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 |