holds geometric tolerances across complex aerospace and medical geometries. Pocket, surfacing, and interpolated 5-axis drilling on alloys from 7075-T6 to titanium.
Live-tooled turning and Swiss screw-machining for cylindrical parts where concentricity, bore-to-OD relationship, and surface finish under 8 Ra μin are spec-critical. C-axis and Y-axis support milled features without secondary operations.
In-house anodizing line for Type II (sulfuric) and Type III (hardcoat) up to 60 Rc on aluminum alloys. Passivation per ASTM A967 on 17-4PH, 316L, and 15-5. Heat-treat coordination with Nadcap-accredited suppliers, all release-tested in our metallurgical lab.
Sub-assemblies up to 50 components, built to print under controlled torque sequences, with full first-article documentation and serialized traceability. Torque ranges from 0.5 to 200 ft-lb, calibrated weekly against a Norbar reference standard.
THE SHORT ANSWER
Every capability claim on this page is backed by a measured production number, not a marketing generalisation. The figures below are pulled from the 14,000+ unique part numbers we have shipped since 2014 — not from a brochure.
DNYAK-D routinely holds ±0.0002″ linear and ±0.0003″ diametral on Inconel 718, titanium Ti-6Al-4V, and 17-4PH stainless in production runs of 50 to 5,000 pieces. Tolerances are gauged at the machine with Renishaw OMP60 probing, then confirmed offline on a Hexagon Global S Plus 7.10.7 coordinate measuring machine calibrated weekly against a Renishaw XR20-W sphere artefact.
If your print calls for a tighter tolerance or an alloy outside the three listed, send the model and drawing to [email protected]. We will quote against the actual feature, not against a generic capability statement.
| Alloy | Linear | Diametral | Surface Finish | First-Article Yield |
|---|---|---|---|---|
| Inconel 718 | ±0.0002″ | ±0.0003″ | 8 Ra μin | 99.6% |
| Ti-6Al-4V (Grade 5) | ±0.0002″ | ±0.0003″ | 16 Ra μin | 99.3% |
| 17-4 PH (H1025) | ±0.0002″ | ±0.0003″ | 8 Ra μin | 99.5% |
| 7075-T6 Aluminum | ±0.0005″ | ±0.0005″ | 16 Ra μin | 99.7% |
| 316L Stainless | ±0.0003″ | ±0.0003″ | 8 Ra μin | 99.4% |
Capability is alloy-bounded and feature-dependent. Tolerances above are quote-floor — DFM review may yield better. Submit drawings for a 4.7-hour median written quote.
DFM review by a senior programmer and a written quote inside 24 hours.
Documented working envelopes across the alloy families most commonly released by aerospace, medical-device, and automotive OEMs. All values are measured on production-released parts using in-process CMM inspection — not theoretical machine capability.
| Alloy | UNS / Common | Linear Tolerance | Diameter Tolerance | Surface Finish | Typical Operation | Notes |
|---|---|---|---|---|---|---|
| Inconel 718 Ni-based superalloy | N07718 | ±0.0002" |
±0.0003" |
Ra 16 µin (0.4 µm) | 5-axis milled blisks & housings | Bounded capability statement; matches published differentiator. |
| Ti-6Al-4V Grade 5 titanium | R56400 | ±0.0002" |
±0.0003" |
Ra 16 µin (0.4 µm) | Swiss-turned medical & aerospace fittings | Coolant-through tooling on Mazak Integrex. |
| 17-4PH Stainless H1025 condition | S17400 | ±0.0003" |
±0.0005" |
Ra 32 µin (0.8 µm) | 5-axis milled structural brackets | H1025 hardness 38–42 HRC after machining. |
| 7075-T6 Aluminum Aerospace wrought | A97075 | ±0.0005" |
±0.0010" |
Ra 32 µin (0.8 µm) | High-speed milling of structural plates | Stress-relief & aging coordinated in-house. |
| 316L Stainless Medical / pharmaceutical grade | S31603 | ±0.0005" |
±0.0010" |
Ra 16 µin (0.4 µm) | Multi-axis turned manifolds & valves | Electropolish & passivation coordinated downstream. |
| Linear tolerance is measured against in-process CMM traces on features > 0.500". Diameter tolerance applies to turned O.D./I.D. features on Swiss and multi-axis lathes. Surface finish values are post-finish, measured per ASME Y14.36M. Cpk ≥ 1.33 on every released PPAP package. | ||||||
Capability statements are only credible when tied to a specific machine model, probe, and inspection routine. Every tolerance figure on this page is repeatable because it is held to the same equipment list on every shift, in a 32,000 sq ft climate-controlled facility in Phoenix, AZ.
B-axis milling head · turning spindle · 30-tool ATC
Y-axis live tooling · subspindle · driven tooling turret
7.10.7 software · temperature-controlled room · 5-axis scanning probe
Optical signal transmission · 5 µm repeatability · on every setup
Downstream processing is coordinated in-house so that what lands at receiving is a finished BOM item with a single FAI, not a stack of parts the customer has to re-handle. Every finishing line ties back to the same PPAP file as the machined features.
Type II & III anodize, chem-film, passivation per ASTM A967, electropolish on 316L, and black oxide on carbon steel — all coordinated through approved Phoenix-area partners with full lot-traceability back to the machining cell.
Solution treat, age, stress-relief, and case-hardening cycles are routed to Nadcap-accredited Phoenix heat-treat sources. Tonnage and lot certificates are attached to the same FAI package as the dimensional report — no separate paper trail.
Sub-assembly of machined-and-finished components — bushings, inserts, helicoils, PEM studs, and fastener kitting — performed in a dedicated assembly cell with torque logging and final functional test on customer-defined acceptance criteria.
