| Processes | Wire Electrical Discharge Machining (EDM) |
| Equipment Capabilities | CNC Control Capabilities |
| Cutting Axis | 5-Axis |
| Materials | Cobalt Super Alloy Nickel Super Alloy Titanium Aluminum |
| Minimum Part Feature | .018" Diameter Electrodes |
| Material Thickness | 5" |
| Length | 30" |
| Width | 30" |
| Height | 15" |
| Surface Finish | 32 – 250 micro-inches |
| Tolerance (+/-) | ±.002" |
| EDM Standards | Component Repair Management, Inc. SOP 007 |
| Cleaning | Hydrogen Fluoride lon Cleaning (HFIC) Finish No. 4.1 Grit Blasting Finish No. 4.2 Hot Alkaline Cleaning Finish No. 4.3 Solvent Cleaning Blending Procedures (GE Standard Practices Manual 70-42-00) Light Duty Alkaline Cleaning (GE Standard Practices Manual 70-32-03) |
| Finishing | Vibratory Deburring Heat Treatment Coatings |
| Inspection | Coordinate Measuring Machine (CMM) Fluorescent Penetrant Inspection (FP I) Mil-Std-2175A (Castings) Method 5.3.1 (Visual) Method 5.3.2.2 {Penetrant) ASQ-Z1.4 & ASQ-Z1.9 ISO-10012 & ANSI-Z540.3 Spot Fluorescent Penetrant Inspection (GE 70-32-03) NACE Inspection Welding |
| Testing | Certified LeveI II NDT Liquid Penetrant Non Destructive Testing (Mil-HNBK-728/1) |
| Quality Program | FAA 14 CFR, Part 145 Repair Station Guidelines |
| Documentation | FAA Form 8130-3 (Airworthiness Approval Tag) |
| Additional Services | Repair Process Development Designated Engineering Representative (DER) |
| Production Volume | 1 to 30 parts |
| Typical Lead Time | 2 to 4 weeks |
| Industry Focus | Aerospace Military Commercial |
| Intended Application | Turbine Components Non-Rotating Vanes Vane Rings Nozzles Ducts Seals Related Non-Rotating Assemblies |
| Industry Standards | Federal Aviation Administration (FAA R9IR0970) European Aviation Safety Agency (EASA.145.5316) |
| File Formats | Modeling Capabilities |